A 320321 Mel CDL
SAUDI ARABIAN AIRLINES MEL / CDL A‐320 A‐321 A320/321 MEL/CDL 30 JUN 12 MEL/CDL MANUAL NUMBER DATE CHAN
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SAUDI ARABIAN AIRLINES MEL / CDL A‐320 A‐321
A320/321 MEL/CDL
30 JUN 12 MEL/CDL MANUAL NUMBER
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THIS PAGE INTENTIONALLY LEFT BLANK
MEL/CDL MANUAL
A320/321 MEL/CDL
30 JUN 12 MEL /CDL MANUAL
00.01.01 CONTENTS
INTRODUCTION A.
Approval The A 320 / 321 MEL/CDL Manual has been developed using the following documents: 1) FAA 320/321 Master Minimum Equipment List (MMEL), Revision 22. 2) Airbus 320/321 Master Minimum Equipment List (MMEL), Date 31 JAN 12. 3) A 320/321 Airplane Flight Manual, Appendix CDL, Date 21 FEB 12.
General Authority of Civil Aviation Approval
Approved By: Director Flight Operations Safety & Economic Regulation
Signature & Date
A320/321 MEL/CDL
00.01.02 CONTENTS
B.
12 FEB 12 MEL/CDL MANUAL
MEL/CDL MANUAL CONTENTS AND ORGANIZATION This Manual is divided into four Sections as detailed below: Section 00 – Table of Contents, Introduction, Log of Revisions, and Control Page. Section 01 – EICAS CROSS-REFERENCE LIST and MEL and (O) PROCEDURES. This Section consists of MEL Table of Contents, Preamble, Definitions, EICAS Cross-Reference List introduction, EICAS Cross-References, MEL and Operating (O) procedures.
Section 02 – CDL. This Section consists of CDL Table of Contents, CDL Item General Locations, Notes, and CDL.
Section 03 – MEL (M) Procedures. This section has been removed as per the Airbus MMEL new format and replaced with Aircraft Maintenance Manual (AMM), this reference is only for maintenance personnel to follow.
Page Numbering: The MEL, CDL, and Maintenance Procedures pages are numbered as follows: 01.21.01 Assigned Page Number 02.21.01
ATA System Number 03.21.01
Section Number
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A320/321 MEL/CDL
30 JUN 12 MEL/CDL MANUAL ATA NUMBER
SYSTEM
00.02.01 TABLE OF CONTENTS PAGE
TABLE OF CONTENTS --
LOG OF REVISIONS.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.00.01 THRU 00.00.02
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INTTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.01.01 THRU 00.01.02
--
MEL/CDL MANUAL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . 00.02.01 THRU 00.02.02
--
LIST OF EFFECTIVE PAGES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00.03.01 THRU 00.03.22
MINIMUM EQUIPMENT LIST - SECTION 01 --
MEL TABLE OF CONTENTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.00.01 THRU 01.00.26
--
FAA MMEL PREAMBLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.01 THRU 01.01.02
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DEFINITIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.02 THRU 01.01.06
--
ECAM WARNING GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.02.01 THRU 01.02.02
--
ECAM WARNING LIST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.03.01 THRU 01.03.26
21
AIR CONDITIONING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.01 THRU 01.21.52
22
AUTO FLIGHT . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 THRU 01.22.24
23
COMMUNICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.01 THRU 01.23.24
24
ELECTRICAL POWER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.01 THRU 01.24.20
25
EQUIPMENT/FURNISHINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.01 THRU 01.25.26
26
FIRE PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01 THRU 01.26.20
27
FLIGHT CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.01 THRU 01.27.58
28
FUEL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01 THRU 01.28.62
29
HYDRAULIC POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.01 THRU 01.29.20
30
ICE AND RAIN PROTECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.01 THRU 01.30.26
31
INDICATING / RECORDING SYSTEMS . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 THRU 01.31.26
32
LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.01 THRU 01.32.58
33
LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.01 THRU 01.33.12
34
NAVIGATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01 THRU 01.34.32
35
OXYGEN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.01 THRU 01.35.08
36
PNEUMATIC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 THRU 01.36.12
38
WATER & WASTE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.38.01 THRU 01.38.02
46
INFORMATION SYSTEM . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.01 THRU 01.46.02
47
INERT GAS SYSTEM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.47.01 THRU 01.47.02
49
AIRBORNE AUXILIARY POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 THRU 01.49.02
52
DOORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.01 THRU 01.52.38
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WINDOWS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.01 THRU 01.56.04
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ENGINE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.01 THRU 01.70.02
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ENGINE FUEL AND CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.01 THRU 01.73.04
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IGNITION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.01 THRU 01.74.04
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ENGINE CONTROLS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.76.01 THRU 01.76.02
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ENGINE INDICATING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.01 THRU 01.77.06
78
EXHAUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01 THRU 01.78.06
79
OIL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.01 THRU 01.79.04
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STARTING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.01 THRU 01.80.02
CONFIGURATION DEVIATION LIST - SECTION 02 --
CDL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.00.01 THRU 02.00.04
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CDL INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.01.01 THRU 02.01.02
21
AIR CONDITIONING . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.21.01 THRU 02.21.02
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COMMUNICATIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.23.01 THRU 02.23.02
27
FLIGHT CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.01 THRU 02.27.20
28
FUEL. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.01 THRU 02.28.02
30
ICE AND RAIN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.30.01 THRU 02.30.02
32
LANDING GEAR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.01 THRU 02.32.02
33
LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.01 THRU 02.33.10
49
AIRBORNE AUXILIARY POWER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.49.01 THRU 02.49.02
51
STRUCTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.01 THRU 02.51.04
52
DOORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.01 THRU 02.52.36
53
FUSELAGE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.01 THRU 02.53.04
54
NACELLE/PAYLON . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.01 THRU 02.54.08
57
WINGS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.01 THRU 02.57.04
71
STRUCTURE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.01 THRU 02.71.02
78
EXHAUST . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.78.01 THRU 02.78.02
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TABLE OF CONTENTS TABLE OF CONTENTS TABLE OF CONTENTS TABLE OF CONTENTS MEL INTRODUCTION MEL INTRODUCTION MEL INTRODUCTION MEL INTRODUCTION MEL INTRODUCTION MEL INTRODUCTION GENERAL GENERAL
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AIR CONDITIONING
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12 FEB 12 12 FEB 12
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AUTO FLIGHT
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Rev 07
12 FEB 12
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AUTO FLIGHT AUTO FLIGHT
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Rev 07 Rev 07
12 FEB 12 12 FEB 12
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AUTO FLIGHT
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Rev 07
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COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS
01.23.01 01.23.02 01.23.03
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
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COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS
01.23.04 01.23.05 01.23.06
Rev 07 Rev 09 Rev 09
12 FEB 12 01 MAY 12 01 MAY 12
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COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS
01.23.07 01.23.08 01.23.09
Rev 07 Rev 09 Rev 07
12 FEB 12 01 MAY 12 12 FEB 12
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COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS
01.23.10 01.23.11 01.23.12
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
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COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS
01.23.13 01.23.14 01.23.15
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
23 23 23 23 23 23 23 23 23 24 24 24 24 24 24
COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS COMMUNICATIONS ELECTRICAL POWER ELECTRICAL POWER ELECTRICAL POWER ELECTRICAL POWER ELECTRICAL POWER ELECTRICAL POWER
01.23.16 01.23.17 01.23.18 01.23.19 01.23.20 01.23.21 01.23.22 01.23.23 01.23.24 01.24.01 01.24.02 01.24.03 01.24.04 01.24.05 01.24.06
Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07
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ELECTRICAL POWER
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12 FEB 12
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ELECTRICAL POWER ELECTRICAL POWER
01.24.08 01.24.09
Rev 10 Rev 07
30 JUN 12 12 FEB 12
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ELECTRICAL POWER
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12 FEB 12
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ELECTRICAL POWER ELECTRICAL POWER
01.24.11 01.24.12
Rev 07 Rev 07
12 FEB 12 12 FEB 12
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ELECTRICAL POWER
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Rev 07
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ELECTRICAL POWER ELECTRICAL POWER
01.24.14 01.24.15
Rev 07 Rev 07
12 FEB 12 12 FEB 12
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ELECTRICAL POWER
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Rev 07
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ELECTRICAL POWER ELECTRICAL POWER ELECTRICAL POWER
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Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
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ELECTRICAL POWER EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS
01.24.20 01.25.01 01.25.02
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
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EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS
01.25.03 01.25.04 01.25.05
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
25 25 25
EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS
01.25.06 01.25.07 01.25.08
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
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EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS
01.25.09 01.25.10 01.25.11
Rev 07 Rev 07 Rev 09
12 FEB 12 12 FEB 12 01 MAY 12
25 25 25 25 25 25 25 25 25 25 25 25 25 25 25
EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS EQUIPMENT & FURNISHNGS
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Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 10 Rev 07 Rev 07 Rev 07 Rev 07
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FIRE PROTECTION
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FIRE PROTECTION FIRE PROTECTION FIRE PROTECTION
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FIRE PROTECTION FIRE PROTECTION FIRE PROTECTION
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FIRE PROTECTION FIRE PROTECTION FIRE PROTECTION
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Rev 07 Rev 07 Rev 07
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FIRE PROTECTION FLIGHT CONTROL FLIGHT CONTROL
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Rev 07 Rev 07 Rev 07
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FLIGHT CONTROL FLIGHT CONTROL FLIGHT CONTROL
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Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07
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FLIGHT CONTROL
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FLIGHT CONTROL
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FUEL FUEL FUEL
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Rev 07 Rev 07l Rev 07l Rev 07l Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07 Rev 07
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FUEL FUEL FUEL
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FUEL FUEL FUEL
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Rev 07 Rev 07 Rev 07
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Rev 07 Rev 07 Rev 07
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HYDRAULIC
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HYDRAULIC HYDRAULIC
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HYDRAULIC
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HYDRAULIC HYDRAULIC HYDRAULIC
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HYDRAULIC HYDRAULIC HYDRAULIC
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HYDRAULIC ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION
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ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION
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ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION
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ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION INDICATING/RECORDING SYSTEM
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INDICATING/RECORDING SYSTEM INDICATING/RECORDING SYSTEM INDICATING/RECORDING SYSTEM
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PNEUMATIC WATER/WASTE WATER/WASTE
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INERT GAS SYSTEM AIRBORNE AUXILIARYPOWER AIRBORNE AUXILIARYPOWER DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS
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DOORS DOORS DOORS WINDOWS WINDOWS WINDOWS WINDOWS ENGINES ENGINES ENGINE FUEL AND CONTROL ENGINE FUEL AND CONTROL ENGINE FUEL AND CONTROL ENGINE FUEL AND CONTROL
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IGNITION
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CONFIGURATION DEVIATION LIST - SECTION 02 TABLE OF CONTENTS
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TABLE OF CONTENTS TABLE OF CONTENTS
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TABLE OF CONTENTS
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CDL INTRODUCTION CDL INTRODUCTION
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AIR CONDITIONING
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AIR CONDITIONING COMMUNICATIONS
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FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS
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FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS
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FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS
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FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS FLIGHT CONTROLS FUEL FUEL ICE AND RAIN PROTECTION ICE AND RAIN PROTECTION LANDING GEAR LANDING GEAR
02.27.13 02.27.14 02.27.15 02.27.16 02.27.17 02.27.18 02.27.19 02.27.20 02.28.01 02.28.02 02.30.01 02.30.02 02.32.01 02.32.02
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APU APU STRUCTURE
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STRUCTURE STRUCTURE STRUCTURE
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DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS DOORS
02.52.10 02.52.11 02.52.12 02.52.13 02.52.14 02.52.15 02.52.16 02.52.17 02.52.18 02.52.19 02.52.20 02.52.21 02.52.22 02.52.23 02.52.24
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52 DOORS
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02.52.35 02.52.36 02.52.37
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52 DOORS 53 FUSELAG 53 FUSELAG
02.52.38 02.53.01 02.53.02
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53 FUSELAG 53 FUSELAG 54 NACELLES / PYL
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Rev 07 Rev 07 Rev 07
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54 NACELLES / PYL 54 NACELLES / PYL 54 NACELLES / PYL
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Rev 07 Rev 07 Rev 07
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02.54.05 02.54.06 02.54.07
Rev 07 Rev 07 Rev 07
12 FEB 12 12 FEB 12 12 FEB 12
54 NACELLES / PYL 57 NACELLES / PYL 57 NACELLES / PYL 57 NACELLES / PYL 57 NACELLES / PYL 71 POWER PLANT 71 POWER PLANT 78 EXHAUST 78 EXHAUST
02.54.08 02.57.01 02.57.02 02.57.03 02.57.04 02.71.01 02.71.02 02.78.01 02.78.02
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A320/321 30 JUN 12 MEL ITEM
MEL/CDL
01.00.01 TABLE OF CONTENTS
PAGE MEL TABLE OF CONTENTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.00.01 FAA MMEL Preamble . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.01 Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.01.02 ECAM General. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.02.01 ECAM Messages Cross Reference List. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.03.01 ATA 21 - AIR CONDITIONING
21-00-03 21-00-04 21-01-01 21-01-02 21-01-03 21-01-04 21-07-01 21-07-02 21-07-03 21-07-04 21-09-01 21-09-02 21-09-03 21-21-01 21-23-01 21-26-01 21-26-02 21-26-03 21-26-04 21-26-05 21-26-06 21-26-07 21-26-08 21-26-09 21-26-10 21-28-03 21-28-04 21-31-01 21-31-02 21-31-03 21-31-04
AFT CRG HEAT MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.01 TEMP CTL 1(2) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.01 AIR COND Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.01 CABIN PRESS Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.02 CARGO VENT Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.02 VENTILATION Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.02 Indications on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.03 Indications on the CAB PRESS SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.05 Indications on the COND SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.06 Indications on the CRUISE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.06 VENT BLOWER FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.07 VENT EXTRACT FAULT Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.08 CAB PR SAFETY VALVE OPEN Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.08 Cabin Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.09 Lavatory and Galley Extraction Fan. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.09 Avionics Blower Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.10 Avionics Extract Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.14 Avionics Skin Exchanger Inlet Bypass Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.20 Avionics Skin Air Outlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.21 Avionics Skin Air Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.22 Avionics Skin Exchanger Isolation Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.26 Avionics Skin Exchanger Outlet Bypass Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.29 Avionics Air Conditioning Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.29 Avionics Ventilation Filte . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.30 Avionics Equipment Ventilation Computer (AEVC) . . . . . . . . . . . . . . . . . . . . . . . . 01.21.32 AFT Cargo Extraction Fan . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.34 AFT Cargo Isolation Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.35 Automatic Cabin Pressure Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (CPC, Outflow Valve AUTO Channel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.37 Manual Cabin Pressure Control System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (MAN V/S CTL selector, Outflow Valve MAN Channel). . . . . . . . . . . . . . . . . . . . . 01.21.39 Pressure Safety Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.40 Landing Elevation Selection AUTO Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.40
A320/321 01.00.02 TABLE OF CONTENTS
MEL/CDL
01 MAY 12 MEL
ITEM
PAGE ATA 21 - AIR CONDITIONING
21-31-05 21-43-02 21-51-02 21-51-03 21-52-01 21-52-02 21-55-01 21-61-01 21-63-02 21-63-03 21-63-04
(Cont’d)
Landing Elevation Selection MAN Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.41 AFT Cargo Compartment Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.41 Pack Flow Selection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.43 Pack Flow Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.43 Air Conditioning Pack. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.46 Air Conditioning Pack Ram Air Inlet Flap. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.47 Emergency Ram Air Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.48 Pack Turbine Bypass Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.49 Cockpit and Cabin Trim Air Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.49 Hot Air Pressure Regulating Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.50 Air Conditioning System Controller Channel (COND CTL 1(2)-A(B)) . . . . . . . . . . 01.21.52 ATA 22 - AUTO FLIGHT
22-01-01 22-01-02 22-05-01 22-05-02 22-05-03 22-05-04 22-10-01 22-10-02 22-10-03 22-10-04 22-10-05 22-10-06 22-10-07 22-30-01 22-30-02 22-30-03 22-60-01 22-60-02 22-60-03 22-60-04 22-70-01 22-70-02 22-70-03 22-70-04
FAC pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 FAC pb-sw OFF light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 AP Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 A/THR Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.01 Approach and Landing Capabilities on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02 Special Messages on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02 Autopilot (AP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.02 Flight Director (FD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.03 Take-over pb Priority Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.03 Take-over pb AP Disconnection Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.04 AUTO LAND lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.05 AP Disengagement Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.05 Sticks and Rudder Pedals Locking Solenoid in AP Mode . . . . . . . . . . . . . . . . . . . 01.22.05 Autothrust (A/THR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.06 Autothrust Instinctive Disconnect pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.06 Autothrust Disengagement Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.09 FAC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.10 FAC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.11 Windshear Detection System Predictive . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.12 Yaw Damper System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.13 Flight Management System (FMS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.13 Navigation Database . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.14 Performance Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.15 Fuel/Time Prediction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.15
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ITEM
01.00.03 TABLE OF CONTENTS PAGE
ATA 22 - AUTO FLIGHT( cont’d) 22-81-01 22-81-02 22-81-03 22-82-01 22-82-02 22-82-04 22-83-01
Auto Flight Control Panel (FCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.16 EFIS Control Panel (FCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.18 FCU Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.20 MCDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.21 MCDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.21 MCDU Annunciator light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.22.21 Flight Management and Guidance Computer (FMGC) . . . . . . . . . . . . . . . . . . . . . 01.22.22 ATA 23 - COMMUNICATIONS
23-00-01 23-01-01 23-01-02 23-09-01 23-09-02 23-10-01 23-10-02 23-10-03 23-13-01 23-13-02 23-20-01 23-20-02 23-31-01 23-40-01 23-40-02 23-40-03 23-40-04 23-51-01 23-51-02 23-51-03 23-51-04 23-51-05 23-51-06 23-52-01 23-52-02
CIDS 1(2) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.01 RCDR Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.01 CALLS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.02 COM HF 1(2) EMITTING Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.04 COM VHF 1(2)(3) EMITTING Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.04 HF System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.05 VHF System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.05 SATCOM Voice Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.05 Radio Management Panel (RMP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.05 RMP Selection Key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.05 Aircraft Communications Addressing Reporting System (ACARS) . . . . . . . . . . . 01.23.06 SATCOM Data Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.06 Passenger Address System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.07 Mechanical Call Horn. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.07 Flight Crew Interphone System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.07 Flight Crew to Ground Communication System. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.08 Service Interphone Jack . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.08 SELCAL Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.08 Boomset. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.09 Hand Microphone. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.09 Cockpit Loudspeaker . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.09 Cockpit Loudspeaker Volume Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.09 Sidestick Radio selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.10 CAPT and F/O ACP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.10 ACP 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.10
A320/321 01.00.04 TABLE OF CONTENTS
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12 FEB 12 MEL PAGE
ATA 23 - COMMUNICATIONS ( cont’d) 23-52-03 23-52-04 23-52-05 23-52-06 23-52-07 23-53-01 23-71-01 23-72-01 23-73-01 23-73-02 23-73-03 23-73-04 23-73-05 23-73-06 23-73-07 23-73-08 23-73-10 23-74-01 23-74-02 23-74-03 23-74-06 23-74-08 23-74-09 23-74-10 23-74-11
Fourth Occupant ACP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11 ACP in the Avionics Compartment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11 ACP Transmission Key . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11 ACP Reception knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11 ACP Reception knob light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.11 AUDIO SWITCHING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12 Cockpit Voice Recorder (CVR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12 Cockpit Door Surveillance System (CDSS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.12 Cabin Intercommunication Data System (CIDS) . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.14 DEU A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.15 DEU B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.16 Cabin Individual Call . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.18 Cabin Loudspeaker . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.18 Handset . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.19 Prerecorded Announcement and Music Reproducer (PRAM) . . . . . . . . . . . . . . . 01.23.20 Cabin Assignment Module (CAM) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.21 Smoke Detection Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.21 FAP Display Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23 EMER pb on Hardkey FAP Sub-panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23 Other Controls on Hardkey FAP Sub-panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23 Door Bottle Pressure Monitoring on the FAP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.23 Slide Pressure Monitoring on the FAP. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24 Area Call Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24 Attendant Information Panel (AIP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24 Additional Attendant Panel (AAP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.23.24
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ITEM
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ATA 24 - ELECTRICAL POWER 24-00-01 24-00-03 24-01-01 24-01-02 24-07-01 24-07-02 24-07-03 24-09-01 24-09-02 24-22-01 24-22-02 24-23-01 24-24-01 24-24-02 24-24-03 24-25-01 24-25-02 24-26-01 24-26-02 24-26-03 24-28-01 24-32-01 24-34-01 24-35-01 24-35-02 24-38-01 24-38-02 24-38-03 24-41-01 24-41-02
DC BUS TIE MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.01 AC GEN MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.01 ELEC Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.01 EMER ELEC PWR Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.04 AC Generation Indications on the ELEC SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.24.05 DC Generation Indications on the ELEC SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.24.06 AC ESS BUS SHED Indication on the ELEC SD page . . . . . . . . . . . . . . . . . . . . . 01.24.06 ELEC AC ESS BUS SHED Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.06 C/B TRIPPED Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.07 AC Main Generation (IDG, GCU, Line Contactor) . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.08 AC Bus Tie Control Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.11 AC Auxiliary Generation (APU Generator, GCU, Line Contactor) . . . . . . . . . . . . . 01.24.11 Emergency Generator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.11 RAT Extension Automatic Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.11 RAT Extension Manual Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.12 Manual Transfer to the AC BUS 2 (ALTN Function) . . . . . . . . . . . . . . . . . . . . . . . 01.24.12 Automatic Transfer to the AC BUS 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.12 GALY & CAB Automatic Load Shed System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.13 GALY & CAB Manual Load Shed System (GALY & CAB pb-sw) . . . . . . . . . . . . . 01.24.14 Commercial Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.15 Static Inverter AC Generation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.15 DC Main Generation (TR 1, TR 2) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.16 DC Emergency Generation (ESS TR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.17 DC TIE Contactor 1PC1 (DC BUS 1-DC BAT BUS), . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4PC (DC ESS BUSDC BAT BUS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.18 DC TIE Contactor 1PC2 (DC BUS 2-DC BAT BUS) . . . . . . . . . . . . . . . . . . . . . . . 01.24.18 BAT 1(2) Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.18 Battery Charger Limiter (BCL) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.19 Battery Voltmeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.19 Ground Power Control Unit (GPCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.20 External Power Receptacle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.24.20
A320/321 01.00.06 TABLE OF CONTENTS
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ITEM
12 FEB 12 MEL PAGE
ATA 25 - EQUIPMENT / FURNISHINGS 25-07-01 25-07-01 25-07-02 25-07-02 25-07-03 25-07-04 25-11-01 25-11-02 25-11-03 25-11-04 25-11-05 25-11-06 25-11-07 25-11-08 25-11-09 25-11-10 25-11-11 25-11-12 25-12-01 25-12-02 25-12-03 25-12-04 25-12-05 25-12-06 25-12-07 25-12-08 25-13-01 25-13-02 25-20-01 25-20-03 25-28-01 25-35-01 25-40-01
Passenger Door Slide Permanently Indicated Armed (A320) . . . . . . . . . . . . . . . . 01.25.01 Cabin Passenger Door / Emergency Exit Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Permanently Indicated Armed (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.01 Passenger Door Slide Permanently Indicated Not Armed (A320) . . . . . . . . . . . . . 01.25.02 Cabin Passenger Door / Emergency Exit Slide . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Permanently Indicated Not Armed (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.02 Emergency Exit Slide Permanently Indicated Armed . . . . . . . . . . . . . . . . . . . . . . 01.25.03 Emergency Exit Slide Permanently Indicated Not Armed . . . . . . . . . . . . . . . . . . . 01.25.03 Pilot Seat Manual Horizontal Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04 Pilot Seat Manual Vertical Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04 Pilot Seat Recline Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04 Pilot Seat Other Manual Adjustments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.04 Pilot Seat Electrical Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.05 Pilot Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.05 Pilot Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06 Pilot Sidestick Armrest Height Adjustment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06 Pilot Sidestick Armrest Pitch Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06 Pilot Sidestick Armrest Memory Position Display . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.06 Pilot Inboard Armrest Vertical Adjustment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07 Pilot Seat Headrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07 Third Occupant Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07 Third Occupant Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.07 Third Occupant Seat Abdominal Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08 Third Occupant Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08 Fourth Occupant Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08 Fourth Occupant Seat Shoulder Harness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08 Fourth Occupant Seat Abdominal Belt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.08 Fourth Occupant Seat Fifth Strap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09 Pilot Sliding Table . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09 Pilot Retractable Footrest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09 Passenger Seat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.09 Cabin Attendant Seat. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.10 Overhead Storage Bin(s)/Cabin and Galley storage Compartment/ Closest. . . . . 01.25.12 Galley Waste Compartment Flapper Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.12 Toilet Waste Compartment Flapper Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.13
A320/321 30 JUN 12 MEL
MEL/CDL
01.00.07 TABLE OF CONTENTS
ITEM
PAGE ATA 25 - EQUIPMENT / FURNISHINGS
25-40-02 25-40-03 25-50-01 25-50-02 25-50-03 25-50-04 25-62-01 25-62-02 25-62-03 25-62-04 25-62-04 25-62-05 25-62-06 25-62-06 25-62-07 25-62-08 25-63-01 25-64-01 25-64-02 25-64-03 25-65-01 25-65-02 25-65-03 25-65-04 25-65-05 25-65-06 25-66-01 25-66-02 25-70-01 25-70-04 25-70-05
( cont’d)
Exterior Lavatory Ashtray. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.14 Interior Lavatory Ashtray . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.14 Cargo Loading System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.14 Decompression Panels in the Cargo Compartments. . . . . . . . . . . . . . . . . . . . . . . 01.25.15 Sidewall Linings and Ceiling Panels in the Cargo Compartments . . . . . . . . . . . . . 01.25.15 Cargo Compartment Restraint Components (Nets, Attach Points, Stanchions) . . 01.25.15 Cabin Passenger Door Slide or Slide Raft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.16 Overwing Emergency Exit Slide or Slide Raft (A320) . . . . . . . . . . . . . . . . . . . . . . 01.25.16 Emergency Exit Slide or Slide Raft (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.16 SLIDE ARMED light (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.17 SLIDE ARMED light (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.17 Survival Kit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.17 Passenger Door CHECK SLIDE PRESSURE Message on . . . . . . . . . . . . . . . . . . . . . . . . Flight Attendant Panel (FAP) (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.17 Passenger Door CHECK SLIDE PRESSURE Message on . . . . . . . . . . . . . . . . . . . . . . . . Flight Attendant Panel (FAP) (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.18 Overwing Emergency Exit CHECK SLIDE PRESSURE . . . . . . . . . . . . . . . . . . . . . . . . . . . Message on Flight Attendant Panel (FAP) (A320). . . . . . . . . . . . . . . . . . . . . . . . . 01.25.18 Overwing Escape Life Line . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.19 Emergency Evacuation Signaling System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (COMMAND pbsw, HORN SHUT OFF pb, CAPT&PURS and CAPT sw). . . . . . . 01.25.19 First Aid Kit. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.20 Emergency Medical Kit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.21 Automated External Defibrillator (AED) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.22 Cockpit Flashlight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.23 Cabin Flashlight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.23 Crash Axe/Crowbar . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.23 Emergency Locator Transmitter (ELT). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.23 Fireproof Gloves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.24 Megaphone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.24 Life Vest . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.24 Supplementary Life Raft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.24 Non-Essential Equipment & furnishings (NEF) . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.25 Movie/stereo Equipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.26 Overhead Reading Lamp. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.25.26
A320/321 01.00.08 TABLE OF CONTENTS
MEL/CDL
ITEM
01 MAY 12 MEL PAGE
ATA 26 - FIRE PROTECTION 26-00-01 26-01-01 26-01-02 26-12-01 26-12-02 26-12-03 26-12-04 26-12-05 26-13-01 26-13-02 26-15-01 26-16-01 26-16-01 26-16-02 26-16-02 26-17-01 26-22-01 26-22-02 26-22-03 26-22-04 26-22-05 26-22-06 26-22-07 26-23-01 26-23-02 26-24-01 26-25-01
SMOKE MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01 FIRE Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.01 CARGO SMOKE Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05 Engine Fire Detection Loop A on the Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05 Engine Fire Detection Loop A on the Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.05 Engine Fire Detection Loop B on the Engine 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06 Engine Fire Detection Loop B on the Engine 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06 FIRE light on the ENG MASTER Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06 APU Fire Detection Loop A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.06 APU Fire Detection Loop B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.07 Avionics Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.07 Smoke Detector in the FWD Cargo Compartment (A320). . . . . . . . . . . . . . . . . . . 01.26.08 Smoke Detector in the FWD Cargo Compartment (A321). . . . . . . . . . . . . . . . . . . 01.26.09 Smoke Detector in the AFT and the BULK Cargo Compartments (A321) . . . . . . . 01.26.10 Smoke Detector in the AFT and the BULK Cargo Compartments (A320) . . . . . . . 01.26.11 Lavatory Smoke Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.12 APU Automatic Fire Extinguishing Control on Ground . . . . . . . . . . . . . . . . . . . . . 01.26.13 APU Fire Extinguisher Overpressure Indication (Red Disc) . . . . . . . . . . . . . . . . . 01.26.14 Squib of the APU Fire Extinguisher Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.15 APU Fire Extinguisher Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.15 APU AUTO EXTING TEST pb-sw on the Maintenance Panel. . . . . . . . . . . . . . . . 01.26.16 APU FIRE light on the External Power Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.16 APU SHUT OFF pb on the External Power Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.17 Cargo Agent Bottle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.17 Squib of the Cargo Bottle 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.19 Portable Fire Extinguisher . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.19 Lavatory Waste Bin Fire Extinguishing System . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.26.20
A320/321 30 JUN 12 MEL
MEL/CDL
ITEM
01.00.09 TABLE OF CONTENTS PAGE
ATA 27 - FLIGHT CONTROLS 27-00-01 27-00-02 27-01-01 27-07-01 27-07-02 27-07-03 27-07-04 27-07-05 27-07-06 27-07-07 27-07-08 27-07-09 27-07-10 27-07-11 27-07-12 27-08-01 27-08-02 27-14-01 27-14-02 27-14-03 27-14-04 27-21-01 27-22-01 27-22-02 27-22-03 27-23-01 27-34-01 27-34-02 27-40-01 27-40-02 27-51-01 27-51-02 27-51-03 27-54-01 27-54-02 27-54-03 27-64-01 27-64-02
F/CTL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.01 SFCS MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.01 FLT CTL Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.01 Aileron Actuator Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.27.02 Aileron Position Indication on the F/CTL SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.27.02 Elevator Actuator Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . 01.27.04 Elevator Position Indication on the F/CTL SD page. . . . . . . . . . . . . . . . . . . . . . . . 01.27.05 Pitch Trim Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . 01.27.06 Rudder Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.27.08 Rudder Trim Position Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . 01.27.09 Rudder Travel Limiter Position Indication on the F/CTL SD page . . . . . . . . . . . . . 01.27.09 ELAC Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.09 SEC Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.09 Spoilers/ Speed brakes Indication on the F/CTL SD page . . . . . . . . . . . . . . . . . . 01.27.10 Spoilers/ Speed brakes Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . 01.27.11 Flap Position Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.13 Slat Position Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.13 Left Aileron Blue Servo-Control (Controlled by ELAC 1) . . . . . . . . . . . . . . . . . . . . 01.27.14 Left Aileron Green Servo- Control (Controlled by ELAC 2) . . . . . . . . . . . . . . . . . . 01.27.15 Right Aileron Green Servo- Control (Controlled by ELAC 1) . . . . . . . . . . . . . . . . . 01.27.15 Right Aileron Blue Servo- Control (Controlled by ELAC 2) . . . . . . . . . . . . . . . . . . 01.27.16 Rudder Pedal Adjustment System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.17 Rudder Trim System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.17 Manual Rudder Trim Reset Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.18 Rudder Trim Position Indication on the Center Pedestal . . . . . . . . . . . . . . . . . . . . 01.27.18 Rudder Travel Limiter System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.18 Elevator Servo Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.18 Elevator Servo Control Position Transducer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.19 Stabilizer Mechanical Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.19 Stabilizer Actuator Electrical Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.19 SFCC Flap Channel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.20 SFCC Slat Channel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.21 Flap Wing Tip Brakes Solenoid . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.21 Flap Hydraulic Motor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.22 Flap PCU Valve Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.22 Flap Pressure Off Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.22 Spoiler 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.23 Spoiler 1 or 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.23
A320/321 01.00.10 TABLE OF CONTENTS
MEL/CDL
30 JUN 12 MEL
ITEM
PAGE ATA 27 - FLIGHT CONTROLS
27-64-03 27-64-04 27-64-05 27-81-01 27-84-01 27-84-02 27-84-03 27-92-01 27-92-02 27-92-03 27-92-04 27-92-05 27-93-01 27-93-02 27-93-03 27-94-01 27-94-02 27-94-03 27-95-01 27-95-02
(Cont’d)
Spoiler 2 or 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.25 Spoilers 1 and 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.26 Spoilers 3 and 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.29 Slat Wing Tip Brakes Solenoids. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30 Slats Hydraulic Motor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30 Slat PCU Valve Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30 Slat Pressure- Off Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.30 Speed brake Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.31 Ground Spoiler Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.34 SIDESTICK PRIORITY light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35 Sidestick Dual Input Visual Warnings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35 Sidestick Dual Input Aural Warning . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35 ELAC 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.35 ELAC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.44 Pitch Normal Law. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.45 SEC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.45 SEC 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.51 SEC 3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.55 FCDC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.57 FCDC 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.27.57 ATA 28 - FUEL
28-00-01 28-01-01 28-07-01 28-07-02 28-07-03 28-07-04 28-09-01 28-09-01 28-09-02 28-09-02 28-09-03 28-12-01 28-12-02 28-12-03 28-12-03
FUEL MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01 FUEL Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.01 Fuel Quantity Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.05 Fuel Temperature Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . 01.28.22 Tank Pump Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.23 Valve Indications on the FUEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.23 FUEL L(R) INNER(OUTER) TK HI TEMP Alert (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.27 FUEL L(R) WING TK HI TEMP Alert (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.28 FUEL L(R) INNER(OUTER) TK LO TEMP Alert (A320) . . . . . . . . . . . . . . . . . . . . 01.28.30 FUEL L(R) WING TK LO TEMP Alert (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.31 FUEL ACT XFR FAULT Alert (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.33 Overpressure Protector between Inner and Outer Tank (A320) . . . . . . . . . . . . . . 01.28.33 Overpressure Protector in Vent Surge Tank . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36 Overpressure Protector in The Inner Tank (A320). . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36 Overpressure Protector in The Wing Tank (A321). . . . . . . . . . . . . . . . . . . . . . . . . 01.28.36
A320/321 12 FEB 12 MEL
MEL/CDL
01.00.11 TABLE OF CONTENTS
ITEM
PAGE ATA 28 - FUEL
28-12-04 28-12-04 28-12-05 28-15-01 28-15-02 28-20-01 28-21-01 28-21-02 28-21-02 28-21-03 28-22-01 28-23-01 28-24-01 28-25-01 28-25-02 28-25-03 28-25-04 28-25-05 28-26-01 28-28-01 28-28-02 28-28-03 28-28-04 28-28-05 28-28-06 28-28-07 28-28-08 28-28-09 28-29-01 28-43-01 28-46-01 28-46-01 28-46-02 28-46-02 28-46-03 28-46-04 28-46-04 28-46-05 28-50-01
(Cont’d )
Overpressure Protector between Center and Inner Tank (A320) . . . . . . . . . . . . . 01.28.37 Overpressure Protector between Center and Wing Tank (A321) . . . . . . . . . . . . . 01.28.37 Overpressure Protector in the ACT (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . 01.28.37 LH Wing Transfer Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.38 RH Wing Transfer Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.39 Automatic Fuel Feed System (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.40 Wing Tank Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.40 Center Tank Pump (A320)(ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.41 Center Tank Pump (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.44 Wing Tank Pump Sequence Valve (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.44 APU Fuel Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.45 Crossfeed Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.45 Engine LP Fuel Valve Electrical Motor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.46 Fuel Quantity Preselector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.46 Fuel Quantity on the Refuel/Defuel Control Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.46 Refuel Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.46 Transfer Defuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.47 Exterior Refuel/Defuel Control Panel (A320 & A321) . . . . . . . . . . . . . . . . . . . . . . 01.28.47 Center Tank Transfer Valve (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.48 ACT Auto Transfer System (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.49 ACT Transfer Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.51 ACT Transfer Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.52 ACT Air Shutoff Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.52 ACT Inward Pressure Relief Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.52 ACT Vent Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.54 ACT Refuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.55 ACT Integrated Impact Wall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.55 ACT 1 Inlet Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.56 APU LP Fuel Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.57 Manual Magnetic Indicators (A320 & A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.28.59 High Level Detection System in the Inner Tank (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.60 High Level Detection System in the Wing Tank (A321) . . . . . . . . . . . . . . . . . . . . . 01.28.60 High Level Detection System in the Center Tank (A320) . . . . . . . . . . . . . . . . . . . 01.28.60 High Level Detection System in the Center Tank (A320) (ACTs) . . . . . . . . . . . . . 01.28.61 High Level Detection System in the ACT (A320) (ACTs). . . . . . . . . . . . . . . . . . . . 01.28.61 Low Level Detection System in the Inner Tank (A320) . . . . . . . . . . . . . . . . . . . . . 01.28.61 Low Level Detection System in the Wing Tank (A321) . . . . . . . . . . . . . . . . . . . . . 01.28.62 Low Level Detection System in the ACT (A320) (ACTs) . . . . . . . . . . . . . . . . . . . . 01.28.62 Fuel Quantity Indicating Computer (FQIC) Channel . . . . . . . . . . . . . . . . . . . . . . . 01.28.62
A320/321 01.00.12 TABLE OF CONTENTS
MEL/CDL
ITEM
12 FEB 12 MEL PAGE
ATA 29 - HYDRAULIC POWER 29-01-01 29-01-02 29-07-01 29-07-02 29-07-03 29-07-04 29-07-05 29-07-06 29-07-07 29-07-08 29-09-01 29-09-02 29-09-03 29-09-04 29-09-05 29-09-06 29-09-07 29-09-08 29-09-09 29-10-01 29-10-02 29-10-03 29-10-04 29-10-05 29-10-07 29-10-08 29-10-09 29-22-01 29-23-01 29-24-01
HYD Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.01 Maintenance HYD Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.03 Yellow ELEC Pump Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . 01.29.03 Engine Driven Pump Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . 01.29.03 Fire Valve Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.03 PTU Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04 Reservoir Quantity Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . 01.29.04 RAT Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04 System Label Indication on the HYD SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.04 System Pressure Indication on the HYD SD page. . . . . . . . . . . . . . . . . . . . . . . . . 01.29.06 HYD B(Y) ELEC PUMP LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08 HYD B(Y) ELEC PUMP OVHT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08 HYD G(Y) ENG 1(2) PUMP LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.08 HYD G(B)(Y) RSVR LO AIR PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.10 HYD G(B)(Y) RSVR LO LVL Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.10 HYD G(B)(Y) RSVR OVHT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.11 HYD PTU FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.11 HYD RAT FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.12 HYD G(B)(Y)(B+G)(G+Y) (B+Y) SYS LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . 01.29.12 Engine Driven Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14 Engine Driven Pump Depressurization Function . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14 Blue System Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.14 Hydraulic System Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15 Yellow Brake Accumulator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15 Engine Pump Fire Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15 Hydraulic System Filter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.15 Hydraulic Case Drain Filter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16 Ram Air Turbine. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16 Power Transfer Unit (PTU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.16 Yellow System Electric Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.29.18
A320/321 30 JUN 12 MEL
MEL/CDL
ITEM
01.00.13 TABLE OF CONTENTS PAGE
ATA 30 - ICE AND RAIN PROTECTION 30-00-01 30-01-01 30-01-02 30-07-01 30-07-02 30-11-01 30-21-01 30-31-01 30-31-02 30-31-03 30-31-04 30-31-05 30-42-01 30-42-02 30-42-03 30-42-04 30-42-05 30-45-01 30-45-02 30-45-03 30-71-01 30-71-02 30-81-01 30-81-02 30-81-03
ICE DETECT MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.01 ANTI ICE Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.01 Wiper Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.03 ANTI ICE Indication on the BLEED SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.03 Arrow Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.03 Wing Anti-Ice Control Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.04 Engine Anti-Ice Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.08 Probe Heat Computer (PHC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.14 Pitot Heater . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.16 Static Ports Heater. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.18 Angle of Attack (AOA) Probes Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.19 TAT Probes Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.20 Window Heat Computer. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.21 Fixed Lateral Window and Sliding Window Heating . . . . . . . . . . . . . . . . . . . . . . . 01.30.22 Windshield Heating . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.22 PROBES/ WINDOW HEAT pb-sw AUTO Control . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.22 PROBES/WINDOW HEAT pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.22 Windshield Wiper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.23 Windshield Wiper PARK Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.23 Rain Repellent System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.24 Waste Water Drain Mast Heating System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.24 Waste Water Drain Line Ice Protection System. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.24 Ice Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.25 External Visual Icing Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.25 Lighting of External Visual Icing Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.30.25 ATA 31 - INDICATING / RECORDING SYSTEMS
31-00-01 31-00-02 31-00-03 31-00-04 31-00-05 31-00-06 31-05-01 31-05-02 31-05-03 31-05-04 31-05-05 31-05-06
QAR MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 ACMS MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 DAR MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 CFDIU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 DMC 1/3 MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.01 DMC 2/3 MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.02 AP Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.02 A/THR Related Indications on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.02 Approach and Landing Capabilities on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.02 Special Messages on the FMA . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.02 Actual Airspeed Reference Line and Scale Indications on the PFD . . . . . . . . . . . 01.31.03 Mach Number Indication on the PFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03
A320/321 01.00.14 TABLE OF CONTENTS
MEL/CDL
ITEM
12 FEB 12 MEL PAGE
ATA 31 - INDICATING / RECORDING SYSTEMS (Cont’d ) 31-05-07 31-05-08 31-05-09 31-05-10 31-05-11 31-05-12 31-06-01 31-06-02 31-06-04 31-06-05 31-06-06 31-06-07 31-07-01 31-07-02 31-08-01 31-08-02 31-08-03 31-08-04 31-20-01 31-30-01 31-30-02 31-30-03 31-30-04 31-30-05 31-30-06 31-30-07 31-38-01 31-38-02 31-38-03 31-53-01 31-53-02 31-53-03 31-53-04 31-53-05 31-53-06 31-55-01 31-56-01 31-56-02
VMO/MMO Characteristic Speed Indication on the PFD . . . . . . . . . . . . . . . . . . . . 01.31.03 Altitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03 Vertical Speed Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.03 Other Air Data Related Indications on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04 Attitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04 Heading Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04 Ground Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04 True Air Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.04 Heading Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05 Position (Aircraft Symbol) Indication on the ND. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05 Navigation Station Information on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05 Chrono Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05 Indications on the System Display pages . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.05 Permanent Data Indications on the SD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.06 Engine Parameter Indications on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.06 Fuel On Board (FOB) Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07 MEMO Messages on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07 Slats/Flaps Position Indications on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07 Electrical Clock Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.07 Centralized Fault Display System (CFDS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.08 Digital AIDS Recorder (DAR). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.08 Digital Flight Data Recorder (DFDR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09 Data Management Unit (DMU) part of Flight Data Interface . . . . . . . . . . . . . . . . . . . . . . . . and Management Unit (FDIMU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09 Flight Data Interface Unit (FDIU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.09 Quick Access Recorder (QAR) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10 Printer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10 DATA LOADING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10 Data Loading Routing Box (DLRB) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.10 Multipurpose Disk Drive Unit (MDDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11 Flight Warning Computer (FWC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11 MASTER CAUT Cancel Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11 MASTER WARN Cancel Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11 MASTER CAUT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.11 MASTER WARN light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.12 Altitude Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.12 System Data Acquisition Concentrator (SDAC). . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13 System Page Manual Call pb onthe ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13 ALL pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.13
A320/321 30 JUN 12 MEL
MEL/CDL
ITEM
01.00.15 TABLE OF CONTENTS PAGE
ATA 31 - INDICATING / RECORDING SYSTEMS (Cont’d ) 31-56-03 31-56-04 31-56-05 31-56-06 31-56-07 31-62-01 31-62-02 31-62-03 31-63-01 31-63-02 31-63-03 31-63-04 31-63-05 31-63-06 31-68-01 31-68-02 31-68-03 31-68-04 31-68-05
CLR pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.14 EMER CANC pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.14 RCL pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.14 STS pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.14 T.O CONFIG pb on the ECP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.14 DMC 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.16 DMC 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.18 DMC 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.19 PFDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.22 PFDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.22 NDU 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.22 NDU 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.23 SDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.23 EWDU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.24 AIR DATA SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . 01.31.24 ATT HDG SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . 01.31.24 ECAM/ND XFR SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . 01.31.24 EIS DMC SWITCHING selector on the Center Pedestal . . . . . . . . . . . . . . . . . . . . 01.31.25 PFD/ND XFR pb on the Lateral Instrument Panel . . . . . . . . . . . . . . . . . . . . . . . . . 01.31.25 ATA 32 - LANDING GEAR
32-07-01 32-07-02 32-07-03 32-07-04 32-07-05 32-07-06 32-07-07 32-07-08 32-07-09 32-07-10 32-07-11 32-07-12 32-07-13
Brakes Temperature Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . 01.32.01 L/G Position Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.17 L/G Doors Position Indication on the WHEEL SD page. . . . . . . . . . . . . . . . . . . . . 01.32.17 L/G CTL Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.17 UP LOCK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.17 [Y] N/W STEERING Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . 01.32.17 Tire Pressure Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.18 ANTI SKID, [1], [2] Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . 01.32.18 AUTO BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.18 [G] NORM BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . 01.32.18 Release Brake Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.32.18 ACCU PRESS/ACCU ONLY Indication on the WHEEL SD page . . . . . . . . . . . . . 01.32.19 [Y] ALTN BRK Indication on the WHEEL SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.32.19
A320/321 01.00.16 TABLE OF CONTENTS
MEL/CDL
ITEM
30 JUN 12 MEL
PAGE ATA 32 - LANDING GEAR (Cont’d)
32-09-01 32-09-02 32-11-01 32-12-01 32-31-01 32-31-02 32-32-01 32-32-02 32-32-03 32-32-04 32-32-05 32-32-06 32-32-07 32-32-08 32-32-09 32-32-10 32-32-11 32-32-12 32-32-13 32-32-14 32-32-15 32-32-16 32-33-01 32-41-01 32-41-02 32-42-01 32-42-02 32-42-03 32-42-04 32-42-05 32-42-06 32-42-08 32-42-09 32-44-01 32-44-02 32-44-03
BRAKES-N/WS MINOR FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.19 WHEEL TYRE LO PR Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.21 Main Gear Torque Link Damper . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.22 Ground Opening Cable . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.22 Landing Gear Control and Interface Unit (LGCIU). . . . . . . . . . . . . . . . . . . . . . . . . 01.32.23 Landing Gear Retracting System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.26 LGCIU 1 Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.26 LGCIU 2 RH L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.27 LGCIU 2 LH L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.29 LGCIU 2 Nose L/G Shock Absorber Proximity Detector . . . . . . . . . . . . . . . . . . . . 01.32.32 LGCIU 2 RH L/G Down Lock Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.33 LGCIU 2 LH L/G Down Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.34 LGCIU 2 Nose L/G Down Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . 01.32.35 LGCIU 2 RH L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.36 LGCIU 2 LH L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.37 LGCIU 2 Nose L/G Up Lock Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.38 LGCIU 2 RH L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.39 LGCIU 2 LH L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.39 LGCIU 2 Nose L/G Doors Open Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . 01.32.40 LGCIU 2 RH L/G Doors Closed Proximity Detector. . . . . . . . . . . . . . . . . . . . . . . . 01.32.41 LGCIU 2 LH L/G Doors Closed Proximity Detector . . . . . . . . . . . . . . . . . . . . . . . . 01.32.42 LGCIU 2 Nose L/G Doors Closed Proximity Detector . . . . . . . . . . . . . . . . . . . . . . 01.32.43 Landing Gear Gravity Extension System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.43 Nose Wheel Tie Bolt . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.43 Main Wheel Tie Bolt. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.44 Main Wheel Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.45 Green System Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.48 Braking/Steering Control Unit (BSCU) System 1 . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.49 Braking/Steering Control Unit (BSCU) System 2 . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.49 AUTO/BRK Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50 Tachometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50 AUTO/BRK (LO,MED, MAX) pb-sw DECEL light . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.50 AUTO/BRK (LO, MED, MAX) pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.51 Yellow System Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.51 ACCU PRESS Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.52 BRAKES Pressure Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.53
A320/321 30 JUN 12 MEL
MEL/CDL
ITEM
01.00.17 TABLE OF CONTENTS PAGE
ATA 32 - LANDING GEAR (Cont’d)
32-44-04 32-45-01 32-47-01 32-48-01 32-48-02 32-48-03 32-51-01 32-51-02 32-51-03 32-51-04 32-61-01 32-61-02
Alternate Braking Control Unit (ABCU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.53 Parking Brake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.53 Brake Temperature Monitoring Unit (BTMU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.54 Brake Fan System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.54 BRK FAN pb-sw HOT light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.54 BRK FAN pb-sw ON light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.54 Nose Wheel Steering Control System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.55 Rudder PEDALS DISC pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.55 NWS Electrical Deactivation Box . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.56 PARKING BRAKE light on the NWS Electrical Deactivation Box . . . . . . . . . . . . . 01.32.58 LDG GEAR Indicator Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.32.58 DOWN Red Arrow light on the Landing Gear lever . . . . . . . . . . . . . . . . . . . . . . . . 01.32.58 ATA 33 - LIGHTS
33-01-01 33-01-02 33-10-01 33-20-01 33-20-02 33-20-03 33-30-01 33-40-01 33-40-02 33-40-03 33-40-04 33-40-05 33-40-06 33-40-07 33-40-08 33-40-09 33-40-10 33-51-01 33-51-01 33-51-02 33-51-03
ANN LT Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.01 SIGNS Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.01 Cockpit General Illumination (Center & Main Instrument Lighting, . . . . . . . . . . . . . . . . . . . Console and Floor Lighting, Dome lights and Lighting Strips, Instrument . . . . . . . . . . . . . and Panel Integral Lighting, Map Holder Lighting, Center Pedestal Lighting) . . . . 01.33.03 Cabin General Illumination. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.03 Cabin Signs (No Smoking/Fasten Seat Belt/Return to Seat). . . . . . . . . . . . . . . . . 01.33.04 Lavatory Sign (Return to seat) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.05 Cargo and Service Compartment Lighting System . . . . . . . . . . . . . . . . . . . . . . . . 01.33.06 Navigation light System 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.06 Navigation light System 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.06 Landing light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.06 Landing light Extension/Retraction System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.07 Runway Turnoff lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.07 Taxi and Takeoff light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.07 Logo lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.07 Beacon light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.08 Wing Scan lights . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.08 Strobe light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.08 Exit Marking Sign (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.09 Exit Marking Sign (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.09 Exit Location Sign in the Main Aisle. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.09 Overhead Emergency Lighting System in the Main Aisle . . . . . . . . . . . . . . . . . . . 01.33.09
A320/321 01.00.18 TABLE OF CONTENTS
MEL/CDL
ITEM
12 FEB 12 MEL PAGE
ATA 33 - LIGHTS (Cont’d) 33-51-04 33-51-04 33-51-05 33-51-07 33-51-08 33-51-09 33-51-10 33-51-11
Overhead Emergency Lighting System in the Door Vicinity (A320). . . . . . . . . . . . 01.33.10 Overhead Emergency Lighting System in the Door Vicinity (A321). . . . . . . . . . . . 01.33.10 Floor Proximity Emergency Escape Path Marking System in the Main Aisle . . . . 01.33.10 Floor Proximity Emergency Escape Path Marking System Exit Marker . . . . . . . . 01.33.11 Overwing Emergency light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11 Overwing Exit Handle light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11 Escape Slide Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11 Lavatory Auxiliary light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.33.11 ATA 34 - NAVIGATION
34-00-01 34-00-02 34-01-01 34-01-02 34-05-01 34-05-02 34-05-03 34-05-04 34-05-05 34-05-06 34-05-07 34-05-08 34-05-09 34-06-01 34-06-02 34-06-03 34-06-04 34-06-05 34-06-06 34-06-07 34-10-01 34-10-02 34-10-03 34-10-04
ADR (1)(2)(3) MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01 IR MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01 ADIRS Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.01 GPWS Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.04 Actual Airspeed Reference Line and Scale Indication on the PFD . . . . . . . . . . . . 01.34.04 Mach Number Indication on the PFD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.04 VMO/MMO Characteristic Speed Indication on the PFD . . . . . . . . . . . . . . . . . . . . 01.34.05 Altitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.05 Baro Reference Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.05 Vertical Speed in Inertial Mode Indication on the PFD . . . . . . . . . . . . . . . . . . . . . 01.34.05 Other Air Data Related Indications on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06 Attitude Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06 Heading Indication on the PFD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.06 Ground Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07 True Air Speed Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07 Wind Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07 Heading Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07 Position (Aircraft Symbol) Indication on the ND. . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07 Radio Navaids Indications on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.07 Chrono Indication on the ND . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08 ADR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08 ADR 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.08 ADR 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.10 IR 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.11
A320/321 30 JUN 12 MEL
MEL/CDL
ITEM
01.00.19 TABLE OF CONTENTS PAGE
ATA 34 - NAVIGATION (Cont’d) 34-10-05 34-10-07 34-11-01 34-11-02 34-11-03 34-11-04 34-21-05 34-22-01 34-22-02 34-23-01 34-23-02 34-23-03 34-23-04 34-23-05 34-23-06 34-30-04 34-40-01 34-40-02 34-40-03 34-40-04 34-40-05 34-40-06 34-40-07 34-50-01 34-50-03 34-50-04 34-50-05 34-50-06 34-50-09
IR 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.12 IR 3 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.13 Angle of Attack (AOA) Sensor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.14 CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR1 . . . . . . 01.34.15 CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR3 . . . . . . 01.34.16 F/O Total Air Temperature (TAT) Sensor Element Connected to ADR2 . . . . . . . . 01.34.16 Standby ALT Metric Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.17 Standby Compass Indicator. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.18 Standby Compass Lighting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.19 ISIS Baro-Altitude Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.20 ISIS Airspeed Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.20 ISIS Bugs Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.20 ISIS Horizon Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.21 ISIS ILS Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.22 ISIS Mach Number Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.22 Instrument Landing System (ILS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.22 Ground Proximity Warning System (GPWS)/Terrain Awareness . . . . . . . . . . . . . . . . . . . . and Warning System (TAWS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.23 Radio Altimeter Automatic Callout . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.26 Radio Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.26 Traffic Collision Avoidance System (TCAS). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.27 Weather Radar System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.27 Predictive Windshear Detection Function . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.29 PULL UP-GPWS pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.29 ATC . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.29 ADF . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.30 DME . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.30 VOR . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.30 MARKER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.30 Global Positioning System (GPS) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.34.31
A320/321 01.00.20 TABLE OF CONTENTS
MEL/CDL
ITEM
01 MAY 12 MEL PAGE
ATA 35 - OXYGEN 35-01-01 35-07-01 35-07-02 35-10-01 35-10-02 35-10-03 35-20-01 35-20-02 35-20-04 35-20-05 35-30-01 35-30-02
OXYGEN Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.01 Crew OXY High Pressure Indication on the DOOR/OXY SD page . . . . . . . . . . . . 01.35.02 Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page . . . . . . . . . 01.35.03 Crew Oxygen Mask . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.03 Crew Oxygen Mask Microphone . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.03 Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc). . . . . . . . . . . . . 01.35.03 Passenger Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.04 Cabin Attendant Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.05 Galley Oxygen Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.05 Manual Release Tool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.06 Flight Crew Portable Device . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.06 Cabin Attendant Portable Device. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.35.07 ATA 36 - PNEUMATIC
36-00-01 36-01-01 36-01-02 36-01-03 36-01-04 36-07-01 36-07-02 36-07-03 36-07-04 36-07-05 36-07-06 36-11-01 36-11-02 36-11-03 36-11-04 36-11-05
AIR BLEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 ENG BLEED pbsw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 ENG BLEED pbsw OFF light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 APU BLEED pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 APU BLEED pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.01 APU Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . 01.36.02 Engine Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . 01.36.02 Engine Bleed HP Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . 01.36.02 Engine Bleed Precooler Inlet Pressure Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.02 Engine Bleed Precooler Outlet Temperature Indication . . . . . . . . . . . . . . . . . . . . . . . . . . . on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.02 X Bleed Valve Indication on the BLEED SD page . . . . . . . . . . . . . . . . . . . . . . . . 01.36.03 Engine Bleed Air Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.03 Engine Bleed Valve (PRV). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.05 Engine Bleed Overpressure Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.05 Engine Bleed Fan Air Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06 Engine Bleed Air Precooler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06
A320/321 01 MAY 12 MEL
MEL/CDL
01.00.21 TABLE OF CONTENTS
ITEM
PAGE ATA 36 - PNEUMATIC (Cont’d)
36-11-06 36-11-07 36-11-08 36-12-01 36-12-02 36-12-03 36-12-04 36-22-01 36-22-02 36-22-03
Engine Bleed IP Check Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.06 Engine Bleed HP Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.08 Bleed Monitoring Computer (BMC) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.08 APU Bleed Air Supply System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.09 APU Bleed Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.09 APU Bleed Check Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.10 Automatic Control of the X Bleed Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.10 Pylon Leak Detection System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.11 Wing Leak Detection System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.11 APU Leak Detection Loop . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.36.11 ATA 38 - WATER/WASTE
38-10-01 38-30-01
Potable Water Systems . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.38.01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories). . . . . . . . 01.38.01 ATA 46 - INFORMATION
46-11-01 46-21-01 46-21-02 46-21-03
SYSTEMS
Electronic Flight Bag (EFB) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.01 Air Traffic Service Unit (ATSU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.01 Datalink Control and Display Unit (DCDU) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.02 ATC MSG pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.46.02 ATA 47 - INERT GAS SYSTEMS
47-00-01
FUEL INERT MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.47.01 ATA 49 - AIRBORNE AUXILIARY POWER
49-00-01 49-01-01 49-01-02 49-01-03 49-01-04 49-07-01 49-10-01 49-10-02
APU MAINTENANCE Message. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 APU MASTER SW pb-sw FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 APU MASTER SW pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 APU START pb-sw AVAIL light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 APU START pb-sw ON light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.01 Indications on the APU SD Page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.02 Power Plant (APU). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.02 APU Air Intake Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.49.02
A320/321 01.00.22 TABLE OF CONTENTS
MEL/CDL
ITEM
12 FEB 12 MEL PAGE
ATA 52 - DOORS 52-01-01 52-01-02 52-01-03 52-07-01 52-07-01 52-07-02 52-07-02 52-07-03 52-07-04 52-07-05 52-07-06 52-10-01 52-10-02 52-10-03 52-10-04 52-10-05 52-10-06 52-10-07 52-10-08 52-30-01 52-30-02 52-30-03 52-30-04 52-30-05 52-30-06 52-30-07 52-33-01 52-51-01 52-51-02
CKPT DOOR CONT Normal Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.01 CKPT DOOR CONT BK UP Overhead Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.02 CKPT DOOR BK UP Overhead Panel. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.05 Passenger Door Permanently Indicated Open on the DOOR/OXY . . . . . . . . . . . . . . . . . . SD page (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.10 Passenger Door/Emergency Exit Permanently . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Indicated Open on the DOOR/OXY SD page(A321) . . . . . . . . . . . . . . . . . . . . . . . 01.52.14 Passenger Door Permanently Indicated . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Closed on the DOOR/OXY SD page (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.18 Passenger Door/Emergency Exit Permanently Indicated Closed . . . . . . . . . . . . . . . . . . . . on the DOOR/OXY SD page (A321) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.19 Overwing Emergency Exit Permanently Indicated Open on the . . . . . . . . . . . . . . . . . . . . . DOOR/OXY SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.20 Overwing Emergency Exit Permanently Indicated Closed on the . . . . . . . . . . . . . . . . . . . . DOOR/OXY SD page (A320). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.23 Cargo Door Indication on the DOOR/OXY SD page . . . . . . . . . . . . . . . . . . . . . . . 01.52.24 Avionics Compartment Access Door Indication on the . . . . . . . . . . . . . . . . . . . . . . . . . . . . DOOR/OXY SD page. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.25 Cabin Passenger Door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27 Overwing Emergency Exit (A320) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27 Passenger Exit Stop Fitting . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27 Door Damper Function (A320 & A321)). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.27 Door Emergency Opening Function. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28 CHECK DOOR PRESSURE Message on the . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Flight Attendant Panel (FAP) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28 Passenger Door Stay Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.28 CABIN PRESSURE light (on Doors) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29 Cargo Door (FWD, AFT and BULK) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29 Cargo Door Actuator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.29 Cargo Door Electrical Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.30 Cargo Door Locking Hooks and Spools (Rollers) . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.30 Cargo Door Hand Pump . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31 Cargo Door Drift Pin. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31 Cargo Doors Open/Locked Indicator light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.31 Cargo Door Balance Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.32 CDLS Normal System (Normal Control Unit, Switch and Lights on the . . . . . . . . . . . . . . . CKPT DOOR Panel,Buzzer, Keypad) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.32 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on . . . . . . . . . . . . . . . . . the CKPT DOOR BK UP Panel) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.34
A320/321 30 JUN 12 MEL
MEL/CDL
TEM
01.00.23 TABLE OF CONTENTS PAGE
ATA 52 - DOORS (Cont’d) 52-51-03 52-51-04 52-51-05 52-51-06 52-53-01 52-53-02 52-53-03 52-53-04
CDLS Buzzer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.34 CDLS Keypad . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.34 CDLS Keypad Green and Red LEDs. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.35 CDLS Door Release Strike (Catch, Spring, Solenoid, Bolt). . . . . . . . . . . . . . . . . . 01.52.36 COCKPIT DOOR FAULT light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.36 COCKPIT DOOR OPEN light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.37 LOCK Function of the COCKPIT DOOR sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.37 UNLOCK Function of the COCKPIT DOOR sw . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.52.37 ATA 56 - WINDOWS
56-10-01 56-10-02 56-10-03 56-20-01
Front Windshield Note: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.01 Lateral Fixed/Sliding Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.02 Sliding Window Opening/Closing Mechanism . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.03 Cabin Window . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.56.03 ATA 70- ENGINE
70-00-01 70-00-02 70-00-03
ENG FADEC MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.01 ENG EIU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.01 ENG EVMU MAINTENANCE Message . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.70.01 ATA 73- ENGINE FUEL AND CONTROL
73-07-01 73-07-02 73-08-01 73-09-01 73-10-01 73-10-03 73-20-01 73-20-05
F. USED Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.01 Fuel Filter Clog Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . 01.73.01 F. F. (Fuel Flow) Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.01 ENG 1(2) FUEL FILTER CLOG Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.02 Fuel Return Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.02 Fuel Metering Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.02 Flex Takeoff Mode . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.02 Minimum Idle on Ground . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.73.03
A320/321 01.00.24 TABLE OF CONTENTS
MEL/CDL
ITEM
12 FEB 12 MEL PAGE
ATA 74 - IGNITION 74-07-01 74-09-01 74-31-01 74-31-02
Selected Igniter Indication on the ENGINE SD page. . . . . . . . . . . . . . . . . . . . . . . 01.74.01 ENG 1(2) IGN A(B)(A+B) FAULT Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.03 Ignition System A . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.03 Ignition System B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.74.04 ATA 76 - ENGINE CONTROL
76-11-01
Thrust lever Position Sensor. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.76.01 ATA 77 - ENGINE INDICATING
77-07-01 77-07-02 77-08-01 77-08-03 77-08-04 77-08-05
Indications on the CRUISE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.01 Indications on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.02 EGT Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05 F.F. (Fuel Flow) Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05 N1 Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05 N2 Indication on the EWD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.77.05 ATA 78 - ENGINE EXHAUST
78-08-01 78-30-01 78-30-02 78-30-03
REV Indication on the EWD. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01 Thrust Reverser . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.01 Thrust Reverser Inhibition Relay sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.05 Thrust Reverser Shutoff Valve. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.78.05 ATA 79 - ENGINE OIL
79-07-01 79-07-02 79-07-03 79-07-04 79-09-01 79-09-02 79-20-02 79-40-01
CLOG Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.01 Oil Pressure Indication and Advisory on the ENGINE SD page . . . . . . . . . . . . . . 01.79.01 Oil Quantity Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.02 Oil Temperature Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . . . . 01.79.02 ENG 1(2) OIL LO PR Alert. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.02 ENG 1(2) OIL FILTER CLOG Alert . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.03 EMCD Visual Pop- Out Indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.04 Fuel Return Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.79.04
A320/321 MEL/CDL
12 FEB 12 MEL
01.00.25 TABLE OF CONTENTS
ATA 80 - STARTING 80-01-31 80-07-01 80-11-01 80-12-01
ENG MAN START pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.01 Start Valve Position Indication on the ENGINE SD page . . . . . . . . . . . . . . . . . . . 01.80.01 Start Valve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.01 FAULT light on the ENG MASTER Panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.80.02
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A320/321 01.00.26 TABLE OF CONTENTS
MEL/CDL
MEL
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 12 FEB 12 MEL
MEL/CDL
FAA MMEL Preamble The following is applicable for authorized certificate holders operating under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating Rules must be operative. However, the Rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety. A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. The MMEL is the basis for development of individual operator MELs which take into consideration the operator’s particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. An operator’s MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator’s MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of FAR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.
01.01.01 MEL INTRODUCTION
Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained. The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment. The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator prior to further operation. MEL conditions and limitations, do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative. When these requirements are met, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by FAR. Such documentation is required prior to operation with any item of equipment inoperative. Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered. Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures, and schedules to ensure timely repair. WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.
A320/321 MEL/CDL
01.01.02 MEL INTRODUCTION
12 FEB 12 MEL
Definitions 1. System Definitions. System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially. a. “SYSTEM & SEQUENCE NUMBERS - ITEM” (Column 1) means the equipment, system, component, or function listed in the “Item” column. The letters “SV” added at the end of a sequence number indicates that it is a Saudia added item and will not be found in the FAA Master MEL. Where applicable, EICAS/EIS status message(s) are also listed in this column..
2. “Airplane Flight Manual” (AFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office. The FAA approved AFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet. (The AFM will not be carried aboard the aircraft). 3. “Placarding” Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition. placard should be located adjacent to the control or indicator for the item affected, unless otherwise specified, placard wording and location will be determined by the placarding procedures located on section 3 of this manual.
b. “NUMBER INSTALLED” (Column 2) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing the MEL. Should the number be a variable (e.g., passenger cabin items) a number is not required, are a dash() symbol is shown.
4. “-” symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed.
c.
6. “Extended over-water operation” means operation over water at a horizontal distance of more than 50 nautical miles from the nearest shoreline.
“NUMBER REQUIRED FOR DISPATCH” (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met. NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Presidency of Civil Aviation (PCA).
d
“REMARKS OR EXCEPTIONS” (Column 4) this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.
e. A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page.
5. “ER” refers to extended range operations of a twoengine airplane which has a type design approval for ER operations and complies with the provisions of Advisory Circular 120-42A.
7. “Federal Aviation Regulations” (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations. 8. “Flight” for MEL purposes means one operational cycle of the aircraft including only one takeoff and one landing. Where a proviso includes a limitation on the number of flights permitted with an inoperative item, the count will start with the next flight after discovery that the item has become inoperative. 9. “Flight Hours” for MEL purposes means the time from the moment the aircraft leaves the surface of the earth until it touches down at the next point of landing (i.e., takeoff to landing time). “Flight Hours” is identical to “time in service,” as defined by GACA/FAR Part 1. Where a proviso includes a limitation on the number of flight hours permitted with an inoperative item, the time will start at the next takeoff after discovery that the item has become inoperative. 10. “Flight Day” means a 24 hour period (from midnight to midnight) Universal Coordinated Time (UCT), during which at least one flight is initiated for the affected aircraft.
A320/321 MEL/CDL
12 FEB 12 MEL
Definitions
(Cont’d)
11. “Icing Conditions” means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s). 12. “Inoperative” means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s). 13. “NOTES:” in Column 4 provides additional information for crewmember or maintenance consideration. Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements. 14. “Inoperative components of an inoperative system”: Inoperative items which are components of a system which is inoperative are usually considered components directly associated with and having no other function than to support that system. (Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MEL). 15. “(M)” symbol indicates a requirement for a specific maintenance procedure which must be accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of Technical Services. Appropriate procedures are required to be published as part of Technical Services manuals or MEL. 16. “(O)” symbol indicates a requirement for a specific operations procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew; however, other personnel may be qualified and authorized to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of Flight Operations. Appropriate procedures are required to be published as a part of Flight Operations manuals or MEL.
NOTES:
01.01.03 MEL INTRODUCTION
The (M) and (O) symbols are required in Saudi Arabian AirLines MEL unless otherwise authorized by the GACA. 17. “Deactivated” and “Secured” means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by Technical Services. 18. “Visual Flight Rules” (VFR) is as defined in FAR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan. 19. “Visual Meteorological Conditions” (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight. This does not preclude operating under Instrument Flight Rules. 20. “Visible Moisture” means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow. 21. “Passenger Convenience Items” , Deleted, See NEF 32. 22. “Non-combustible materials” means metallic objects that will not sustain a fire. 23. “ R epai r ” and “ R epl acement ” r e f e r t o s u c h maintenance action as necessary to restore an inoperative item to an operative condition. 24. “Crewmember “ means a person assigned to perform duty in an aircraft during flight time. 25. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators: Category A. Items in this category shall be repaired within the time interval specified in the remarks column of the operator’s approved MEL. Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the
Definitions
(Cont’d)
A320/321 01.01.04 MEL INTRODUCTION
MEL/CDL
malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 1000 UCT on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th. Category C. Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 1000 UCT on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th. Category D. Items in this category shall be repaired within one hundred twenty (120) consecutive calendar days (2880 hours), excluding the day t he malfunction was recorded in the aircraft maintenance record/logbook. The letter designators are inserted adjacent to Column 2. 26. Electronic Fault Alerting System - General New generation aircraft display system fault indications to the flight crew by use of computerized display systems. Each aircraft manufacturer has incorporated individual design philosophies in determining the data that would be represented. The following customized definition may be used to help determine the level of messages affecting the aircraft’s dispatch status. a. AIRBUS (A320, A321, A330) Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide different levels of system condition messages (WARNING, CAUTION, STATUS and ADVISORY). A-320/321 and A-330 also provide MAINTENANCE status messages. Any message that affects airplane distpatchability will normally be at the WARNING, CAUTION or STATUS level. MAINTENANCE messages (A320/321 and A-330 only) are also indicated on ECAM Status Page below the white Maintenance label.
12 FEB 12 MEL A MAINTENANCE status (Class II) message on ECAM indicates the presence of a system fault which can be identified by CFDS (A-320/321) or CMS (A-330) interrogation. The systems are designed to be fault tolerant; however for any MAINTENANCE status (ClassII) message the A3120/321 MEL must be verified for dispatch capability. For the A-330, MAINTENANCE status messages do not affect dispatch. b. BOEING (B-747-468, B-777) Boeing aircraft equipped with Engine Indicating and Crew Alerting Systems (EICAS), provide different priority levels of system messages (WARNING, C AU T I O N , AD VI SO R Y, ST AT US a n d MAINTENANCE). Any messages that affects aircraft dispatch status will be displayed as a STATUS message level or higher. The absence of an EICAS STATUS or higher level (WARNING, CAUTION, ADVISORY) message indicates that the system/component is operating within its approved operating limits or tolerances. System conditions that result only in a maintenance level message, i.e., no correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program. c. DOUGLAS (MD-11, MD-90) Some Douglas aircraft are equipped with an alerting function which is a subsystem within the Electronic Instrument System (EIS). The alerting function provides various levels of system condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and STATUS). Alerts that affect aircraft dispatch will include W AR N I N G , C AU T I O N , ST AT US or MAINTENANCE level. MAINTENANCE alerts are displayed on the status page of the EIS display panel under the maintenance heading. A MAINTENANCE alert on the EIS indicates the presence of a system fault which can be identified by the Central Fault Display System (CFDS for MD11), or Engine and Alert Display (EAD for MD-90) interrogation. The systems are designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be verified for dispatch purposes.
Definitions
(Cont’d)
A320/321 12 FEB 12 MEL
MEL/CDL
d. EMBRAER ( ERJ-170) The ERJ-170 are equipped with an Engine indicating and crew alerting system (EICAS) that provides three different message levels : WARNING,CAUTION, and ADVISORY. The ERJ 170 SERIES and STATUS messages. Failures that effect dispatchability are presented to the flight crew at one of these levels.other failures may be presentes only to the maintenance personnel on the multi function display (MFD) maintenance pages or through the download of the Central Maintenance Computer (CMC). 26. System conditions that result only in a maintenance level message, I.e. No correlation with a higher level EICAS message, do not affect dispatch and do not require action other than as addressed within an operator’s standard maintenance program. 27. “Day of Discovery” is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and/or record. This day is excluded from the calendar days or flight days specified in the MEL for the repair of an inoperative item of equipment. This provision is applicable to all MEL items, i.e., categories “A, B, C, and D.” 28. “Operative” or “Operates normally” - When the MEL specifies that an item of equipment is operative or that it operates normally, it means that the system and/or component will accomplish its intended purpose and is consistently functioning normally within its design operating limit(s) and tolerance(s). It does not mean that its operational status must be verified; it is to be considered operative unless reported or is known to be malfunctioning. 29. “Must be verified operative” or “Must be verified to operate normally”- When the MEL specifies that an item of equipment must be verified operative, it means that it must be checked and confirmed operative at the interval(s) specified for the item. When the MEL specifies that an item of equipment must be verified operative, but no interval is specified, verification is required only at the time of deferral. 30. A “(FD)” symbol indicates a requirement for the technical personnel to notify flight dispatch as soon as a relevant MEL item becomes open on the hold item list and must be shown on the flight dispatch release, or an amendment made. Such items normally involve
01.01.05 MEL INTRODUCTION restrictions associated with flight level, speed, weight, etc.
31. “Considered inoperative”,as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the repaircategory. 32. Nonessential equipment and furnishings (NEF) are those items installed on the aircraft as part of the original certification,supplemental type certificate, or engineering order that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules. They are those item that if inoperative, damaged or missing have no effect on the aircraft’s ability to be operated safely under all operational conditions.
Weight Reductions The MEL weight reductions must be applied to the maximum performance limited weights, as follows: 1. Takeoff -
Weight penalty is applied to the most restrective of the Zero Wind weight or Climb Limit weight.
2. Enroute -
Weight penalty is applied to cruise and one engi ne i nopera t iv e A lt it u d e Capability limited weights.
3. Landing -
Weight penalty is applied to the most restrective of tailored landing charts, field length or landing climb limited weight.
Dispatch Fuel Penalty The percentage increase in the fuel must be applied to the minimum dispatch fuel requirement. Minimum dispatch fuel required is the sum of trip fuel, alternate fuel and reserve fuel. *
*
*
A320/321 01.01.06 MEL INTRODUCTION
MEL/CDL
THIS PAGE INTENTIONALLY LEFT BLANK
MEL
A320/321 MEL/CDL
12 FEB 12 MEL
01.02.01 GENERAL
ECAM WARNINGS / MEL ENTRY The following pages give correspondence between ACAM caution/warning messages and MEL item number: CAUTION 1) This section is, normally, not intended to cover false cautions/warnings. However, if a caution/warning is determined to be false by troubleshooting, the crew should refer to the concerned caution/warning message item (if listed) in the associated ATA chapter 01.
2) In order to help the crew to determine the MEL ENTRY point corresponding to a caution/warning message, the REMARK column contains the text: a) “Actual warning” or “Actual caution”. The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions corresponding to an actual failure of the system/ component monitored by the caution/warning. b) “False warning” or “False caution”. The associated MEL item number is the MEL ENTRY point which gives the dispatch conditions corresponding to the failure of the warning, determined by troubleshooting. The system/component monitored by the caution/warning being still operative.
3) When the REMARK column contains neither, “Actual caution/warning”, nor “False caution/warning” textes, the MEL ENTRY point corresponds to an actual warning which indicates an actual failure of the system/component monitored by the caution/warning. 4) When either an actual, or a false caution/warning is activated, this section gives the MEL ENTRY point to be considered. But the crew MUST CHECK THAT THE AIRCRAFT SYSTEMS/COMPONENTS ARE IN A CONDITION WHCIH COMPLIES WITH THE DISPTACH CONDITIONS. IF NOT, AIRCRAFT DISPATCH IS NOT ALLOWED. 5) When a caution/warning is associated with the wording “Not applicable” in the Display Condition column, this means that the MEL is not appropriate document to be consulted. When such caution/warnins have been triggered, application of associated procedure, if any , (refer to FCOM Abnormal/Emergency procedures), and/or accomplishment of maintenance action, if required, would permit to fix the problem.
( Cont'd on next page )
A320/321 MEL/CDL
01.02.02 GENERAL
12 FEB 12 MEL
ECAM WARNINGS / MEL ENTRY ( Cont'd )
ECAM The A320/321 Family aircraft is equipped with Electronic Centralized Aircraft Monitoring (ECAM) which provides different levels of aircraft systems monitoring messages: - ECAM warning.
- ECAM advisory.
- ECAM caution.
-ECAM memo.
ECAM warning and ECAM caution messages are listed in the “MEL Entries” section. ECAM advisory and ECAM memo messages are not listed in the “MEL Entries” section. CONDITION OF DISPATCH COLUMN - NO DISPATCH: It is not permitted to dispatch the aircraft when the ECAM displays this alert. - NOT APPLICABLE: The ECAM alert does not report a system failure and is not related to MEL. The MEL shall not be used. This is not a NO-GO situation. The corrective action to revert to normal condition is immediate, obvious or well known by flight crew and/or maintenance personnel. EXAMPLES 1) If the “BAT FAULT” caution message is displayed on ECAM, the crew must refer to MEL 24-30-02 (Battery channel). 2) If the “ac bus 1 fault fault” CAUTION MESSAGE IS DISPLAYED ON ecam, a/c DISPATCH IS NOT ALLOWED. 3) If the “GEN 1 OFF” caution message is displayed on ECAM no MEL entry is required, and the text “Not applicable” is written in the Remark column. In this example, the crew must switch on the generator pb sw. 4) If ”PACK 1 + 2 FAULT” caution message is displayed the crew must refer to FCOM for “FLIGHT WITHOUT PRESURIZATION”. Note : The ECAM warnings and cautions listed in section 00E in the column “ECAM WARNINGS” are generic. *example : ECAM WARNING FCU 1(2) (1 + 2) FAULT
DISPATCH CONDITION
REMARK
Refer to MEL 22-81-01
Wording FCU 1(2) (1 + 2) FAULT represents the three messages ; “FCU 1 FAULT” “FCU 2 FAULT” “FCU 1 + 2 FAULT”. *
*
*
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.01 ECAM MESSAGES
ATA 21 AIR CONDITIONING ECAM WARNING
ACTION
DISPATCH CONDITION
AIR AFT CRG VENT FAULT
Refer to MEL 21-28-03
COND CTL 1(2)-A(B)
Refer to MEL 21-63-04
PACK 1(2) FAULT
Refer to MEL 21-52-01
PACK 1+ 2 FAULT
Refer to FCOM/PRO-SPO-20
PACK 1(2) OFF
Refer to MEL 21-52-01
PACK 1(2) OVHT
Refer to MEL 21-52-01
PACK 1 (2) REGUL FAULT
Refer to MEL 21-27-01-01
If pack outlet temperature is affected
Refer to MEL 21-07-01-03
If pack compressor outlet temperature is affected
Refer to MEL 21-51-03
If pack flow sensor is affected
Refer to MEL 21-52-01
If pack flow control valve is affected
Refer to MEL 21-52-02
If pack ram air inlet is affected
Refer to MEL 21-61-01
If turbine bypass valve affected
CAB PR EXCESS CAB ALT
Not applicable
EXCESS RESIDUAL PR
Apply ECAM procedure
LDG ELEV FAULT
Refer to MEL 21-31-04
LO DIFF PR
Not applicable
OFV NOT OPEN
NO DISPATCH
SAFETY VALVE OPEN
Refer to FCOM/PRO-SPO-20
Actual alert
Refer to MEL 21-09-03
False alert
SYS 1(2) FAULT
Refer to MEL 21-31-01
SYS 1+2 FAULT
Refer to FCOM/PRO-SPO-20
A320/A321 01.03.02 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 21 AIR CONDITIONING ECAM WARNING
ACTION
DISPATCH CONDITION
COND AFT CAB DUCT OVHT
Refer to MEL 21-63-02
AFT CARGO DUCT OVHT
Refer to MEL 21-43-02
AFT CRG HEAT FAULT
Refer to MEL 21-43-02
AFT CRG ISOL VALVE
Refer to MEL 21-28-04
CKPT DUCT OVHT
Refer to MEL 21-63-02
FWD CAB DUCT OVHT
Refer to MEL 21-63-02
HOT AIR FAULT
Refer to MEL 21-63-03
L + R CAB FAN FAULT
NO DISPATCH
LAV + GALLEY FAN FAULT
Refer to MEL 21-23-01
TRIM AIR SYS FAULT
Not applicable
If the trim air valves are colsed
Refer to MEL 21-63-02
If the associated AFT CAB TRIM VALVE message is displayed
Refer to MEL 21-63-02
If the associated FWD CAB TRIM VALVE message is displayed
Refer to MEL 21-63-02
If the associated CKPT TRIM VALVE message is displayed
Refer to MEL 21-63-02
If the associated TRIM AIR HI PR message is displayed
Refer to MEL 21-26-04
If the VENT SKIN VALVE FAULT alert is displayed on the EWD.
Refer to MEL 21-26-05
If the VENT SKIN VALVE FAULT alert is displayed on the EWD.
VENT AVNCS SYS FAULT
Refer to MEL 21-26-03, or Refer to MEL 21-26-08, or Refer to MEL 21-26-06, or Refer to MEL 21-26-10
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.03 ECAM MESSAGES
ATA 21 AIR CONDITIONING ECAM WARNING
ACTION
DISPATCH CONDITION
VENT BLOWER FAULT
Refer to MEL 21-26-01 Refer to MEL 21-09-01
Actual caution False caution
EXTRACT FAULT
Refer to MEL 21-26-02
Actual caution
Refer to MEL 21-09-02
False caution
Refer to MEL 21-26-04
Faulty valve determined on the CAB PRESS page
SKIN VALVE FAULT
Refer to MEL 21-26-05 ATA 22 AUTO FLIGHT ECAM WARNING
ACTION
DISPATCH CONDITION
AUTO FLT A/THR LIMITED
Not applicable
A/THR OFF
Refer to MEL 22-30-01
Actual caution
Refer to MEL 22-30-03
False caution
Refer to MEL 22-10-01
Actual warning
Refer to MEL 22-10-06
False warning
AP OFF FAC 1 FAULT
Refer to MEL 22-60-01
FAC 2 FAULT
Refer to MEL 22-60-02
FAC 1 + 2 FAULT
NO DISPATCH
FCU 1 (2) FAULT
Refer to MEL 22-81-03-01
FCU 1 + 2 FAULT
NO DISPATCH
REAC W/S DET FAULT (if installed)
Refer to MEL 22-60-03
RUD TRIM 1 (2) FAULT
Refer to MEL 27-22-01
RUD TRIM SYS
NO DISPATCH
A320/A321 01.03.04 EICAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 22 AUTO FLIGHT ECAM WARNING
ACTION
DISPATCH CONDITION
AUTO FLT RUD TRV LIM 1 (2)
Refer to MEL 27-23-01
RUD TRV LIM SYS
NO DISPATCH
YAW DAMPER 1 (2)
Refer to MEL 22-60-04
YAW DAMPER SYS
NO DISPATCH
WINDSHEAR DET FAULT
Refer to MEL 22-60-03 ATA 23 COMMUNICATIONS
ECAM WARNING
ACTION
DISPATCH CONDITION
COM ACARS FAULT (If installed)
Refer to MEL 46-21-01
CIDS 1 + 2 FAULT
NO DISPATCH
HF 1 (2) DATA FAULT (If installed)
Refer to MEL 23-10-01
HF 1 (2) EMITTING (If installed)
Refer to MEL 23-51-03
If hand microphone selector is jammed in the transmitting position
Refer to MEL 23-51-06
If side stick radio selector is jammed in the transmitting position
Refer to MEL 23-52-05
If a transmission Key on one ACP is jammed in the transmitting position.
Refer to MEL 23-09-01
False alert
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.05 ECAM MESSAGES
ATA 23 COMMUNICATIONS ECAM WARNING
ACTION
DISPATCH CONDITION
COM SATCOM DATA FAULT (If installed)
Refer to MEL 23-10-03, and Refer to MEL 23-20-02
SATCOM FAULT (If installed)
Refer to MEL 23-10-03, and Refer to MEL 23-20-02
VHF 3 DATA FAULT
Refer to MEL 23-10-02
VHF 1(2)(3) EMITTING
Refer to MEL 23-51-03,
If hand microphone selector is jammed in the transmitting position
Refer to MEL 23-51-06
If side stick radio selector is jammed in the transmitting position
Refer to MEL 23-52-05
If a transmission Key on one ACP is jammed in the transmitting position False caution
Refer to MEL 23-09-02
ATA 24 ELECTRICAL POWER ECAM WARNING
ACTION
DISPATCH CONDITION
C/B TRIPPED
Refer to affected systems
Actual alert
Refer to MEL 24-09-02
False alert
A320/A321 01.03.06 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 24 ELECTRICAL POWER ECAM WARNING
ACTION
DISPATCH CONDITION
ELEC AC BUS 1 FAULT
NO DISPATCH
AC BUS 2 FAULT
NO DISPATCH
AC ESS BUS ALTN
NO DISPATCH
AC ESS BUS FAULT
NO DISPATCH
AC ESS BUS SHED
NO DISPATCH
Actual caution
Refer to MEL 24-09-01
False caution
APU GEN FAULT
Refer to MEL 24-23-01
BAT 1(2) FAULT
NO DISPATCH
BAT 1 (2) OFF
Not applicable
BCL 1 (2) FAULT
Refer to MEL 24-38-02
DC BAT BUS FAULT
NO DISPATCH
DC BUS 1 + 2 FAULT
NO DISPATCH
DC BUS 1 FAULT
NO DISPATCH
DC BUS 2 FAULT
NO DISPATCH
DC EMER CONFIG
NO DISPATCH
DC ESS BUS FAULT
NO DISPATCH
DC ESS BUS SHED
NO DISPATCH
EMER CONFIG
NO DISPATCH
EMER GEN 1 LINE OFF
Not applicable
ESS BUSSES ON BAT
NO DISPATCH
ESS TR FAULT
Refer to MEL 24-34-01
GEN 1 (2) FAULT
Refer to MEL 24-22-01
GEN 1 (2) OFF
Not applicable
GEN 1 (2) (APU GEN) OVERLOAD
Refer to MEL 24-26-01
IDG DISCONNECTED
Refer to MEL 24-22-01
IDG 1 (2) OIL LO PR
Refer to MEL 24-22-01
IDG 1 (2) OIL OVHT
Refer to MEL 24-22-01
STATIC INV FAULT
NO DISPATCH
TR 1 (2) FAULT
Refer to MEL 24-32-01
Actual caution
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.07 ECAM MESSAGES
ATA 26 FIRE PROTECTION ECAM WARNING APU FIRE
ACTION
DISPATCH CONDITION
NO DISPATCH
Actual alert
Refer to MEL 49-10-01
False alert
APU FIRE DET FAULT
Refer to MEL 26-13-01, and Refer to MEL 26-13-02
FIRE LOOP A(B) FAULT AVIONICS SMOKE
ENG 1(2)FIRE
Refer to MEL 26-13-01
If loop A is failed
Refer to MEL 26-13-02
If loop B is failed
NO DISPATCHr
Actual alert
Refer to MEL 26-15-01
False alert
NO DISPATCH
ENG 1(2) FIRE DET FAULT
NO DISPATCH
FIRE LOOP A FAULT
Refer to MEL 26-12-01
If engine 1 is affected
Refer to MEL 26-12-02
If engine 2 is affected
Refer to MEL 26-12-03
If engine 1 is affected
Refer to MEL 26-12-04
If engine 2 is affected
NO DISPATCH
Actaual alert
Refer to MEL 26-16-02
False alert
Refer to MEL 26-23-02
If the SMOKE FWD CRG BTL FAULT alert is not displayed on the EWD
Refer to MEL 26-23-01
If the SMOKE FWD CRG BTL FAULT alert is displayed on the EWD
FIRE LOOP B FAULT SMOKE AFT CARGO SMOKE AFT CRG BTL FAULT
AFT CRG DET FAULT
Refer to MEL 26-16-02
A320/A321 01.03.08 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 26 FIRE PROTECTION ECAM WARNING
ACTION
DISPATCH CONDITION
NO DISPATCH
Actual alert
Refer to MEL 26-16-01
False alert
Refer to MEL 26-23-02
If the SMOKE AFT CRG BTL FAULT alert is not displayed on the EWD
Refer to MEL 26-23-01
If the SMOKE AFT CRG BTL FAULT alert is displayed on the EWD
SMOKE FWD CARGO SMOKE FWD CRG BTL FAULT
FWD CRG DET FAULT
Refer to MEL 26-16-01
DET FAULT
Refer to MEL 23-73-10-01
LAVATORY DET FAULT
Refer to MEL 26-17-01
LAVATORY SMOKE
NO DISPATCH
Actual alert
Refer to MEL 26-17-01
False alert
ATA 27 FLIGHT CONTROLS ECAM WARNING
ACTION
CONFIG L(R) SIDESTICK FAULT
NO DISPATCH
PITCH TRIM NOT IN T.O. RANGE
NO DISPATCH
RUD TRIM NOT IN T.O. RANGE
NO DISPATCH
SLATS (FLAPS) NOT IN T.O. CONFIG
NO DISPATCH
SPEED BRK NOT RETRACTED
NO DISPATCH
DISPATCH CONDITION
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.09 ECAM MESSAGES
ATA 27 FLIGHT CONTROLS ECAM WARNING
ACTION
DISPATCH CONDITION
F/CTL AIL SERVO FAULT
Refer to MEL 27-14-01, or Refer to MEL 27-14-02, or Refer to MEL 27-14-03, or Refer to MEL 27-14-04
ALTN LAW
NO DISPATCH
DIRECT LAW
NO DISPATCH
ELAC 1 FAULT
Refer to MEL 27-93-01
ELAC 1 PITCH FAULT
Refer to MEL 27-93-01
ELAC 2 FAULT
NO DISPATCH
ELAC 2 PITCH FAULT
NO DISPATCH
ELEV SERVO FAULT
NO DISPATCH
If servocontrol is affected
Refer to MEL 27-34-02
If servocontrol position transducer is affected
FCDC 1 FAULT
NO DISPATCH
FCDC 2 FAULT
Refer to MEL 27-95-02
FCDC 1+2 FAULT
NO DISPATCH
FLAP ATTACH SENSOR
NO DISPATCH
FLAP LVR NOT ZERO
Not applicable
FLAP SYS 1 FAULT
NO DISPATCH Refer to MEL 27-54-01
FLAP SYS 2 FAULT
If the maintenance confirms that the F/CTL FLAP SYS 1 FAULT alert is displayed on the EWD due to a flap motor failure
Refer to MEL 27-51-01 Refer to MEL 27-54-01
FLAP TIP BRK FAULT
Refer to MEL 27-51-03
FLAPS (SLATS) FAULT
NO DISPATCH
If the maintenance confirms that the FTCL FLAP SYS 2 FAULT alert is displayed on the EWD due to a flap motor failure.
A320/A321 01.03.10 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 27 FLIGHT CONTROLS ECAM WARNING
ACTION
DISPATCH CONDITION
F/CTL FLAPS (SLATS) LOCKED
NO DISPATCH
GND SPLR FAULT
Refer to MEL 32-42-06
If the braking system is affected
Refer to MEL 27-92-02
If the braking system is not affected
GND SPLR (1 + 2)(3 + 4) FAULT
Refer to MEL 27-92-02
L(R) AIL FAULT
NO DISPATCH
L(R) ELEV FAULT
NO DISPATCH
L + R ELEV FAULT
NO DISPATCH
L(R) SIDESTICK FAULT
NO DISPATCH
SEC 1 FAULT
Refer to MEL 27-94-01
SEC 2 FAULT
Refer to MEL 27-94-02
SEC 3 FAULT
Refer to MEL 27-94-03
SIDESTICK PRIORITY
Refer to FCOM/PRO-ABN-27
SLAT SYS 1 FAULT
NO DISPATCH Refer to MEL 27-84-01
SLAT SYS 2 FAULT
If the maintenance confirms the F/CTL SLAT SYS 1 FAULT alert is displayed on the EWD due to a slat motor failure.
Refer to MEL 27-51-02 Refer to MEL 27-84-01
SLAT TIP BRK FAULT
Refer to MEL 27-81-01
SPD BRK DISAGREE
Refer to MEL 27-92-01
SPD BRK FAULT
Refer to MEL 27-92-01
SPD BRK STILL OUT
Not applicable
SPD BRK 2(3 + 4) FAULT
Refer to MEL 27-92-01
If the maintenance confirms the F/CTL SLAT SYS 2 FAULT alert is displayed on the EWD due to a slat motor failure.
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.11 ECAM MESSAGES
ATA 27 FLIGHT CONTROLS ECAM WARNING
ACTION
DISPATCH CONDITION
F/CTL SPLR FAULT
Refer to MEL 27-64-01, Refer to MEL 27-64-02, Refer to MEL 27-64-03, Refer to MEL 27-64-04, or Refer to MEL 27-64-05
STABILIZER JAM
NO DISPTACH ATA 28 FUEL
ECAM WARNING
ACTION
DISPATCH CONDITION
FUEL ACT PUMP LO PR
Refer to MEL 28-28-03
ACT UNUSABLE
Not applicable
ACT XFR FAULT
Refer to MEL 28-12-05, or
Actual alert
Refer to MEL 28-46-02, or Refer to MEL 28-28-01, or Refer to MEL 28-28-02, or Refer to MEL 28-28-04, or Refer to MEL 28-28-05, or Refer to MEL 28-28-06, or Refer to MEL 28-28-09, or Refer to MEL 28-46-05 Refer to MEL 28-09-03 APU LP VALVE FAULT
Refer to MEL 28-29-01
AUTO FEED FAULT
Refer to MEL 28-20-01
AUTO TRANSFER FAULT
Refer to MEL 28-26-01
False alert
A320/A321 01.03.12 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 28 FUEL ECAM WARNING
ACTION
DISPATCH CONDITION
FUEL CTR TK PUMP 1(2) LO PR
Refer to MEL 28-21-02
CTR TK PUMPS LO PR
Refer to MEL 28-21-02
CTR TK PUMPS OFF
Not applicable
CTR TK XFR OFF
Not applicable
ENG 1(2) LP VALVE OPEN
Refer to MEL 28-24-01
FQI CH 1(2) FAULT
Refer to MEL 28-50-01
F.USED/FOB DISAGREE
Not applicable
L(R) INNER (OUTER) TK HI TEMP
Disptach possible only if “delay T.O.” is not displayed on ECAM
Actual alert
Refer to MEL 28-09-01
False alert
Disptach possible only if “delay T.O.” is not displayed on ECAM
Actual alert
Refer to MEL 28-09-01
False alert
NO DISPATCH
Actual alert
Refer to MEL 28-09-02
False alert
NO DISPATCH
Actual alert
Refer to MEL 28-09-02
False alert
L(R) WING TK HI TEMP
L(R) INNER (OUTER) TK LO TEMP L(R) WING TK LO TEMP L(R) TK PUMP 1(2) LO PR
Refer to MEL 28-21-01
L(R) TK PUMP 1 + 2 LO PR
NO DISPATCH
L(R) WING TK LO LVL
NO DISPATCH
Actual alert
Refer to MEL 28-46-04
False alert
L+R WING TK LO LVL
NO DISPATCH
L(R) WING TK OVERFLOW
NO DISPATCH
L(R) XFR VALVE CLOSED or OPEN
Refer to MEL 28-15-01, or Refer to MEL 28-15-02
L(R) XFR VALVE FAULT
Refer to MEL 28-21-02
X FEED VALVE FAULT
NO DISPATCH
XFR VALVES FAULT
Refer to MEL 28-21-02
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.13 ECAM MESSAGES
ATA 29 HYDRAULIC POWER ECAM WARNING
ACTION
DISPATCH CONDITION
HYD B ELEC PUMP LO PR B ELEC PUMP OVHT B RSVR LO AIR PR B RSVR LO LVL B RSVR OVHT B SYS LO PR B + G SYS LO PR B + Y SYS LO PR G ENG 1 PUMP LO PR G RSVR LO AIR PR G RSVR LO LVL G RSVR OVHT G SYS LO PR G + Y SYS LO PR
NO DISPATCH
Actual caution
Refer to MEL 29-09-01
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-02
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-04
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-05
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-06
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-09
False caution
NO DISPATCH
Actual warning
Refer to MEL 29-09-09
False warning
NO DISPATCH
Actual warning
Refer to MEL 29-09-09
False warning
NO DISPATCH
Actual caution
Refer to MEL 29-09-03
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-04
False caution
NO DISPATCH
Actual alert
Refer to MEL 29-09-05
False alert
NO DISPATCH
Actual caution
Refer to MEL 29-09-06
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-09
False caution
NO DISPATCH
Actual warning
Refer to MEL 29-09-09
False warning
A320/A321 01.03.14 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 29 HYDRAULIC POWER ECAM WARNING
ACTION
DISPATCH CONDITION
NO DISPATCH
Actual caution
Refer to MEL 29-09-07
False caution
NO DISPTACH
Actual caution
Refer to MEL 29-09-08
False caution
Refer to MEL 29-24-01
Actual caution
Refer to MEL 29-09-01
False caution
Refer to MEL 29-24-01
Actual alert
Refer to MEL 29-09-02
False alert
NO DISPATCH
Actual caution
Refer to MEL 29-09-03
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-04
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-05
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-06
False caution
NO DISPATCH
Actual caution
Refer to MEL 29-09-09
False caution
HYD PTU FAULT RAT FAULT Y ELEC PUMP LO PR Y ELEC PUMP OVHT Y ENG 2 PUMP LO PR Y RSVR LO AIR PR Y RSVR LO LVL Y RSVR OVHT Y SYS LO PR
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.15 ECAM MESSAGES
ATA 30 ICE AND RAIN PROTECTION ECAM WARNING
ACTION
DISPATCH CONDITION
ANTI ICE ALL PITOT
NO DISPATCH
CAPT (F/O) (STBY) AOA
Refer to MEL 30-31-04
CAPT (F/0) (STBY) L(R) STAT
Refer to MEL 30-31-03
CAPT (F/O) (STBY) PITOT
Refer to MEL 30-31-02
CAPT + F/O PITOT
NO DISPATCH
CAPT + STBY PITOT
NO DISPATCH
CAPT (F/O) (STBY) PROBES
Refer to MEL 30-31-01
CAPT (F/O) TAT
Refer to MEL 30-31-05
DETECT FAULT
Refer to MEL 30-81-01
ENG 1(2) VALVE CLSD or OPEN
Refer to MEL 30-21-01
F/O + STBY PITOT
NO DISPATCH
ICE DETECTED
Not applicable
L(R) WINDOW
Refer to MEL 30-42-01
If Window Heat Computer affected
Refer to MEL 30-42-02 L(R) WINSHIELD
Refer to MEL 30-42-01 Refer to MEL 30-42-03
L + R WINSHIELD
NO DISPATCH
SEVERE ICE DETECTED
Not applicable
WING ANTI ICE L(R) HI PR
Refer to MEL 30-11-01B
L(R) VALVE OPEN
Refer to MEL 30-11-01
OPEN ON GND
Refer to MEL 30-11-01
SYS FAULT
Refer to MEL 30-11-01
If Window Heat Computer affected
A320/A321 01.03.16 EICAS MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 31 INDICATING/RECORDING SYSTEMS ECAM WARNING
ACTION
EIS DMC 1 FAULT
Refer to MEL 31-62-01
DMC 2 FAULT
Refer to MEL 31-62-02
DMC 3 FAULT
Refer to MEL 31-62-03
FWS FWC 1 FAULT
NO DISPATCH
FWC 2 FAULT
Refer to MEL 31-53-01
FWC 1 + 2 FAULT
NO DISPATCH
OEB/FWC DISCREPANCY
NO DISPATCH
SDAC 1 FAULT
NO DISPATCH
SDAC 2 FAULT
Refer to MEL 31-55-01
SDAC 1 + 2 FAULT
NO DISPATCH
RECORDER DFDR FAULT
Refer to MEL 31-30-03
SYS FAULT
Refer to MEL 31-30-05
DISPATCH CONDITION
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.17 ECAM MESSAGES
ATA 32 LANDING GEAR ECAM WARNING
ACTION
DISPATCH CONDITION
BRAKES ALTN BRK FAULT
NO DISPATCH
ALTN L(R) RELEASED
NO DISPATCH
A/SKID N/WS FAULT
NO DISPATCH
A/SKID N/WS OFF
Not applicable
AUTO BRK FAULT
Refer to MEL 32-42-05
BRK Y ACCU LO PR
NO DISPATCH
Actual caution
Refer to MEL 32-44-02
False caution
SYS 1 FAULT
Refer to MEL 32-42-03
SYS 2 FAULT
Refer to MEL 32-42-04
HOT
NO DISPATCH
Actual caution
Refer to MEL 32-07-01
False caution
NORM BRK FAULT
NO DISPATCH
NORM + ALT FAULT
NO DISPATCH
PARK BRK ON
Not applicable
RELEASED
Refer to MEL 32-42-02
If green brake supply affected
Refer to MEL 32-42-06
If a tachometer affected
BRAKES-N/WS MINOR FAULT
Refer to MEL 32-09-01
CONFIG PARK BRK ON
NO DISPATCH
L/G DOORS NOT CLOSED
NO DISPATCH
GEAR NOT DOWN
Not applicable
GEAR NOT DOWNLOCKED
Not applicable
GEAR NOT UPLOCKED
Not applicable
GEAR UPLOCK FAULT
Refer to MEL 32-31-02
A320/A321 01.03.18 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 32 LANDING GEAR ECAM WARNING
ACTION
DISPATCH CONDITION
L/G LGCIU 1 FAULT
NO DISPATCH
LGCIU 2 FAULT
Refer to MEL 32-31-01
If the LGCIU 2 is inoperative
Refer to MEL 32-32-02, or
If a RH L/G proximity detector associated with the LGCIU 2 is inoperative: apply the relevant item
Refer to MEL 32-32-05, or Refer to MEL 32-32-08, or Refer to MEL 32-32-11, or Refer to MEL 32-32-14 Refer to MEL 32-32-03, or
If a LH L/G proximity detector associated with the LGCIU 2 is inoperative: apply the relevant item
Refer to MEL 32-32-06, or Refer to MEL 32-32-09, or Refer to MEL 32-32-12, or Refer to MEL 32-32-15 Refer to MEL 32-32-04, or
Refer to MEL 32-32-07, or Refer to MEL 32-32-10, or Refer to MEL 32-32-13, or Refer to MEL 32-32-16 SHOCK ABSORBER FAULT
NO DISPATCH
SYS DISAGREE
NO DISPATCH
If a Nose L/G proximity detector associated with the LGCIU 2 is inoperative: apply the relevant item
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.19 ECAM MESSAGES
ATA 32 LANDING GEAR ECAM WARNING
ACTION
DISPATCH CONDITION
WHEEL HYD SEL FAULT
NO DISPATCH
N/W STRG FAULT
Refer to MEL 32-51-01
TYRE LO PR
NO DISPATCH
Actual caution
Refer to MEL 32-09-02
False caution
ATA 34 NAVIGATION ECAM WARNING
ACTION
NAV ADR 1 FAULT
Refer to MEL 34-10-01
ADR 2 FAULT
Refer to MEL 34-10-02
ADR 3 FAULT
Refer to MEL 34-10-03
ADR (1+2)(1+3)(2+3) FAULT
NO DISPATCH
ADR 1+2+3 FAULT
NO DISPATCH
ALTI DISCREPANCY
Refer to MEL 34-10-01, or Refer to MEL 34-10-02, or Refer to MEL 34-10-03
ADR DISAGREE
NO DISPATCH
ATT DISCREPANCY
Refer to MEL 34-10-04, or Refer to MEL 34-10-05, or Refer to MEL 34-10-06, or Refer to MEL 34-10-07
CAPT (F/O)(STBY) AOA FAULT
Refer to MEL 34-11-01
FM/GPS POS DISAGREE
Not applicable
GPS 1(2) FAULT
Refer to MEL 34-50-09
GPWS FAULT
Refer to MEL 34-40-01
GPWS TERR DET FAULT
Refer to MEL 34-40-01
DISPATCH CONDITION
A320/A321 01.03.20 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 34 NAVIGATION ECAM WARNING
ACTION
NAV HDG DISCREPANCY
Refer to MEL 34-10-04, or Refer to MEL 34-10-05, or Refer to MEL 34-10-06, or Refer to MEL 34-10-07
IAS DISCREPANCY
Refer to MEL 34-10-01, or Refer to MEL 34-10-02, or Refer to MEL 34-10-03
ILS 1(2) (1 + 2) FAULT
Refer to MEL 34-30-04
IR DISAGREE
NO DISPATCH
IR NOT ALIGNED
Refer to MEL 34-10-04, or Refer to MEL 34-10-05, or Refer to MEL 34-10-06, or Refer to MEL 34-10-07
IR 1 FAULT
Refer to MEL 34-10-04
IR 2 FAULT
Refer to MEL 34-10-05
IR 3 FAULT
Refer to MEL 34-10-06, or Refer to MEL 34-10-07
IR (1+2)(1+3)(2+3) FAULT
NO DISPATCH
LS 1(2)(1+2) FAULT
Refer to MEL 34-30-04
PRED W/S DET FAULT (If installed)
Refer to MEL 34-40-06
RA DEGRADED
Refer to MEL 34-40-03
RA 1(2) FAULT
Refer to MEL 34-40-03
TCAS FAULT
Refer to MEL 34-40-04
TCAS STANDBY
Not applicable
OVERSPEED
Not applicable
DISPATCH CONDITION
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.21 ECAM MESSAGES
ATA 36 PNEUMATIC ECAM WARNING
ACTION
DISPATCH CONDITION
AIR APU BLEED FAULT
Refer to MEL 36-12-02
APU BLEED LEAK
Refer to MEL 36-12-01
Actual caution
Refer to MEL 36-22-03
False caution
BLEED 1(2) OFF
Refer to MEL 36-11-01
ENG HP VALVE FAULT
Refer to MEL 36-11-07
ENG 1(2) BLEED ABNORM PR
Refer to MEL 36-11-01
ENG 1(2) BLEED FAULT
Refer to MEL 36-11-01
ENG 1(2) BLEED LEAK
NO DISPATCH
Actual caution
Refer to MEL 36-22-01
False caution
ENG 1(2) (1 + 2) BLEED LO TEMP
Refer to MEL 36-11-04
ENG 1(2) BLEED NOT CLSD
Refer to MEL 36-11-02
ENG 1(2) LEAK DET FAULT
Refer to MEL 36-22-01
L(R) WING LEAK
NO DISPATCH
L(R) WING LEAK DET FAULT
NO DISPATCH
X BLEED FAULT
Refer to MEL 36-12-04
BLEED MONITORING FAULT
NO DISPATCH
MONIT SYS 1(2) FAULT
Refer to MEL 36-11-08
A320/A321 01.03.22 ECAM MESSAGES
MEL/CDL
12 FEB 12 MEL
ATA 46 INFORMATION SYSTEM ECAM WARNING
ACTION
DISPATCH CONDITION
DATALINK ATC FAULT
Refer to MEL 46-21-01
ATSU FAULT
Refer to MEL 46-21-01
COMPANY FAULT
Refer to MEL 46-21-01 ATA 49 AIRBORNE AUXILIARY POWER
ECAM WARNING
ACTION
DISPATCH CONDITION
APU AUTO (EMER) SHUT DOWN
Refer to MEL 49-10-01 ATA 52 DOORS
ECAM WARNING
ACTION
DISPATCH CONDITION
NO DISPTACH
Actual caution
Refer to MEL 52-07-05
False caution
NO DISPATCH
Actual caution
Refer to MEL 52-07-06
False caution
NO DISPATCH
Actual caution
Refer to MEL 52-07-01
False caution
NO DISPATCH
Actual caution
Refer to MEL 52-07-03
False caution
NO DISPATCH
Actual caution
Refer to MEL 52-07-01
False caution
NO DISPATCH
Actual alert
Refer to MEL 52-07-06
False alert
NO DISPATCH
Actual caution
Refer to MEL 52-07-01
False caution
DOOR AFT (BULK) (FWD) CARGO L(R) AFT AVIONICS L(R) AFT CABIN L(R) EMER EXIT (A320) L(R) EMER EXIT (A321) L(R) FWD AVIONICS L(R) FWD CABIN
A320/A321 12 FEB 12 MEL
MEL/CDL
01.03.23 ECAM MESSAGES
ATA 52 DOORS ECAM WARNING
ACTION
DISPATCH CONDITION
DOOR L(R) FWD EMER EXIT (A320) L(R) FWD EMER EXIT (A321)
NO DISPATCH
Actual alert
Refer to MEL 52-07-03
False alert
NO DISPATCH
Actual alert
Refer to MEL 52-07-01
False alert
ATA 70 ENGINE ECAM WARNING
ACTION
DISPATCH CONDITION
ENG COMPRESSOR VANE
NO DISPATCH
DUAL FAILURE
Not applicable
THR LEVERS NOT SET
Refer to MEL 73-20-01
REV SET
Not applicable
THRUST LOCKED
Not applicable
TYPE DISAGREE
NO DISPATCH
VIB SYS FAULT
Refer to MEL 77-07-02-05, or Refer to MEL 77-07-02-06
ENG 1(2) BLEED STATUS FAULT
Apply ECAM procedure
If this alert is displayed on the EWD before the first engine start, check that no amber cross is displayed on the ENG SD page for OIL TEMP indication of the affected engine. If an amber cross is displayed, the associated EIU may be the cause of the failure (associated engine start not possible).
A320/A321 01.03.24 ECAM MESSAGES
MEL/CDL
01 MAY 12 MEL
ATA 70 ENGINE ECAM WARNING
ACTION
DISPATCH CONDITION
ENG 1(2) COMPRESSOR VANE
NO DISPATCH
CTL VALVE FAULT
NO DISPATCH
EGT (FF)(N1)(N2) DISCREPANCY
NO DISPATCH
EIU FAULT
NO DISPATCH
FADEC A(B) FAULT
NO DISPATCH
FADEC ALTERNATOR
NO DISPATCH
FADEC FAULT
NO DISPATCH
FADEC HI TEMP
NO DISPATCH
FAIL
Not applicable
FUEL CTL FAULT
NO DISPATCH
FUEL FILTER CLOG
NO DISPATCH
Actual alert
Refer to MEL 73-09-01
False alert
FUEL RETURN VALVE
Refer to MEL 73-10-01
HP FUEL VALVE
NO DISPATCH
IGN A(B) FAULT
Refer to MEL 74-31-01 or MEL 74-31-02
Actual alert
Refer to MEL 74-09-01
False alert
NO DISPATCH
Actual alert
Refer to MEL 74-09-01
False alert
IGN A+B FAULT LOW N1
NO DISPATCH
N1(N2)(EGT) OVER LIMIT
Not applicable
OIL FILTER CLOG
NO DISPATCH
Actual alert
Refer to MEL 79-09-02
False alert
OIL HI TEMP
NO DISPATCH
OIL LO PR
NO DISPATCH
Actual alert
Refer to MEL 79-09-01
False alert
ONE TLA FAULT
Refer to MEL 76-11-01
A320/A321 MEL/CDL
MEL
01.03.25 ECAM MESSAGES
ATA 70 ENGINE ECAM WARNING
ACTION
DISPATCH CONDITION
ENG 1(2) OVSPD PROT FAULT
NO DISPATCH
PROBES FAULT ENG 1(2) REV INHIBITED
NO DISPATCH Refer to MEL 78-30-01
REV ISOL FAULT
Refer to MEL 78-30-03
REV PRESSUREIZED
NO DISPATCH
REV SWITCH FAULT
Refer to MEL 78-30-02
REVERSE UNLOCKED
NO DISPATCH
REVERSER FAULT
Refer to MEL 78-30-01
SENSOR FAULT
NO DISPATCH
SHUT DOWN
Not applicable
STALL
Not applicable
START FAULT
Apply ECAM procedure
Refer to FCOM/PRO-SUP-70 START VALVE FAULT
Refer to MEL 80-11-01
THR LEVER ABV IDLE
Not applicable
THR LEVER DISAGREE
NO DISPATCH
THR LEVER FAULT
NO DISPATCH
*
*
*
If the associated THR LEVER NOT AT IDLE message is displayed
A320/A321 01.03.26 ECAM MESSAGES
MEL/CDL
THIS PAGE INTENTIONALLY LEFT BLANK
MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.01 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-00
MAINTENANCE Messages on the STATUS SD page
21-00-03
AFT CRG HEAT MAINTENANCE Message
21-00-03A 21-00-04
21-01-01
1
-
AFT CRG HEAT MAINTENANCE message may be displayed on the STATUS SD page.
C
2
-
TEMP CTL 1(2) MAINTENANCE message may be displayed on the STATUS SD page.
C
2
0
One or both may be inoperative provided ECAM BLEED page displaying system operative.
C
2
0
One or both may be inoperative provided ECAM BLEED page displaying system operative.
C
1
0
May be inoperative provided that all zone duct temperature indications are operative on the COND SD page.
TEMP CTL 1(2) MAINTENANCE Message
21-00-04A 21-01
C
Overhead Panels AIR COND Overhead Panel
21-01-01-01 PACK pb-sw FAULT light 21-01-01-01A 21-01-01-02 PACK pb-sw OFF light 21-01-01-02A 21-01-01-03 HOT AIR pb-sw FAULT light 21-01-01-03A
A320/321
01.21.02 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-01
Overhead Panels
21-01-01
AIR COND Overhead Panel
21-01-01-04 HOT AIR pb-sw OFF light 21-01-01-04A 21-01-02
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
CABIN PRESS Overhead Panel
21-01-02-01 CABIN PRESS MODE SEL pbsw FAULT light 21-01-02-01A 21-01-03
CARGO VENT Overhead Panel
21-01-03-02 AFT ISOL VALVE pb-sw FAULT light 21-01-03-02A 21-01-04
VENTILATION Overhead Panel
21-01-04-01 CAB FANS pbsw OFF light 21-01-04-01A
12 FEB 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-01 21-01-04
Overhead Panels VENTILATION Overhead Panel
21-01-04-02 BLOWER pb-sw FAULT light 21-01-04-02A
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
2
0
One or both may be inoperative.
21-01-04-03 EXTRACT pb-sw FAULT light 21-01-04-03A
21-07 21-07-01
Indications on SD pages Indications on the BLEED SD page
21-07-01-01 Pack Outlet Temperature Indication on the BLEED SD page 21-07-01-01A
01.21.03 AIR CONDITIONING
A320/321
01.21.04 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-07
Indications on SD pages
21-07-01
Indications on the BLEED SD page
21-07-01-02 Pack Turbine Bypass Valve Position Indication on the BLEED SD page 21-07-01-02A
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
21-07-01-03 Pack Compressor Outlet Temperature Indication on the BLEED SD page 21-07-01-03A 21-07-01-04Pack Flow Indication on the BLEED SD page 21-07-01-04A
12 FEB 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.05 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-07 21-07-01
Indications on SD pages Indications on the BLEED SD page
21-07-01-05 Pack Flow Control Valve Position Indication on the BLEED SD page 21-07-01-05A
C
2
0
One or both may be inoperative.
C
1
0
May be inoperative.
C
2
0
One or both may be inoperative.
21-07-01-06Emergency Ram Air Inlet Indication on the BLEED SD page 21-07-01-06A 21-07-02
Indications on the CAB PRESS SD page
21-07-02-01INLET and EXTRACT Indications on the CAB PRESS SD page 21-07-02-01A
Note: During ground operations, correct avionics ventilation should be provided.
A320/321
01.21.06 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-07
Indications on SD pages
21-07-02
Indications on the CAB PRESS SD page
21-07-02-02 Pressure Safety Valves Position Indication on the CAB PRESS SD page 21-07-02-02A
C
1
0
(M)
Pressure safety valves may be indicated open provided that both valves are visually checked closed. MAINTENACE PROCEDURE Refer to AMM 21-31-00-040-004
21-07-02-03 Pack 1 and 2 Indications on the CAB PRESS SD page 21-07-02-03A
21-07-03
C
2
0
One or both may be inoperative.
C
2
0
One or more indications may be inoperative.
C
2
0
Cabin and cockpit zone indications may be inoperative.
Indications on the COND SD page
21-07-03-01Indications on the COND SD page 21-07-03-01A 21-07-04
Indications on the CRUISE SD page
21-07-04-01A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.07 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-09
ECAM Alerts
21-09-01
VENT BLOWER FAULT Alert
Note: During ground operations, correct avionics ventilation should be provided.
21-09-01A
Blower fan operative
C
1
0
(O)(M) May be displayed provided that: 1) The blower fan is checked operative before each flight, and 2) The VENT AVNCS SYS FAULT alert is checked operative before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Disregard the VENT BLOWER FAULT alert displayed on the EWD. Disregard the BLOWER pb-sw FAULT light illuminated on the VENTILATION Overhead Panel. Note: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B . . . . . . . . . . . . . . . . . . . . . . . . .Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. MAINTENACE PROCEDURE Refer to AMM 21-26-00-040-010
21-09-01B
Blower fan inoperative
C
1
0
May be displayed provided that the avionics blower fan is considered inoperative. Refer to Item 21-26-01 Avionics Blower Fan
A320/321
01.21.08 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-09
ECAM Alerts
21-09-02
21-09-02A
VENT EXTRACT FAULT Alert
Extract fan operative
Note: During ground operations, correct avionics ventilation should be provided. C
1
0
(O)(M) May be displayed provided that: 1) The extract fan is checked operative before each flight, and 2) The VENT AVNCS SYS FAULT alert is checked operative before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Disregard the VENT EXTRACT FAULT alert displayed on the EWD. MAINTENACE PROCEDURE Refer to AMM 21-26-00-040-011
21-09-02B
Extract fan inoperative
C
1
0
May be displayed provided that the avionics extract fan is considered inoperative. Refer to Item 21-26-02 Avionics Extract Fan
21-09-03
21-09-03A
CAB PR SAFETY VALVE OPEN Alert C
1
0
(M)
May be displayed provided that both safety valves are visually checked closed. MAINTENACE PROCEDURE Refer to AMM 21-31-00-040-005
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.09 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-21
Air Distribution and Recirculation
21-21-01
Cabin Fan
21-21-01A 21-23
C
2
1
C
1
0
One may be inoperative.
Lavatory and Galley Ventilation
21-23-01
21-23-01B
Lavatory and Galley Extraction Fan (O)
May be inoperative provided that all duct temperatures indications for the cabin are operative on the COND SD page. OPERATING PROCEDURES GENERAL INFORMATION Two amber crosses replace the cabin zone temperature indications on the COND SD page. Refer to Item 21-07-03-01 Indications on the COND SD page The INOP SYS column on the STATUS SD page may display the LAV DET message. The cabin zone temperature regulation is lost. The Air Conditioning System Controller commands FWD and AFT cabin ducts temperature using the position of the FWD CABIN selector and the AFT CABIN selector on the AIR COND overhead panel. Slight effect on cabin comfort may occur. The cockpit temperature regulation is still operative.
A320/321
01.21.10 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-01
21-26-01A
Avionics Blower Fan
VENT AVNCS C SYS FAULT not displayed
Note: During ground operation, correct avionics ventilation should be provided. 1
0
(O)
May be inoperative provided that: 1) The BLOWER pb-sw is set to OVRD, 2) Both air conditioning packs are operative, and 3) The VENT AVNCS SYS FAULT alert is not displayed. OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning correctly operates with both air conditioning packs set to on. - BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Check that the VENT AVNCS SYS FAULT and VENT EXTRACT FAULT alerts are not displayed on the EWD. · If the VENT EXTRACT FAULT alert is displayed on the EWD, the blower fan may be seized. In that case: - Contact the maintenance personnel to exchange the blower fan and the extract fan. Only the VENT EXTRACT FAULT alert must then be displayed on the EWD. - When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract Fan
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.11 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-01 21-26-01B
Avionics Blower Fan Air conditioning C inlet valve checked open
1
0
(O)(M) May be inoperative provided that: 1) The BLOWER pb-sw is set to OVRD, 2) Both air conditioning packs are operative, and 3) The air conditioning inlet valve is checked open before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning correctly operates with both air conditioning packs set to on. - BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Check that the VENT EXTRACT FAULT alert is not displayed on the EWD · If the VENT EXTRACT FAULT alert is displayed on the EWD, the blower fan may be seized. In that case: - Contact the maintenance personnel to exchange the blower fan and the extract fan. Only the VENT EXTRACT FAULT alert must then be displayed on the EWD. - When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract Fan MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-006
A320/321
01.21.12 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-01 21-26-01C
Avionics Blower Fan Avionics C ventilation system checked
1
0
(O)(M) May be inoperative provided that: 1) The BLOWER pb-sw is set to OVRD, 2) Both air conditioning packs are operative, 3) The air conditioning inlet valve is secured in the open position, and 4) The avionics ventilation system is checked before each flight.
OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that air the conditioning correctly operates with both air conditioning packs set to on. - BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Check that the VENT EXTRACT FAULT alert is not displayed on the EWD · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert using the CLR pb. The VENT AVNCS SYS FAULT alert will be displayed after landing
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.21.13 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-01 21-26-01C
Avionics Blower Fan Avionics ventilation system checked (cont’d)
OPERATING PROCEDURES (cont’d) · If the VENT EXTRACT FAULT alert is displayed on the EWD, the blower fan may be seized. In that case: - Contact the maintenance personnel to exchange the blower fan and the extract fan. Only the VENT EXTRACT FAULT alert must then be displayed on the EWD. - When the blower and extract fans are exchanged, Refer to Item 21-26-02 Avionics Extract Fan
MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-013
A320/321
01.21.14 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-02
21-26-02A
Avionics Extract Fan
VENT AVNCS C SYS FAULT not displayed
Note: During ground operation, correct avionics ventilation should be provided. 1
0
(O)
May be inoperative provided that: 1) The blower fan is operative, 2) The EXTRACT pb-sw is set to OVRD, 3) Both air conditioning packs are operative, and 4) The VENT AVNCS SYS FAULT alert is not displayed. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Time limitation on ground with electrical network supplied: OAT (°C) MAX TIME
£ 38
£ 45
£ 55
No limit
3h
35 min
DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning correctly operates with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Clear the VENT EXTRACT FAULT alert using the CLR pb. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.15 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-02 21-26-02A
Avionics Extract Fan VENT AVNCS SYS FAULT not displayed (cont’d)
OPERATING PROCEDURES (Cont’d)
- AVNCS VENT/EXTC/FAN (123VU AE2) (A320) - AVNCS VENT/EXTC/FAN (123VU AC4) (A321) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull - Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD. Note: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B . . . . . . . . . . . . . . . . . . . . . . . . . Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. 21-26-02B
Air conditioning C inlet valve checked open
1
0
(O)(M) May be inoperative provided that: 1) The blower fan is operative, 2) The EXTRACT pb-sw is set to OVRD, 3) Both air conditioning packs are operative, and 4) The air conditioning inlet valve is checked open before each flight.
(Cont’d on next page)
A320/321
01.21.16 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
12 FEB 12 MEL
MEL/CDL
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-02 21-26-02B
Avionics Extract Fan Air conditioning inlet valve checked open (cont’d)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Time limitation on ground with electrical network supplied:
OAT (°C) MAX TIME
£ 38
£ 45
£ 55
No limit
3h
35 min
DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning correctly operates with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Clear the VENT EXTRACT FAULT alert using the CLR pb. - AVNCS VENT/EXTC/FAN (123VU AE2 or AC4) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.21.17 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-02 21-26-02B
Avionics Extract Fan Air conditioning inlet valve checked open
OPERATING PROCEDURES (cont’d)
Note: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft.
MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-007
A320/321
01.21.18 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-02 21-26-02C
Avionics Extract Fan Avionics C ventilation system checked
1
0
(O)(M) May be inoperative provided that: 1) The blower fan is operative, 2) The EXTRACT pb-sw is set to OVRD, 3) Both air conditioning packs are operative, 4) The air conditioning inlet valve is secured in the open position, and 5) The avionics ventilation system is checked before each flight. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Time limitation on ground with electrical network supplied: OAT (°C) MAX TIME
£ 38
£ 45
£ 55
No limit
3h
35 min
DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning correctly operates with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Clear the VENT EXTRACT FAULT alert using the CLR pb. - AVNCS VENT/EXTC/FAN (123VU AE2 or AC4) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.21.19 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-02 21-26-02C
Avionics Extract Fan Avionics ventilation system checked (cont’d)
OPERATING PROCEDURES (Cont’d) · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert using the CLR pb. The VENT AVNCS SYS FAULT alert will be displayed after landing.
Note: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft.
MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-015
A320/321
01.21.20 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-03
21-26-03A
Avionics Skin Exchanger Inlet Bypass Valve C
1
0
(O)(M) May be inoperative provided that: 1) The avionics skin exchanger inlet bypass valve is manually secured in the closed position, and 2) The avionics ventilation system is checked before each flight. Note: During ground operations, correct avionics ventilation should be provided.
OPERATING PROCEDURES ON GROUND · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. The VENT AVNCS SYS FAULT alert will be displayed after landing. MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.21 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-04
21-26-04A
Avionics Skin Air Outlet Valve
C
1
0
(O)(M) May be inoperative provided that: 1) The internal flap is manually secured in the open position, 2) The skin air outlet valve is displayed in a partially open position amber or green on the CAB PRESS SD page, 3) Both air conditioning packs are operative, 4) The skin exchanger isolation valve is secured in the open position, and 5) The avionics ventilation system is checked before each flight.
Note: During ground operations, correct avionics ventilation should be provided.
(Cont’d on next page)
A320/321
01.21.22 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
12 FEB 12 MEL
MEL/CDL
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-04
Avionics Skin Air Outlet Valve
21-26-04A (cont’d)
OPERATING PROCEDURES ON GROUND · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. The VENT AVNCS SYS FAULT alert will be displayed after landing. · If the VENT SKIN VALVE FAULT alert is displayed on the EWD: Apply the ECAM procedure. Note: Avionics smoke may be not perceptible from the cockpit due to the opening of the internal flap of the valve. In the case of AVIONICS SMOKE alert: Apply the ECAM procedure even if the smoke is not perceptible. MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-002
21-26-05
Avionics Skin Air Inlet Valve
Note: During ground operations, correct avionics ventilation should be provided.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.23 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-05 21-26-05A
Avionics Skin Air Inlet Valve (cont’d) Air Conditioning C Inlet Valve open on ground
1
0
(O)(M) May be inoperative provided that: 1) The avionics skin air inlet valve is manually secured in the closed position, 2) The air conditioning inlet valve is open on ground, and 3) The avionics ventilation system is checked before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning is operating with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Check that the skin air inlet valve is closed on the CAB PRESS SD page. - Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. Note: With only one air conditioning pack operative, operating time on ground is limited to 1 h.
(Cont’d on next page)
A320/321
01.21.24 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-05 21-26-05A
Avionics Skin Air Inlet Valve Air Conditioning Inlet Valve open on ground (cont’d)
OPERATING PROCEDURES (Cont’d) AFTER TAKEOFF EXTRACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO AFTER LANDING EXTRACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-004
21-26-05B
Air Conditioning C Inlet Valve Secured Open
1
0
(O)(M) May be inoperative provided that: 1) The avionics skin air inlet valve is manually secured in the closed position, 2) The air conditioning inlet valve is secured in the open position, and 3) The avionics ventilation system is checked before each flight.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.21.25 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-05 21-26-05B
Avionics Skin Air Inlet Valve Air Conditioning Inlet Valve Secured Open (Cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning is operating with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Check that the skin air inlet valve is closed on the CAB PRESS SD page.
· After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. The VENT AVNCS SYS FAULT alert will be displayed after landing.
(Cont’d on next page)
A320/321
01.21.26 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-05 21-26-05B
Avionics Skin Air Inlet Valve Air Conditioning Inlet Valve Secured Open (cont’d)
OPERATING PROCEDURES (Cont’d) Note: With only one air conditioning pack operative, operating time on ground is limited to 1 h. AFTER TAKEOFF EXTRACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO AFTER LANDING EXTRACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OVRD MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-014
21-26-06
21-26-06A
Avionics Skin Exchanger Isolation Valve Valve inoperative in the open position
Note: During ground operations, correct avionics ventilation should be provided. C
1
0
(O)(M) May be inoperative in the open position provided that the avionics ventilation system is checked before each flight.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.27 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-06
21-26-06A
Avionics Skin Exchanger Isolation Valve Valve inoperative in the open position (cont’d)
OPERATING PROCEDURES ON GROUND · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. MAINTETNANCE PROCEDURE Refer to AMM 21-26-00-040-008
21-26-06B
Valve secured open
C
1
0
(O)(M) May be inoperative provided that: 1) The avionics skin exchanger isolation valve is secured in the open position, and Note: If the valve cannot be secured in the open position, it can be interchanged with the skin exchanger outlet bypass valve. 2) The avionics ventilation system is checked before each flight. (Cont’d on next page)
A320/321
01.21.28 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-06
21-26-06B
Avionics Skin Exchanger Isolation Valve Valve secured open (Cont’d)
OPERATING PROCEDURES
ON GROUND · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb.
MAINTETNANCE PROCEDURE Refer to AMM 21-26-00-040-016
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.29 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-07
Avionics Skin Exchanger Outlet Bypass Valve
21-26-07A
C
1
0
May be inoperative. Note: During ground operations, correct avionics ventilation should be provided.
21-26-08
21-26-08A
Avionics Air Conditioning Inlet Valve C
1
0
(O)(M) May be inoperative provided that: 1) The avionics air conditioning inlet valve is manually secured in the open position, 2) Both air conditioning packs are operative, and 3) The avionics ventilation is checked before each flight. Note: During ground operations, correct avionics ventilation should be provided. OPERATING PROCEDURES ON GROUND · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. MAINTETNANCE PROCEDURE Refer to AMM 21-26-00-040-003
A320/321
01.21.30 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-09
Avionics Ventilation Filte
Note: During ground operations, correct avionics ventilation should be provided.
21-26-09A
VENT AVNCS C SYS FAULT not displayed
1
0
(O)
May be inoperative (clogged) provided that: 1) The blower and extract fans are operative, 2) The EXTRACT pb-sw is set to OVRD, 3) Both air conditioning packs are operative, and 4) The VENT AVNCS SYS FAULT alert is not displayed.
OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning is operating with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD - Check that the VENT AVNCS SYS FAULT alert is not displayed on the EWD. 21-26-09B
Valve checked C open
1
0
(O)(M) May be inoperative (clogged) provided that: 1) The blower and extract fans are operative, 2) The EXTRACT pb-sw is set to OVRD, 3) Both air conditioning packs are operative, and 4) The air conditioning inlet valve is checked open before each flight. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.31 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-09 21-26-09B
Avionics Ventilation Filte Valve checked open (cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning is operating with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD MAINTETNANCE PROCEDURE Refer to AMM 21-26-00-040-009
21-26-09C
Valve secured open
C
1
0
(O)(M) May be inoperative (clogged) provided that: 1) The blower and extract fans are operative, 2) The EXTRACT pb-sw is set to OVRD, 3) Both air conditioning packs are operative, 4) The air conditioning inlet valve is secured in the open position, and 5) The avionics ventilation system is checked before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the air conditioning is operating with both air conditioning packs set to on. - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD (Cont’d on next page)
A320/321
01.21.32 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-09 21-26-09C
Avionics Ventilation Filte Valve secured open (cont’d)
OPERATING PROCEDURES (Cont’d) · After application of the maintenance procedure: Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb. The VENT AVNCS SYS FAULT alert will be displayed after landing. MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-017
21-26-10
21-26-10A
Avionics Equipment Ventilation Computer (AEVC) C
1
0
(O)(M) May be inoperative provided that: 1) Both air conditioning packs are operative, 2) The BLOWER pb-sw and the EXTRACT pb-sw are set to OVRD, 3) The air conditioning inlet valve and the skin air outlet valve are checked in the correct position before each flight, 4) The extract fan is checked operative before each flight, and 5) The skin air inlet valve is secured in the closed position. Note: During ground operations, correct avionics ventilation should be provided. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.21.33 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
21-26-10
Avionics Equipment Ventilation Avionics Equipment Ventilation Computer (AEVC)
21-26-10A (cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION - Supply the aircraft electrical network. - Check that the conditioning is operating with both air conditioning packs set to on. - BLOWER pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OVRD - EXTRACT pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . OVRD Note: If the ground horn sounds: EIS/HORN/SPLY (121VU P09) C/B. . . . . . . . . . . . . . . . . . . . . . . . . . Pull The C/B must be closed again after first engine start If the ground horn sounds after landing when engines are off, it can be silenced again. In this case, the ADIRS must be set to OFF before leaving the aircraft. Note: In the case of a low pressure in the avionics compartment ventilation ducts, the weather radar image may not be displayed on the ND on ground. Clear the VENT AVNCS SYS FAULT alert displayed on the EWD using the CLR pb (Cont’d on next page)
A320/321
01.21.34 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-26
Avionics Equipment Ventilation
21-26-10
Avionics Equipment Ventilation Computer (AEVC)
21-26-10A (cont’d)
OPERATING PROCEDURES (Cont’d) IN FLIGHT · In the case of an air conditioning pack failure: - The cabin altitude may reach about 9 700 ft, and - The CAB PR EXCESS CAB ALT alert may be displayed on the EWD. MAINTENANCE PROCEDURE Refer to AMM 21-26-00-040-005
21-28
Cargo Compartment Ventilation
21-28-03 21-28-03A
AFT Cargo Extraction Fan C
1
0
(O)
May be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Live animals must not be carried in the aft cargo compartment.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.35 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-28
Cargo Compartment Ventilation
21-28-04 21-28-04A
AFT Cargo Isolation Valve AFT ISOL VALVE pb-sw FAULT light operative
C
2
0
(O)
One or both may be inoperative provided that: 1) Both valves are checked closed, and 2) AFT ISOL VALVE pb-sw FAULT light is checked operative.
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Live animals must not be carried in the aft cargo compartment. DURING COCKPIT PREPARATION - ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST - Check that the AFT ISOL VALVE pb-sw FAULT light comes on - ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . BRT or DIM - AFT ISOL VALVE pb-sw . . . . . . . . . . . . . . . . . . . OFF - Check that the AFT ISOL VALVE pb-sw FAULT light does not come on.
(Cont’d on next page)
A320/321
01.21.36 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-28
Cargo Compartment Ventilation
21-28-04 21-28-04A
AFT Cargo Isolation Valve AFT ISOL VALVE pb-sw FAULT light operative (cont’d)
OPERATING PROCEDURES (cont’d) Note: · If the AFT ISOL VALVE pb-sw FAULT light comes on: The AFT cargo isolation valve must be secured in the closed position. Refer to Item 21-28-04B AFT Cargo Isolation Valve
21-28-04B
Both valves C secured closed
1
0
(O)(M) One or both may be inoperative provided that both valves are secured in the closed position. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Live animals must not be carried in the aft cargo compartment. ON GROUND · When the AFT cargo isolation valves are secured in the closed position: The AFT isolation valves are displayed open green on the COND SD page. MAINTENANCE PROCEDURE Refer to AMM 21-28-00-040-002
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.37 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-31
Pressure Control and Monitoring
21-31-01
21-31-01A
Automatic Cabin Pressure Control System (CPC, Outflow Valve AUTO Channel) Automatic CPC A 1 inoperative
2
1
(O)(M) Automatic cabin pressure control system 1 may be inoperative for three flight days provided that: 1) It is deactivated, 2) The cabin pressure indications on the CAB PRESS SD page are checked operative in manual mode, 3) The LDG ELEV selector MAN function is operative, and 4)Extanded overwater flight is prohibited. OPERATING PROCEDURES DURING COCKPIT PREPARATION · If CPC 1 is affected: AIR COND/CAB/PRESS/CTL 1 (49VU D09) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull · If CPC 2 is affected: AIR COND/CAB/PRESS/CTL 2 (122VU Y22) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull - RPCU (122VU X23) C/B . . . . . . . . . . . . . . . . . . . Pull - MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . . . . MAN - On the CAB PRESS SD page, check that the cabin differential pressure, the cabin vertical speed, the cabin altitude, and the outflow valve position are available.
(Cont’d on next page)
A320/321
01.21.38 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-31
Pressure Control and Monitoring
21-31-01
21-31-01A
Automatic Cabin Pressure Control System (CPC, Outflow Valve AUTO Channel) Automatic CPC 1 inoperative (cont’d)
OPERATING PROCEDURES (cont’d) - MAN V/S CTL sw . . . . . . . . . . . . . . . . . . . . . . . . DN - On the CAB PRESS SD page, check outflow valve movement. - RPCU (122VU X23) C/B . . . . . . . . . . . . . . . . . . . Push - MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . . . . AUTO
21-31-01B
Automatic CPC C 2 inoperative
2
1
(O)(M) Automatic cabin pressure control system 2 may be inoperative provided that: 1) It is deactivated, 2) The cabin pressure indications on the CAB PRESS SD page are checked operative in manual mode, and 3) The LDG ELEV selector MAN function is operative.
OPERATING PROCEDURES Refer to item 21-31-01A for operating procedures
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.39 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-31
Pressure Control and Monitoring
21-31-01
21-31-01C
Automatic Cabin Pressure Control System (CPC, Outflow Valve AUTO Channel)
Both automatic C CPCs inoperative
2
0
Both may be inoperative provided that: 1) The manual cabin operative, and
pressure
control
system
is
2) The flight is not pressurized. Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Cabin
Flight must conducted in accordance with FOPM CH 8 Maintenance Ferry Flights. 21-31-02
21-31-02A
Manual Cabin Pressure Control System (MAN V/S CTL selector, Outflow Valve MAN Channel) C
1
0
(M)
May be inoperative provided that: 1) The LDG ELEV selector MAN function is operative, and 2) Both automatic cabin pressure control systems are checked operative before each flight. MAINTENANCE PROCEDURE Refer to AMM 21-31-00-040-002
A320/321
01.21.40 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-31
Pressure Control and Monitoring
21-31-03
Pressure Safety Valve
21-31-03A
C
2
1
(M)
One may be inoperative in the closed position provided that: 1) Both automatic cabin pressure control systems are operative, and 2) The three outflow valve motors are checked operative. MAINTENANCE PROCEDURE Refer to AMM 21-31-00-040-001
21-31-04
21-31-04A
Landing Elevation Selection AUTO Function C
1
0
(O)
May be inoperative. OPERATING PROCEDURES BEFORE TAKEOFF - Set the LDG ELEV selector on the CABIN PRESS panel at the destination airport altitude. - On the CAB PRESS SD page, check that the LDG ELEV MAN message is displayed .
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.41 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-31
Pressure Control and Monitoring
21-31-05
Landing Elevation Selection MAN Function
21-31-05A
C
1
0
(O)
May be inoperative provided that: 1) The landing elevation selection AUTO function is operative, and 2) Both FMGCs are operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION On the CAB PRESS SD page, check that the LDG ELEV AUTO message is displayed to confirm correct position of the LDG ELEV selector. Note: The landing field elevation of the destination airport may not be correctly displayed on the CAB PRESS SD page. It is automatically corrected after first engine start.
21-43
Cargo Compartment Heating
21-43-02
21-43-02A
AFT Cargo Compartment Heating HOT AIR pb-sw C OFF
1
0
(O)
Hot air pressure regulating valve or trim air valve may be inoperative provided that: 1) The HOT AIR pb-sw on the CARGO HEAT overhead panel is set to OFF, and 2) The operative valve is indicated closed on the COND SD page. (Cont’d on next page)
A320/321
01.21.42 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-43
Cargo Compartment Heating
21-43-02
21-43-02A
AFT Cargo Compartment Heating HOT AIR pb-sw OFF (cont’d)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS AFT CARGO compartment heat is not be available. Live animals and/or temperature sensitive cargo, must not be carried in the aft cargo compartment. DURING COCKPIT PREPARATION - HOT AIR pb-sw (on the CARGO HEAT overhead panel)...................................................... OFF - On the COND SD page, check that the operative valve (either the hot air pressure regulating valve or the trim air valve) is indicated closed.
21-43-02B
Valves secured C closed
1
0
(O)(M) Hot air pressure regulating valve or trim air valve may be inoperative provided that one of these valves is secured in the closed position. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS AFT CARGO compartment heat is not be available. Live animals and/or temperature sensitive cargo, must not be carried in the aft cargo compartment. MAINTENANCE PROCEDURE Refer to AMM task
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.43 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-51
Pack Flow Control
21-51-02
Pack Flow Selection
21-51-02A 21-51-03
C
1
0
C
2
1
May be inoperative.
Pack Flow Sensor
21-51-03A
(O)
One may be inoperative. OPERATING PROCEDURE GENERAL INFORMATION The hot air pressure regulating valve automatically closes. The Flow Control Valve on the affected side operates in pneumatic backup mode. DURING COCKPIT PREPERATION AIR COND HOT AIR pb-sw. . . . . . . . . . . . . . . . . . OFF
21-52
Air Cooling System
21-52-01 21-52-01D
Air Conditioning Pack No FL limitation
C
2
1
(O)(M) One may be inoperative provided that: (FD) 1) The following alerts: AIR PACK 1(2) REGUL FAULT AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULT associated with the operative pack are not displayed on the EWD, and 2) The affected PACK 1(2) pb-sw is set to OFF, and 3) The speedbrakes are operative, and 4) The associated pack flow control valve is secured in the closed position. (Cont’d on next page)
A320/321
01.21.44 AIR CONDITIONING
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-52
Air Cooling System
21-52-01 21-52-01D
Air Conditioning Pack No FL limitation (cont’d)
OPERATING PROCEDURES
DURING COCKPIT PREPARATION PACK FLOW pb-sw (A320) . . . . . . . . . . . . . . . . . HI ECON FLOW pb-sw (A321) . . . . . . . . . . . . . . . . . Off
IN FLIGHT · If BLOWER pb-sw and EXTRACT pb-sw are set to OVRD: - The cabin altitude may reach about 9,700 ft, and - The CAB PR EXCESS CAB ALT alert may be displayed on the EWD
MAINTENANCE PROCEDURE Refer to AMM 21-51-00-040-002
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.45 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-52
Air Cooling System
21-52-01 21-52-01E
Air Conditioning Pack Limitation to 31 500 ft
C
2
1
(O)(M) One may be inoperative provided that: (FD) 1) The flight altitude is limited to 31 500 ft, and 2) The following alerts: AIR PACK 1(2) REGUL FAULT AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULT associated with the operative pack are not displayed on the EWD, and 3) The affected PACK 1(2) pb-sw is set to OFF, and 4) The associated pack flow control valve is secured in the closed position.
OPERATING PROCEDURES Refer to Item 21-52-01D
MAINTENANCE PROCEDURE Refer to AMM 21-51-00-040-002
A320/321
01.21.46 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
01 MAY 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-52
Air Cooling System
21-52-01 21-52-01G
Air Conditioning Pack Air cycle machine failed
C
2
1
(O)(FD) One may be operated on heat exchanger cooling only (air cycle machine failure) provided that: 1) The following alerts: AIR COND CTL 1(2)-A FAULT AIR COND CTL 1(2)-B FAULT associated with the operative pack are not displayed on the EWD, and 2) The affected pack outlet temperature indication is operative on the BLEED SD page.
OPERATING PROCEDURES DURING COCKPIT PREPARATION PACK 1(2) pb-sw in "heat exchanger cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF IN FLIGHT · When the TAT is equal to or less than 12° C: PACK 1(2) pb-sw in "heat exchanger cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . On · If the non affected air conditioning pack fails: Maximum flight altitude . . . . . . . . . . . . . . . . . . . . .31,500 ft
(Cont’d on next page)
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.47 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-52
Air Cooling System
21-52-01 21-52-01G
Air Conditioning Pack (cont’d) Air cycle machine failed (cont’d)
OPERATING PROCEDURES (Cont’d) DURING DESCENT · If the TAT is above 12° C: PACK 1(2) pb-sw in "heat exchanger cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF AT THE END OF THE DESCENT, BEFORE LANDING PACK 1(2) pb-sw in "heat exchanger cooling only" . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
21-52-01H
Non pressurized flight
C
2
0
Both may be inoperative provided that the flight is not pressurized. Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Cabin
Refer to FOPM CH 8 Maintenance Ferry Flights 21-52-02
21-52-02A
Air Conditioning Pack Ram Air Inlet Flap Flap deactivated
C
2
0
(M)
One or both may be inoperative provided that the affected flap is deactivated in the open position. MAINTENANCE PROCEDURE Refer to AMM 21-61-00-040-002
21-52-02B
Only one inoperative
C
2
1
One may be inoperative in the closed position provided that the associated air conditioning pack is considered inoperative. Refer to Item 21-52-01 Air Conditioning Pack
A320/321
01.21.48 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
01 MAY 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-52
Air Cooling System
21-52-02
21-52-02C
Air Conditioning Pack Ram Air Inlet Flap Non pressurized flight
C
2
0
Both may be inoperative in the closed position provided that the flight is not pressurized. Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Cabin
Refer to FOPM CH 8 Maintenance Ferry Flights 21-55
Emergency Ram Air Inlet
21-55-01 21-55-01A
Emergency Ram Air Inlet Ram air inlet deactivated
C
1
0
(M)
May be inoperative provided: 1) The emergency ram air inlet is deactivated in the closed position, and 2) Both air conditioning packs are checked operative. MAINTENANCE PROCEDURE Refer to AMM 21-55-00-040-002
21-55-01B
Non pressurized flight
C
1
0
May be inoperative in the open position provided that: 1) Extended overwater flight is not conducted, and 2) The flight is not pressurized. Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Refer to FOPM CH 8 Maintenance Ferry Flights
Cabin
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.49 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONIN 21-61
Pack Temperature Control
21-61-01
Pack Turbine Bypass Valve
21-61-01A 21-63
C
2
1
Affected valve C checked closed
3
0
One may be inoperative.
Cockpit and Cabin Temperature Control
21-63-02 21-63-02A
Cockpit and Cabin Trim Air Valve (O)
One or more may be inoperative provided that the affected valve is checked closed on the COND SD page. OPERATING PROCEDURES DURING COCKPIT PREPARATION On the COND SD page page, check that the affected trim air valve is closed amber. IN FLIGHT · If the affected zone temperature becomes uncomfortable: HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
21-63-02B
Hot air pressure C valve checked operative
3
0
(O)
One or more may be inoperative provided that the hot air pressure regulating valve is checked operative on the COND SD page.
(Cont’d on next page)
A320/321
01.21.50 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
01 MAY 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONIN 21-63
Cockpit and Cabin Temperature Control
21-63-02 21-63-02B
Cockpit and Cabin Trim Air Valve Hot air pressure valve checked operative (cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION - HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OFF then on - On the COND SD page, check that the hot air pressure regulating valve follows the HOT AIR pb-sw command. IN FLIGHT · If affected zone temperature becomes uncomfortable: HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
21-63-02E
Hot air pressure C valve considered inoperative
3
0
One or more may be inoperative provided that the hot air pressure regulating valve is considered inoperative.
Refer to Item 21-63-03 Hot Air Pressure Regulating Valve
21-63-03
21-63-03A
Hot Air Pressure Regulating Valve
Hot air pressure C valve checked closed
1
0
(O)
May be inoperative in the closed position provided that: 1) HOT AIR pb-sw is set to OFF, and 2) Hot Air Pressure Regulating Valve is checked closed on the COND SD page. (Cont’d on next page)
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.21.51 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONIN 21-63
Cockpit and Cabin Temperature Control
21-63-03 21-63-03A
Hot Air Pressure Regulating Valve Hot air pressure valve checked closed (cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION - HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF - On the COND SD page page, check that the hot air pressure regulating valve is closed amber.
21-63-03B
All trim valve C checked closed
1
0
(O)
May be inoperative in the open position provided that: 1) HOT AIR pb-sw is set to OFF, and 2) All Trim Air Valves are checked closed on the COND SD page. OPERATING PROCEDURES GENERAL INFORMATION On the COND SD page, the hot air pressure regulating valve is displayed amber open. DURING COCKPIT PREPARATION - HOT AIR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OFF - On the COND SD page, check that all the trim air valves are closed amber.
21-63-03C
Hot air pressure C valve secured closed
1
0
(O)(M) May be inoperative provided that the hot air pressure regulating valve is secured in the closed position.
(Cont’d on next page)
A320/321
01.21.52 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
01 MAY 12 MEL
MEL/CDL
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-63
Cockpit and Cabin Temperature Control
21-63-03 21-63-03C
Hot Air Pressure Regulating Valve Hot air pressure valve secured closed (cont’d)
OPERATING PROCEDURES GENERAL INFORMATION On the COND SD page, the hot air pressure regulating valve is displayed closed amber. MAINTENANCE PROCEDURE Refer to AMM 21-63-00-040-002
21-63-04
21-63-04A
Air Conditioning System Controller Channel (COND CTL 1(2)-A(B)) C
4
2
One may be inoperative on each side.
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.01 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-01
FLT CTL Overhead Panel
22-01-01
FAC pb-sw FAULT light
22-01-01A
C
2
1
One may be inoperative.
C
2
0
One or both may be inoperative.
22-05-01A
B
2
1
One or more indications may be inoperative on one FMA.
22-05-01B
B
2
0
22-01-02
FAC pb-sw OFF light
22-01-02A 22-05
FMA Indications on the PFD
22-05-01
AP Related Indications on the FMA
(O)
One or more indications may be inoperative on both FMAs provided that that AP is not used. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS RVSM operations are not permitted. Maximum landing capability is CAT I.
22-05-02
A/THR Related Indications on the FMA
22-05-02A
B
2
1
One or more indications may be inoperative on one FMA.
22-05-02B
B
2
0
One or more indications may be inoperative on both FMAs provided that the autothrust (A/THR) is considered inoperative. Refer to Item 22-30-01 Autothrust (A/THR)
A320/321 MEL/CDL
01.22.02 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-05
FMA Indications on the PFD
22-05-03
Approach and Landing Capabilities on the FMA
22-05-03A
C
2
0
(O)
One or more may be inoperative on one or both FMAs. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I.
22-05-04
Special Messages on the FMA
22-05-04A 22-10
B
2
1
B
2
1
“MAN PITCH TRIM ONLY” is required on one side.
Autopilot/Flight Director (AP/FD)
22-10-01 22-10-01A
Autopilot (AP) (O)
One may be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS - When one AP is inoperative: Landing capability is CAT II. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.03 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-10
Autopilot/Flight Director (AP/FD)
22-10-01
Autopilot (AP)(Cont’d)
22-10-01B
A
2
0
(O)(FD)
Both may be inoperative provided: 1) Current weather enroute does not indicate thrunderstorm, activites, and approach minimums are limited to CAT I or higher, 2) Aircraft is not dispatched into RVSM airspace, 3) For international flight Aircraft is released for one leg fly ( 2 ½ hours maximum) to a maintenance station for repair, 4) For domestic flight Aircraft is released for two leg fly ( 2 hours total ) to a maintenance station for repair, OPERATING PROCEDURES -
22-10-02
When both APs are inoperative: RVSM operations are not permitted. Maximum landing capability is CAT I.
Flight Director (FD)
22-10-02A
B
2
1
(O)(FD)
One may be inoperative. OPERATING PROCEDURES FOR TAKEOFF -
22-10-03 22-10-03A
For a takeoff without one FD: Refer to FCOM /PRO No Flight Director Takeoff
Take-over pb Priority Function 2
2
Both must be operative.
A320/321 MEL/CDL
01.22.04 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-10
Autopilot/Flight Director (AP/FD)
22-10-04
22-10-04A
Take-over pb AP Disconnection Function B
2
1
(O)(FD)
One may be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I. BEFORE ENGINE START - AP 1 · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On - Operative take-over pb · · · · · · · · · · · · · · · · · · · · Press - Check that the red AP OFF message is displayed on the EWD. - AP 2 · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On - Operative take-over pb · · · · · · · · · · · · · · · · · · · · Press - Check that the red AP OFF message is displayed on the EWD. BEFORE APPROACH - If the AP is used for approach: The operative AP disconnect pb must be assigned to the PF.
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.05 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-10
Autopilot/Flight Director (AP/FD)
22-10-05
AUTO LAND lights
22-10-05A
C
2
0
(O)(FD)
One or both may be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS -
22-10-06
If Captain side or both lights are inoperative: Maximum landing capability is CAT I.
AP Disengagement Warning
22-10-06A
C
1
0
(O)(FD)
May be inoperative provided that the AP is not engaged. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS RVSM operations are not permitted. Maximum landing capability is CAT I.
22-10-07
22-10-07A
Sticks and Rudder Pedals Locking Solenoid in AP Mode C
3
1
(O)(FD)
One or two may be inoperative unlocked provided that no autoland is performed. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I.
A320/321 MEL/CDL
01.22.06 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-30
Autothrust
22-30-01
Autothrust (A/THR)
22-30-01A
B
1
0
(O)(FD)
May be inoperative provided that the autothrust (A/THR) is disconnected before each flight. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum Landing capability is CAT I. AFTER ENGINE START - Press and hold either autothrust instinctive disconnect pb for at least 15 seconds. - The A/THR system is permanently disconnected for the entire flight. Check that A/THR INOP SYS is displayed on the STATUS SD page. - All A/THR functions protection are lost.
22-30-02
22-30-02A
including
ALPHA
FLOOR
Autothrust Instinctive Disconnect pb C
2
1
(O)
One may be inoperative provided that the ability to disconnect the autothrust (A/THR) via the remaining Instinctive Disconnect pb and by the FCU A/THR pb is checked before each flight. OPERATING PROCEDURES The purpose of the procedure is to check the A/THR disconnection via the remaining Instinctive Disconnect pb and via the A/THR pb on the FCU. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.22.07 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-30
Autothrust
22-30-02
22-30-02A
Autothrust Instinctive Disconnect pb (Cont’d)
OPERATING PROCEDURES(Cont’d) AFTER IRS ALIGNMENT Note: Disregard alerts during the test. Use the EMER CANCEL pb on the ECAM control panel as necessary. Aircraft configuration for the check via the FMS 1: -
ENG/FADEC GND PWR 1 and 2 · · · · · · · · · · · · · ON
-
Both thrust levers · · · · · · · · · · · · · · · · · · · · · · · · MCT
-
FD · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Off
-
AUTO FLT/FMGC/2 (121 VU M17) C/B · · · · · · · Pull
-
A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
Check that green SPEED and white A/THR indications appear on the PFD.
-
Check that A/THR pb light bars are ON.
Check of the A/THR disconnection via the remaining Instinctive Disconnect pb: -
A/THR instinctive disconnect pb (non affected autothrust) · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push
-
Check that the A/THR pb light bars are OFF.
-
Check that green SPEED and white A/THR indications are no more displayed on the PFD. (Cont’d on next page)
A320/321 MEL/CDL
01.22.08 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-30
Autothrust
22-30-02
22-30-02A
Autothrust Instinctive Disconnect pb (Cont’d)
OPERATING PROCEDURES(Cont’d) - A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On - Check that the A/THR pb light bars are ON. - Check that green SPEED and white A/THR indications are displayed on the PFD. Check of the A/THR disconnection via the A/THR pb on the FCU: - A/THR pb (on the FCU) · · · · · · · · · · · · · · · · · · · · · · Off - Check that the A/THR pb light bars are OFF. - Check that green SPEED and white A/THR indications are no more displayed on the PFD. - A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On Aircraft configuration for the check via the FMS 2: - AUTO FLT/FMGC/2 (121VU M17) C/B · · · · · · · · Push - AUTO FLT/FMGC/1 (49VU B02) C/B · · · · · · · · · · · Pull - Wait 2 min. Check of the A/THR disconnection via the remaining Instinctive Disconnect pb: - A/THR instinctive disconnect pb (non affected autothrust)· · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push - Check that the A/THR pb light bars are OFF. - Check that green SPEED and white A/THR indications are no more displayed on the PFD. - A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On - Check that the A/THR pb light bars are ON. - Check that green SPEED and white A/THR indications are displayed on the PFD. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.09 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-30
Autothrust
22-30-02
22-30-02A
Autothrust Instinctive Disconnect pb (Cont’d)
OPERATING PROCEDURES(Cont’d) Check of the A/THR disconnection via the A/THR pb on the FCU: -
A/THR pb (on the FCU) · · · · · · · · · · · · · · · · · · · · Off
-
Check that the A/THR pb light bars are OFF.
-
Check that green SPEED and white A/THR indications are no more displayed on the PFD.
-
A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
Restore normal aircraft configuration:
22-30-03
22-30-03A
-
A/THR · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Off
-
AUTO FLT/FMGC/1 (49VU B02) C/B · · · · · · · · Push
-
ENG/FADEC GND PWR 1 and 2 · · · · · · · · · · · · · Off
-
Both thrust levers· · · · · · · · · · · · · · · · · · · · · · · · IDLE
-
RCL pb (on the ECAM control panel) · · · · · · · · Push
-
Wait 2 min before using the MCDU and the FD.
Autothrust Disengagement Warning B
1
0
May be inoperative provided that the autothrust (A/THR) is considered inoperative. Refer to Item 22-30-01 Autothrust (A/THR)
A320/321 MEL/CDL
01.22.10 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-60
Flight Augmentation (FAC)
22-60-01 22-60-01A
FAC 1 1
1
(M)
Must be operative. Note: The AUTO FLT FAC 1 FAULT alert may be displayed with the associated AUTO FLT/FAC1/28VDC C/B tripped. This may be due to a short circuit within either rudder trim actuator channel 1 or rudder travel actuator channel 1. In this case, the FAC 1 may be recovered provided that the affected part of the faulty actuator is deactivated using the associated maintenance procedure. Refer to AMM 27-22-00-040-001, or Refer to AMM 27-23-00-040-01. Refer to Item 27-22-01 Rudder Trim System, or Refer to Item 27-23-01 Rudder Travel Limiter System (Including Rudder and Pedals Travel Limiter Units) MAINTENANCE PROCEDURE Refer to AMM task.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.11 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-60
Flight Augmentation (FAC)
22-60-02 22-60-02A
FAC 2 C
1
0
(O)(FD)
May be inoperative provided that: 1) All ADIRSs, ELACs, SECs, SFCCs, LGCIUs and RAs are operative, and 2) The Rudder Travel Limiter System 2 is considered inoperative. Refer to item 22-60-04 Yaw Damper System, and Refer to item 27-22-01 Rudder Trim System, and Refer to Item 27-23-01 Rudder Travel Limiter System (Including Rudder and Pedals Travel Limiter Units)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. ON GROUND -
If the AUTO FLT FAC 2 FAULT alert is displayed on the EWD
Or -
If erroneous speeds are displayed: - AUTO FLT/FAC 2/28VDC (121VU M19) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull - FAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . OFF
A320/321 MEL/CDL
01.22.12 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-60
Flight Augmentation (FAC)
22-60-03
22-60-03A
Windshear Detection System Predictive C
1
0
(O)
May be inoperative provided: 1)Alternate procedures are established and used,and 2)GPWS windshear alert mode (Mode 7) is operative.
OPERATING PROCEDURES Flight Crewmember must refer to the winshear section, in the FCOM . prior to their first departure of the day.
22-60-03B
A
1
0
(O)(FD)
May be inoperativeprovided: 1)alternate procedures are estalished and used 2)Takeoff and landings are not condcuted in known or forecast windshear conditions, and 3)Repairs are made within three flight days.
OPERATING PROCEDURES Flight Crewmember must refer to the winshear section, in the FCOM prior to their first departure of the day.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.13 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-60
Flight Augmentation (FAC)
22-60-04
Yaw Damper System
22-60-04A
C
2
1
(O)(M) (FD)
One may be inoperative.
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. MAINTENANCE PROCEDURE Refer to AMM 27-26-00-040-001 22-70
Flight Management System (FMS)
22-70-01
22-70-01A
Flight Management System (FMS) C FMS 1 inoperative with IR 1 (NAV mode) or GPS 1 operative
2
1
(O)
The FMS 1 may be inoperative provided that: 1) Two MCDUs are operative, and 2) The IR 1 NAV mode or GPS 1 is operative. OPERATING PROCEDURES IN FLIGHT -
In the case of FMS 1+2 failure: MCDU NAV B/UP · · · · · · · · · · · · · · · · · · · · · · · · Use Refer to FCOM/DSC-22-20-60-130 (MCDU BACKUP NAVIGATION).
A320/321 MEL/CDL
01.22.14 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-70
Flight Management System (FMS)
22-70-01B
FMS 2 inoperative with IR 1 (NAV mode) or GPS 1 operative
C
2
1
(O)
The FMS 2 may be inoperative provided that the IR 1 NAV mode or GPS 1is operative.
OPERATING PROCEDURES Refer to MEL 22-70-01A
22-70-01C
22-70-02 22-70-02A
FMS 1 inoperative
C
2
1
C
2
0
The FMS1 may be inoperative provided that the flight remains within radio navaids coverage.
Navigation Database (O)(FD)
May be out of currency provided: 1)Current Aeronautical Charts are used to verify Navigation Fixes before dispatch, and 2)Procedures are established and used to verify status and suitability of Navigation Facilties used to define route of flight.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.22.15 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-70
Flight Management System (FMS)
22-70-02
Navigation Database
22-70-02A (cont’d)
OPERATING PROCEDURES 1. Both, pilots and dispatch must check the flight plan route against current aerounautical cfhart(s) and NOTAMs for suitability and serviceability of NAV Fixes. 2. Pilot must ensure that all applicable charts for enroute to destination and alternate(s) are available on board. 3. All required terminal and approach plates are available on board, and 4. Cross check FMGS waypoints using current fligh crew navigation charts.
22-70-03
Performance Information
22-70-03A
22-70-04 22-70-04A
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
Fuel/Time Prediction
A320/321 MEL/CDL
01.22.16 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-81
Flight Control Unit (FCU)
22-81-01
Auto Flight Control Panel (FCU)
22-81-01-01 AP Engagement pb 22-81-01-01A
B
2
1
One may be inoperative provided that the associated autopilot (AP) is considered inoperative. Refer to Item 22-10-01A Autopilot (AP)
22-81-01-01B
A
2
0
Both may be inoperative provided that both autopilots (AP) is considered inoperative. Refer to Item 22-10-01B Autopilot (AP)
22-81-01-02 A/THR Arming pb 22-81-01-02A
B
1
0
May be inoperative provided that the autothrust (A/THR) is considered inoperative. Refer to Item 22-30-01 Autothrust (A/THR)
22-81-01-03 Mode Engagement pb (LOC, EXPED, APPR) 22-81-01-03A
B
3
0
One or more may be inoperative.
3
3
Must be operative.
22-81-01-04 Selection knob (ALT, HDG-TRK, SPD-MACH) 22-81-01-04A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.17 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-81
Flight Control Unit (FCU)
22-81-01
Auto Flight Control Panel (FCU)
22-81-01-05
V/S-FPA Selection knob
22-81-01-05A
B
1
0
May be inoperative provided that operations do not required its use.
B
1
0
May be inoperative provided that the HDG-V/S selection is operative.
C
1
0
May be inoperative provided that the SPD selection is operative.
C
1
0
May be inoperative.
C
4
0
One or more may be inoperative provided that the associated indications are operative on both PFDs and both Nds.
22-81-01-06 HDG-V/S/TRKFPA Change Over pb 22-81-01-06A 22-81-01-07 SPD/MACH Change Over pb 22-81-01-07A 22-81-01-08 METRIC ALT pb 22-81-01-08A 22-81-01-09 Selection Window (SPDMACH, HDGTRK, ALT, V/SFPA) 22-81-01-09B
A320/321 MEL/CDL
01.22.18 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-81
Flight Control Unit (FCU)
22-81-02
EFIS Control Panel (FCU)
22-81-01-10 AP1, AP2 and A/THR pb light Bars 22-81-01-10A
C
3
0
One or more may be inoperative provided that the associated indication is operative on both PFDs.
C
3
0
One or more may be inoperative.
C
2
1
One may be inoperative.
C
2
1
One may be inoperative provided that the unit required for the intended flight is operative on both EFIS control panels.
2
2
Both must be operative.
22-81-01-11 Mode Engagement (LOC, EXPED, APPR) pb light Bars 22-81-01-11A 22-81-02-01 Baro Reference Display Window 22-81-02-01A 22-81-02-02 Baro Reference selector Outer Ring (in Hg/hPa) 22-81-02-02A
22-81-02-03 Baro Reference selector Inner knob 22-81-02-03A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.19 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-81
Flight Control Unit (FCU)
22-81-02
EFIS Control Panel (FCU)
22-81-02-04 FD pb 22-81-02-04A
B
2
1
One may be inoperative provided that the associated FD is considered inoperative. Refer to Item 22-10-02 Flight Director (FD)
22-81-02-05 LS pb 22-81-02-05A
C
2
1
One may be inoperative provided that the associated ILS is considered inoperative. Refer to Item 34-30-04 Instrument Landing System (ILS)
22-81-02-06 Optional Data (ARPT, NDB, VOR.D, WPT, CSTR) Display pb 22-81-02-06A
C
10
0
One or more may be inoperative.
B
2
1
One may be inoperative provided that the ND unit associated with the operative ND range selector is operative.
B
2
1
One may be inoperative provided that the ND unit associated with the operative ND mode selector is operative.
22-81-02-07 ND Range selector 22-81-02-07A
22-81-02-08 ND Mode selector 22-81-02-08A
A320/321 MEL/CDL
01.22.20 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-81
Flight Control Unit (FCU)
22-81-02
EFIS Control Panel (FCU)
22-81-02-09 ADF/VOR sw 22-81-02-09A
C
4
0
One or more may be inoperative provided that the associated ADF/VOR indication on ND is considered inoperative. Refer to Item 34-50-03A (ADF) Refer to Item 34-50-05A (VOR) Refer to Item 34-06-06 Radio Navaids Indications on the ND
22-81-02-10 LS and FD pb light Bars 22-81-02-10A
C
4
2
One per each side may be inoperative provided that the associated indication is displayed on both PFDs.
C
10
0
One or more may be inoperative.
C
2
1
One channel may be inoperative provided that Two RMPs, all DUs, both RAs, both LGCIUs, both FACs, both Automatic Cabin Pressure Control Systems, all ADIRUs and the ISIS Baro-altimeter function are operative.
22-81-02-11 Optional Data (ARPT, NDB, VOR.D, WPT, CSTR) Display pb light Bars 22-81-02-11A 22-81-03
FCU Channel
22-81-03-01 FCU Channel 22-81-03-01A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.21 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-82
Multipurpose Control and Display Unit (MCDU)
22-82-01
MCDU 1
22-82-01B
B
1
0
May be inoperative provided that: 1) The MCDU 2 is operative, and 2) The flight remains within radio navaids coverage.
22-82-02 22-82-02B
22-82-04
22-82-04A
MCDU 2 Flight within navaids coverage
B
1
0
May be inoperative provided that the flight remains within radio navaids coverage.
C
8
0
One or more may be inoperative.
MCDU Annunciator light
A320/321 MEL/CDL
01.22.22 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-83
Flight Management and Guidance Computer (FMGC)
22-83-01
22-83-01A
Flight Management and Guidance Computer (FMGC) FMGC 1 inoperative
A
2
1
(O)
One may be inoperative for three flight days provided that: 1)FMGC 1 is deactivated, 2) FMS 1 is considered inoperative, Refer to Item 22-70-01 Flight Management System (FMS), and 3)The terrain inoperative.
function
of
TAWS
is
considered
Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS) OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION - If FMGC 1 is affected: AUTO FLT/FMGC/1 (49VU B02 or 121VU M16) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull - If ADS-B is required for the intended flight: ATC selector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 - If FMGC 2 is affected: AUTO FLT/FMGC/2 (121VU M17) C/B· · · · · · · · · · Pull (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.22.23 AUTO FLIGHT
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
22 AUTO FLIGHT 22-83
Flight Management and Guidance Computer (FMGC)
22-83-01
22-83-01A
Flight Management and Guidance Computer (FMGC) FMGC 1 inoperative (Cont’d)
OPERATING PROCEDURES (Cont’d)
Note: During IR alignment, when the FMGC 2 is deactivated, IRS IN ALIGN memo cannot be displayed until the FD 1 is engaged. 22-83-01B
FMGC 2 inoperative
C
2
1
(O)
If ADS-B is required for the intended flight: ATC selector · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · 1 FMGC 2 may be inoperative provided that: 1) FMGC 2 is deactivated, and 2) FMS 2 is considered inoperative. Refer to Item 22-70-01 Flight Management System (FMS)
OPERATING PROCEDURES Refer to MEL 22-83-01A for operating procedure.
*
*
*
A320/321 MEL/CDL
01.22.24 AUTO FLIGHT 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.01 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-00
MAINTENANCE Message on the STATUS SD page
23-00-01
CIDS 1(2) MAINTENANCE Message
23-00-01A 23-01
C
1
-
CIDS 1(2) MAINTENANCE message may be displayed on the STATUS SD page.
C
1
0
May be inoperative.
AUTO Position C
1
0
Overhead Panels
23-01-01
RCDR Overhead Panel
22-01-01-01 RCDR GND CTL pb-sw ON light 23-01-01-01A 22-01-01-31 RCDR GND CTL pb-sw 22-01-01-31A
(O)
May be inoperative in the AUTO position. OPERATING PROCEDURES ON GROUND CVR can only be tested through the CVR test pb-sw during the first 5 minutes after supply of the aircraft electrical network.
22-01-01-31B
ON Position
C
1
0
(O)
May be inoperative in the ON position. OPERATING PROCEDURES AFTER LANDING -
22-01-01-31C
CVR Considered Inoperative
A
1
0
To stop CVR recording, if needed: COM/CVR/SPLY (49 VU E14) C/B · · · · · · · · · · · PULL
May be inoperative provided that the CVR is considered inoperative. Refer to Item 23-71-01 Cockpit Voice Recorder (CVR)
A320/321 MEL/CDL
01.23.02 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-01
Overhead Panels
23-01-01
RCDR Overhead Panel
23-01-01-32 CVR ERASE pb 23-01-01-32A
C
1
0
May be inoperative.
A
1
0
May be inoperative provided that the Cockpit Voice Recorder (CVR) is considered inoperative.
23-01-01-33 CVR TEST pb 23-01-01-33A
Refer to Item 23-71-01 Cockpit Voice Recorder (CVR) 23-01-02
CALLS Overhead Panel
23-01-02-31 CALLS ALL pb 23-01-02-31A
C
1
0
Use of C Passenger address system
1
0
May be inoperative.
23-01-02-32 CALLS EMER pb CALLS FWD pb, CALLS MID pb, CALLS EXIT pb, CALLS AFT pb 23-01-02-32A
(O)
May be inoperative provided that the passenger address system is used for communication between the cockpit and the cabin. OPERATING PROCEDURES PIC will brief cabin crew that he will use passenger address system for communications.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.03 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-01
Overhead Panels
23-01-02
CALLS Overhead Panel
23-01-02-32 CALLS EMER pb CALLS FWD pb, CALLS MID pb, CALLS EXIT pb, CALLS AFT pb
23-01-02-32B
Use of Cockpit C handset interphone
1
0
(O)
May be inoperative provided that the cockpit handset interphone is used for communication between the cockpit and the cabin.
OPERATING PROCEDURES
PIC will brief cabin crew that he will use cockpit handset interphone for communications.
A320/321 MEL/CDL
01.23.04 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-09
ECAM Alerts
23-09-01
COM HF 1(2) EMITTING Alert
23-09-01A 23-09-02 23-09-02A
Refer to Item 23-10-01 HF System COM VHF 1(2)(3) EMITTING Alert C
3
2
(O)
One may be displayed provided that : 1) The alert is confirmed to be false by troubleshooting, and 2) The affected VHF is deactivated and considered inoperative. Refer to Item 23-10-02 VHF System OPERATING PROCEDURES GENERAL INFORMATION To make troubleshooting easier, Refer to FCOM/PROABN-23 COM VHF 1(2)(3)/HF 1(2) EMITTING. DURING COCKPIT PREPARATION · To deactivate the VHF1 system, apply: COM/VHF/1 (49 VU G09) C/B . . . . . . . . . . . . . . . . PULL · To deactivate the VHF2 system, apply: COM NAV/VHF/2 (121 VU L04) C/B . . . . . . . . . . . PULL · To deactivate the VHF3 system, apply: COM NAV/VHF/3 (121 VU L05) C/B . . . . . . . . . . . PULL
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.05 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-10
Speech Communication
23-10-01
HF System
23-10-01A
23-10-02
1
1
(FD)
Must be operative on routes that require HF communication with ATSU, provided SATCOM Voice Mode is available for use by that unit.
C
1
0
(FD)
May be inoperative provided SATCOM Voice Mode is operative.
C
3
2
VHF System
23-10-02B
VHF 2 or VHF 3 may be inoperative. Note: The VHF 3 may be used as one of the VHFs required by regulations, provided that the VHF 3 is set to VOICE mode before each flight.
23-10-03
SATCOM Voice Mode
23-10-03A
23-13
1
1
(FD)
Must be operative on communication with ATSU.
C
1
0
(FD)
May be inoperative provided HF System and SELCAL Function are operative.
C
3
2
Radio Management
23-13-01
23-13-01B
Radio Management Panel (RMP) RMP 2 may be inoperative.
routes
that
require
HF
A320/321 MEL/CDL
01.23.06 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-13
Radio Management
23-13-02
RMP Selection Key
23-13-02A
C
3
2
One may be inoperative on each RMP provided that : 1) VHF 1 selection key is operative on RMP 1, and 2) If HF is required, HF 1 selection key is operative on RMP 1.
23-20
Data Transmission and Automatic Calling
23-20-01
Aircraft Communications Addressing Reporting System (ACARS)
23-20-01A
B
1
0
(O)(FD) May be inoperative provided altenate procedures are used. OPERATING PROCEDURES 1. Flight crew must transmit depature, enroute, and the arrival reports in accordance with the route manual communication requirement. 2. Flight crew must complete the in-flight performance data records if required.
cruise
NOTE: Any portion of the system that is operative may be used. 23-20-02 23-20-02A
SATCOM Data Mode B
1
0
May be inoperativeprovided operation or procedures do not requier its use.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.07 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-31
Passenger Address System
23-31-01
Passenger Address System
23-31-01A
1
1
Must be operative. Note: i.
In the case of partial failure of the passenger address system, refer to the item(s) of the affected system(s).
ii. Total failure of the passenger address system (indicated by the COM CIDS 1+2 FAULT alert displayed on the EWD) is not permitted. 23-40
Interphone
23-40-01
Ground External Horn
23-40-01A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES ON GROUND -
When the aircraft electrical network is supplied: Monitor the avionics equipment ventilation in the cockpit.
BEFORE LEAVING THE AIRCRAFT Set the three ADIRS Mode selectors to OFF. 23-40-02
23-40-02A
Flight Crew Interphone System 1
1
Must be operative for each person on cockpit duty.
A320/321 MEL/CDL
01.23.08 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-40
Interphone
23-40-03
Flight Crew to Ground Communication System
23-40-03A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES Instruct ground crew to connect to flight interphone jack and establish communications through flight interphone.
23-40-04
Service Interphone Jack
23-40-04A
C
8
0
(O)
One or more may be inoperative. OPERATING PROCEDURES Instruct ground crew to connect to flight interphone jack and establish communications through flight interphone.
23-51
Audio Management
23-51-01
SELCAL Function
23-51-01A
C
1
1
(FD)
Must be operative for dispatch from Kingdom on routes that require HF communication with ATSU and SATCOM Voice Mode must be operative.
1
0
(FD)
May be inoperative for dispatch back to Kingdom on routes that require HF communication with ATSU provided: 1) Crew continuously monitors HF communication, and 2) SATCOM Voice Mode is operative.
C
1
0
(FD)
May be inoperative provided SATCOM Voice Mode is operative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.09 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-51
Audio Management
23-51-02
Boomset
23-51-02A
A
2
0
May be inoperative provided: 1) Flight data recorder and hand mic are operative, and 2) Repaire are made within three flight days.
23-51-03
Hand Microphone
23-51-03A 23-51-04
23-51-05A
2
1
One may be inoperative provided both associated boom micrphones are operative.
C
2
1
Only F/O loudspeaker may be inoperative provided that at least one crewmember on cockpit duty wears a boomset compatible with the quick donning oxygen mask.
C
2
1
Cockpit Loudspeaker
23-51-04A
23-51-05
C
Cockpit Loudspeaker Volume Control (O)
Only F/O side may be inoperative provided that the affected crewmember on cockpit duty wears a boomset compatible with the quick donning oxygen mask.
OPERATING PROCEDURES Cockpit crew will be aware and prepared for monitoring communications during the flight.
A320/321 MEL/CDL
01.23.10 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-51-06
Sidestick PTT sw
23-51-06B
C
2
1
(M)
Only F/O side may be inoperative in the open position (non transmitting position) provided that the INT/RAD sw on CAPT ACP, on F/O ACP and on ACP 3 are operative. Note: Apply the maintenance procedure only when the operative sidestick radio selector is failed in the closed position (transmitting position). MAINTENANCE PROCEDURE Refer to AMM 23-51-00-040-001
23-52
Audio Control Panel (ACP)
23-52-01
CAPT and F/O ACP
23-52-01A
C
2
1
(O)
One may be inoperative provided that : 1) ACP 3 is operative, and 2) The AUDIO SWITCHING selector is operative. OPERATING PROCEDURES In order to recover audio channel on the affected side : AUDIO SWITCHING.................................CAPT 3 (F/O 3)
23-52-02 23-52-02A
ACP 3 C
1
0
May be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.11 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-52
Audio Control Panel (ACP)
23-52-03
Fourth Occupant ACP
23-52-03A 23-52-04
1
0
May be inoperative.
D
1
0
May be inoperative.
C
14 12
ACP in the Avionics Compartment
23-52-04A 23-52-05
C
ACP Transmission Key
23-52-05A
One may be inoperative on each ACP provided that : 1) VHF 1 transmission key is operative either on CAPT ACP or on F/O ACP, and 2) If HF is required, HF 1 transmission key is operative either on CAPT ACP or on F/O ACP.
23-52-06
ACP Reception knob
23-52-06A
C
16 14
One may be inoperative on each ACP provided that : 1) VHF 1 reception knob is operative either on CAPT ACP or on F/O ACP, and 2) If HF is required, HF 1 reception knob is operative either on CAPT ACP or on F/O ACP,and 3) If ILS is required for approach, one ILS reception knob is operative either on CAPT ACP or on F/O ACP.
23-52-07 23-52-07A
ACP Reception knob light C
14
0
May be inoperative.
A320/321 MEL/CDL
01.23.12 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-53
AUDIO SWITCHING Panel on the Center Pedestal
23-53-01
AUDIO SWITCHING selector
23-53-01A 23-71
C
1
0
May be inoperative.
A
1
0
May be inoperative provided:
Cockpit Voice Recorder (CVR)
23-71-01
Cockpit Voice Recorder (CVR)
23-71-01A
1) Flight Data Recorder (FDR) is operative, and 2) Repair is made within three flight days. 23-72
Cockpit Door Surveillance System (CDSS)
23-72-01
23-72-01A
Cockpit Door Surveillance System (CDSS) C
1
0
(O)(FD) May be inoperative provided: 1) An alternate means of viewing the area on the cabin side of the flight crew compartment is available and functions, 2) Alternate procedures are established and used of ensuring the security of the area outside the fligh crew compartment door, 3) With the forward camera inoperative, the cabin area in front of the cockpit must be illuminated when the cabin is in darkness, and 4) With the forward camera inoperative, an additional crew member must be assigned for duty in the cockpit. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.23.13 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-72
Cockpit Door Surveillance System (CDSS)
23-72-01
23-72-01A
Cockpit Door Surveillance System (CDSS) (Cont’d)
OPERATING PROCEDURES 1. When the forward camera which provides a view of the area directly in front of the cockpit is inoperative (camera 1), an additional crew member must be assigned for duty in the cockpit. 2. Before the cockpit door is opened, he/she must look through the door viewing lens, identify the person seeking admission and confirm with the PIC TO OPEN THE DOOR. 3. Ensure that the cabin ceiling light of the area in front of the cockpit door is operative and ON when requireed. 4. When any of the cameras 2, 3, inoperataive, another flight attendant must assure that the crew member/flight crew member required to enter the cockpit is not followed by passenger(s). Note: Any portion of the system which is operative may be used.
A320/321 MEL/CDL
01.23.14 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-01
Cabin Intercommunicatio n Data System (CIDS)
23-73-01-01Cabin Intercommunicatio n Data System (CIDS) Function 23-73-01-01A
1
1
(M)
The CIDS function must be operative. Note: i.
Failure of a single CIDS director is indicated by a MAINTENANCE message on the STATUS SD page. Refer to Item 23-00-01 MAINTENANCE Message
CIDS
1(2)
ii. In the case of disturbance of the CIDS function, the deactivation of the affected CIDS director may recover normal operation of the CIDS function. Refer to AMM TASK 23-73-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.15 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-02
DEU A
23-73-02-01 Cabin DEU A 23-73-02-01A
C
21
0
(O)
One or more may be inoperative and affected passenger seat may be occupied provided that : 1) The passenger announcement can be throughout the cabin during the flight, and
heard
2) The passenger address system is used to alert the passengers when "Return to Seat / Fasten Seat Belt / No Smoking" signs are requested. OPERATING PROCEDURES GENERAL INFORMATION On the affected cabin area: -
general cabin illumination is set to full brightness,
-
Passenger Call is not available,
-
The (No Smoking/Fasten Seat Belt/No Portable Electric Device) Signs are not available.
IN FLIGHT -
When return to seat is requested, or When seat belts should be fasten, or When smoking is prohibited, or When portable electric device use is prohibited, Use the passenger address system to alert cabin attendants and passengers.
A320/321 MEL/CDL
01.23.16 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-02
DEU A
23-73-02-01 Cabin DEU A 23-73-02-01B
C
21
0
(FD)
One or more may be inoperative provided that the affected seats are blocked and placarded inoperative.
C
3
2
(FD)
May be inoperative provided that the affected lavatory is closed and placarded inoperative.
23-73-02-02 Lavatory DEU A 23-73-02-02A
NOTE: In case foreword lavatory placarded extra pilot should be assigned to operate the flight as a safety pilot to relieve the pilot when leaving the cockpit for personal reasons. 23-73-03
DEU B
23-73-03-01 Cabin DEU B 23-73-03-01B
C
18
0
(O)
One or more may be inoperative provided that: 1) One DEU B and the associated handset are operative at each pair of floor level exit doors, and 2) The slide bottle pressure and door bottle pressure associated with each affected DEU B are checked on the associated direct reading pressure gauge before the first flight of each day, and
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.23.17 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-03
DEU B
23-73-03-01 Cabin DEU B 23-73-03-01B (cont’d)
3) The associated lavatory fire extinguisher system is checked operative, and 4) The absence of smoke in the affected lavatory is periodically checked. Refer to Item 25-62-06 Passenger Door Slide Pressure Message on the PTP/FAP (If Installed), and Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the PTP/FAP, and Refer to Item 26-17-01 Lavatory Smoke Detection System.
OPERATING PROCEDURES PIC will brief cabin crew for the use of one cabin handset per pair of floor level exit doors, if necessary. Define the cabin handset location to be used by the purser, if necessary.
A320/321 MEL/CDL
01.23.18 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-04
Cabin Individual Call
23-73-04-01 Passenger Call 23-73-04-01A
23-73-05
C
42
0
C
42
0
One or more may be inoperative.
Cabin Loudspeaker
23-73-05-01 Cabin Loudspeaker 23-73-05-01A
(FD)
One or more may be inoperative provided that no seat is occupied from which a passenger cannot hear a passenger announcement.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.19 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-05
Cabin Loudspeaker
23-73-05-02 Lavatory Loudspeaker 23-73-05-02A
C
3
0
(O)(FD) One or more may be inoperative provided lavatory is not used for passengers. It may used by crew member. OPERATING PROCEDURES Flight attendant must be briefed to assure that affected lavatory is not used by any passenger.
23-73-06
Handset
23-73-06-01 Cockpit Handset 23-73-06-01A
C
1
0
(A320)
C
3
2
(A321)
C
5
4
May be inoperative provided that the cockpit audio control panel (ACP) is used for the communication between the cockpit and the cabin.
23-73-06-02 Cabin Handset 23-73-06-02A
(O)
One may be inoperative provided that one handset is operative at each pair of floor level exit doors. OPERATING PROCEDURES 1. The PIC in his briefing must inform all crew members wich handset(s) is/are inoperative and the affected flight attendant(s) should use the next available operative station or communicat in person when the need arises. 2. FAIC must be seated in aposition having an operative handset during Takeoff & Landing.
A320/321 MEL/CDL
01.23.20 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-06
Handset
23-73-06-03 Cabin Handset Key 23-73-06-03A
C Passenger address and Cabin to cockpit interphone operative (A320)
3
(A321)
5
C
1
One or more may be inoperative provided that: 1) Passenger address from the affected handset is operative, and 2) Cabin to cockpit interphone from affected handset is operative.
3
23-73-06-03B
23-73-07
Refer to Item 23-73-06-02 Cabin Handset
Prerecorded Announcement and Music Reproducer (PRAM)
23-73-07-01 Prerecorded Announcement and Music Reproducer (PRAM) 23-73-07-01A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES Procedure to replace the perecorded announcement must be established and necessary demonstation equipment must be provided onboard.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.21 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-08
Cabin Assignment Module (CAM)
23-73-08-01 Cabin Assignment Module (CAM) 23-73-08-01A 23-73-10
C
1
0
C
1
0
May be inoperative or missing.
Smoke Detection Function
23-73-10-01 Smoke Detection Function (CIDSSDF) 23-73-10-01A
(FD)
May be inoperative provided that: 1) The cargo compartments are empty or do not contain flammable or combustible materials, and 2) The lavatory smoke detection system is considered inoperative. Refer to Item 26-17-01 Lavatory Smoke Detection System Note: Failure of a single CIDS-SDF channel is indicated by a MAINTENANCE message on the STATUS SD page. Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message
A320/321 MEL/CDL
01.23.22 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-73
Cabin Intercommunication Data System
23-73-10
Smoke Detection Function
23-73-10-01 Smoke Detection Function (CIDSSDF) 23-73-10-01B
C
1
0
May be inoperative provided that the restrictions concerning lavatory smoke detection system and cargo smoke detection system are applied. Refer to Item 26-17-01 Lavatory Smoke Detection System, and Refer to Item 26-16-01 Smoke Detector in the FWD Cargo Compartment (if FWD cargo compartment smoke detection system installed) and Refer to Item 26-16-02 Smoke Detector in the AFT and the BULK Cargo Compartments (if AFT cargo compartment smoke detection system installed). Note: Failure of a single CIDS-SDF channel is indicated by a MAINTENANCE message on the STATUS SD page. Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.23.23 COMMUNICATIONS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-74
Cabin Crew Panel
23-74-01
FAP Display Unit
23-74-01A
C
1
0
(O)
May be inoperative provided that the safety related messages on the FAP are considered inoperative. Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the PTP/FAP, and Refer to Item 25-62-06 Passenger Door Slide Pressure Message on the PTP/FAP (If Installed), and Refer to Item 25-62-07 Emergency Exit Slide Pressure Message on the PTP/FAP OPERATING PROCEDURES GENERAL INFORMATION The cabin lighting may be dimmed through the Additional Attendant Panel (AAP) (If available).
23-74-02
EMER pb on Hardkey FAP Sub-panel
23-74-02A 23-74-03
1
1
Must be operative.
D
1
0
May be inoperative.
(A320)
C
4
0
Refer to Item 52-10-06 DOOR PRESS LOW/CHECK DOOR PRESSURE Message on the PTP/FAP
(A321)
C
8
0
Other Controls on Hardkey FAP Sub-panel
23-74-03A 23-74-06
23-74-06A
Door Bottle Pressure Monitoring on the FAP
A320/321 MEL/CDL
01.23.24 COMMUNICATIONS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATIONS 23-74
Cabin Crew Panel
23-74-08
Slide Pressure Monitoring on the FAP
23-74-08A
Refer to Item 25-62-06 Passenger Door Slide Pressure Message on the PTP/FAP Refer to Item 25-62-07 Emergency Exit Slide Pressure Message on the PTP/FAP Note: Apply both MEL Items.
23-74-09
Area Call Panel
23-74-09A 23-74-10
23-74-11A
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
Attendant Information Panel (AIP)
23-74-10A 23-74-11
C
Additional Attendant Panel (AAP)
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.01 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-00
MAINTENANCE Messages on the STATUS SD page
24-00-01
DC BUS TIE MAINTENANCE Message
24-00-01A 24-00-03
1
-
DC BUS TIE MAINTENANCE message may be displayed on the STATUS SD page.
C
1
-
AC GEN MAINTENANCE message may be displayed on the STATUS SD page.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
3
1
One GEN pb-sw FAULT light and/or the APU GEN pb-sw FAULT light may be inoperative provided that the associated generator indications are operative on the ELEC SD page.
AC GEN MAINTENANCE Message
24-00-03A 24-01
C
Overhead Panels
24-01-01
ELEC Overhead Panel
24-01-01-01 BAT 1(2) pb-sw FAULT light 24-01-01-01A 24-01-01-02 BAT 1(2) pb-sw OFF light 24-01-01-02A 24-01-01-03 GEN pb-sw FAULT light and APU GEN pb-sw FAULT light 24-01-01-03A
A320/321 MEL/CDL
01.24.02 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-01
Overhead Panels
24-01-01
ELEC Overhead Panel
24-01-01-04 GEN pb-sw OFF light and APU GEN pb-sw OFF light 24-01-01-04A
C
3
0
One or more may be inoperative.
C
1
0
May be inoperative provided that the AC ESS bus indication is operative on the ELEC SD page.
C
1
0
May be inoperative provided that the AC ESS bus indication is operative on the ELEC SD page.
C
1
0
24-01-01-05 AC ESS FEED pb-sw FAULT light 24-01-01-05A 24-01-01-06 AC ESS FEED pb-sw ALTN light 24-01-01-06A 24-01-01-07 EXT PWR pb-sw AVAIL light 24-01-01-07A
(O)
May be inoperative. OPERATING PROCEDURES BEFORE PUSHBACK Confirm the external power disconnection either on the ELEC SD page or with the ground crew. PARKING -
If the APU is not available: - EXT PWR pb-sw . . . . . . . . . . . . . . . . . . . . . . . . ON - Confirm the external power connection either on the ELEC SD page or with the ground crew before engine shutdown.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.03 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-01
Overhead Panels
24-01-01
ELEC Overhead Panel
24-01-01-08 EXT PWR pb-sw ON light 24-01-01-08A
C
1
0
C
1
0
May be inoperative.
24-01-01-09 GALY & CAB pbsw FAULT light 24-01-01-09A
(O)
One may be inoperative provided that: 1) For each generator, the AC load indication is operative on the ELEC SD page, and 2) The GALY & CAB automatic load shed system is checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check of the galley automatic load shed system: -
Supply the electrical network from the APU or the external power.
-
GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO
-
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
-
Check that a part of the operative galley equipment does not operate.
-
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push Note: Disregard this procedure if main galleys are not connected.
A320/321 MEL/CDL
01.24.04 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-01
Overhead Panels
24-01-01
ELEC Overhead Panel
24-01-01-10 GALY & CAB pbsw OFF light 24-01-01-10A
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
2
1
One may be inoperative provided that the frequency and the temperature indications of the affected generator are operative on the ELEC SD page.
B
1
0
May be inoperative.
24-01-01-11 COMMERCIAL pb-sw OFF light 24-01-01-11A 24-01-01-12 BUS TIE pb-sw OFF light 24-01-01-12A 24-01-01-13 IDG pb-sw FAULT light 24-01-01-13A
24-01-02
EMER ELEC PWR Overhead Panel
24-01-02-01 RAT & EMER GEN FAULT light 24-01-02-01A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.05 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-07
Indications on the ELEC SD page
24-07-01
24-07-01A
AC Generation Indications on the ELEC SD page C
3
0
(O)
One or more indications related to the AC generation may be inoperative provided that: 1) The load, voltage, and frequency indications are operative on one engine driven generator , and 2) The associated ELEC GEN 1(2) FAULT alert is operative, and 3) The galley automatic load shed system is checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check that GEN 1(2) pb-sw FAULT light is on (with the GEN 1(2) pb-sw in the on position). Check of the galley automatic load shed system: -
Supply the electrical network from the APU or the external power.
-
GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO
-
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
-
Check that a part of the operative galley equipment does not operate.
-
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push Note: Disregard this procedure if main galleys are not connected. (Cont’d on next page)
A320/321 MEL/CDL
01.24.06 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-07
Indications on the ELEC SD page
24-07-02
DC Generation Indications on the ELEC SD page (Cont’d)
24-07-02A 24-07-03
2
0
One or more indications related to the DC generation may be inoperative.
C
1
0
May be displayed.
C
1
0
AC ESS BUS SHED Indication on the ELEC SD page
24-07-03A 24-09
C
ECAM Alerts
24-09-01 24-09-01A
ELEC AC ESS BUS SHED Alert (O)
May be displayed provided that: 1) The alert is confirmed to be false by troubleshooting, and 2) The AC ESS BUS SHED is checked operative before each flight, and 3) HF 1 is deactivated. Refer to Item 23-10-01 HF System OPERATING PROCEDURES GENERAL INFORMATION When the ELEC AC ESS BUS SHED alert is displayed on the EWD: -
The AC ESS BUS SHED message may appear on the ELEC SD page,
-
The CAPT AOA message may be displayed in the INOP SYS column on the STATUS SD page, (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.07 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-09
ECAM Alerts
24-09-01 24-09-01A
ELEC AC ESS BUS SHED Alert (Cont’d)
OPERATING PROCEDURES(Cont’d) -
The ELEC/AC BUS/8XP/MONG (49VU H11) C/B may trip.
DURING COCKPIT PREPARATION COM/HF1 (49VU HA14) C/B · · · · · · · · · · · · · · · · · Pull Check of the AC ESS BUS SHED: - Supply the electrical network from the APU or the external power. - Check that the CAPT right DU is operative. IN FLIGHT -
If either the ANTI ICE F/O AOA alert or the ANTI ICE F/O PROBES alert is displayed on the EWD, and icing conditions cannot be avoided: - ADR 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF - AIR DATA sw . . . . . . . . . . . . . . . . . . . . . . . . . . F/O 3 Note: If the ADR 2 pb-sw is set to OFF, takeoff in CONF 1+F is not permitted.
-
24-09-02 24-09-02A
If either the ANTI ICE STBY AOA alert or the ANTI ICE STBY PROBES alert is displayed on the EWD, and icing conditions cannot be avoided: ADR 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
C/B TRIPPED Alert C
1
0
(M)
May be displayed provided that the alert is confirmed to be false by troubleshooting. MAINTENANCE PROCEDURE Refer to AMM 24-50-00-040-001
A320/321 MEL/CDL
01.24.08 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-22
AC Main Generation
24-22-01
24-22-01A
AC Main Generation (IDG, GCU, Line Contactor) B
2
1
(O)(M) One may be inoperative provided that: (FD) 1) The flight altitude is limited to 33 000 ft, and 2) The APU and AC auxiliary generation are operative and used throughout the flight, and 3) The APU fuel pump is operative, and 4) The APU oil consumption is checked adequate for the intended flight, and 5) All busses have power, and 6) The indications and alerts for the remaining AC main generation and the AC auxiliary generation are operative, and 7) The galley automatic load shed system is checked operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS landing capability is CAT II. APU fuel consumption with APU GEN pb-sw On: FL
GND
200
250
300
335
390
KG/H
100
63
57
54
49
42
Note: When the External Power is disconnected, the IFE is lost until the APU supplies the electrical network. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.24.09 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-22
AC Main Generation
24-22-01
24-22-01A
AC Main Generation (IDG, GCU, Line Contactor) (Cont’d)
OPERATING PROCEDURES(Cont’d) DURING COCKPIT PREPARATION Check of the galley automatic load shed system: -
Supply the electrical network from the APU or the external power.
-
GALY & CAB pb-sw · · · · · · · · · · · · · · · · · · · · · · AUTO
-
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
-
Check that a part of the operative galley equipment does not operate.
-
ELEC/GALY & CAB/GND/FLT/LOGIC (122VU S24) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Push Note: Disregard this procedure if main galleys are not connected. (Cont’d on next page)
A320321 MEL/CDL
01.24.10 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-22
AC Main Generation
24-22-01
24-22-01A
AC Main Generation (IDG, GCU, Line Contactor) (Cont’d)
OPERATING PROCEDURES(Cont’d) AFTER ENGINE START Check that the electrical busses have power: -
APU MASTER SW pb-sw · · · · · · · · · · · · · · · · · · · · ON
-
APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
GEN 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
GEN 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
On the ELEC SD page, check that all AC busses have power.
-
GEN pb-sw (operative)· · · · · · · · · · · · · · · · · · · · · · · On
-
APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
On the ELEC SD page, check that all AC busses have power.
-
APU GEN pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · On Note: If necessary, disconnected.
the
IDG
may
be
CAUTION For economical reason, the IDG should not operate for more than 50 flight hours in the disconnected mode. MAINTENANCE PROCEDURE Refer to AMM 24-20-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.11 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-22
AC Main Generation
24-22-02
AC Bus Tie Control Function
24-22-02A 24-23
1
1
Must be operative.
AC Auxiliary Generation
24-23-01
AC Auxiliary Generation (APU Generator, GCU, Line Contactor)
Note: When the GPCU and the APU Generator are both inoperative, the engines cannot be started.
24-23-01A
C
1
0
May be inoperative provided that the APU GEN pb-sw is set to OFF.
24-23-01B
A
1
0
May be inoperative for four flights provided that the APU GEN pb-sw is set to OFF.
1
1
Must be operative.
1
0
24-24
AC Emergency Generation
24-24-01
Emergency Generator
24-24-01A 24-24-02
24-24-02A
RAT Extension Automatic Control B
(M)
May be inoperative provided that the RAT extension manual control is checked operative every day. MAINTENANCE PROCEDURE Refer to AMM 24-20-00-040-002
A320/321 MEL/CDL
01.24.12 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-24
AC Emergency Generation
24-24-03
RAT Extension Manual Control
24-24-03A 24-25
B
1
0
C
1
0
May be inoperative.
AC Essential Generation Switching
24-25-01
Manual Transfer to the AC BUS 2 (ALTN Function)
24-25-01A
(O)
May be inoperative provided that: 1) The AC ESS FEED pb-sw is set to NORM, and 2) It is checked on the ELEC SD page that the AC BUS 1 supplies the AC ESS BUS, and 3) The TR 2 is operative. OPERATING PROCEDURES DURING PRELIMINARY COCKPIT PREPARATION On the ELEC SD page, check that the AC BUS 1 supplies the AC ESS BUS.
24-25-02
24-25-02A
Automatic Transfer to the AC BUS 2 C
1
0
(O)
May be inoperative provided that: 1) The AC ESS FEED pb-sw is set to NORM, and 2) It is checked on the ELEC SD page that the AC BUS 1 supplies the AC ESS BUS, and 3) The TR 2 is operative. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.13 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-24
AC Emergency Generation
24-25-02
Automatic Transfer to the AC BUS 2
24-25-02A
(Cont’d)
OPERATING PROCEDURES DURING PRELIMINARY COCKPIT PREPARATION On the ELEC SD page, check that the AC BUS 1 supplies the AC ESS BUS.
24-26
Galley and Commercial Supply System
24-26-01
GALY & CAB Automatic Load Shed System
24-26-01A
Manual Load Shed System Operative
C
1
0
24-26-01B
All GALY & CAB Loads disconnected
C
1
0
May be inoperative provided that the manual load shed system and the GALY & CAB pb-sw FAULT light are operative.
(M)
May be inoperative provided that all GALY & CAB loads are disconnected. MAINTENANCE PROCEDURE Refer to AMM 24-56-00-040-001
A320/321 MEL/CDL
01.24.14 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-26
Galley and Commercial Supply System
24-26-02
24-26-02A
GALY & CAB Manual Load Shed System (GALY & CAB pb-sw) All GALY & CAB loads disconnected
C
1
0
(M)
May be inoperative provided that all GALY & CAB loads are disconnected. MAINTENANCE PROCEDURE Refer to AMM 24-56-00-040-002
24-26-02B
COMMERCIAL C supply system operative
1
0
(O)(M) May be inoperative provided that the COMMERCIAL supply system is checked operative. OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
If the AVNCS SMOKE emergency procedure is applied or if the AVIONICS SMOKE alert is displayed on the EWD replace the action to set the GALY & CAB pb-sw to OFF by the following actions: - EMER EXIT LT selector . . . . . . . . . . . . As required - COMMERCIAL pb-sw . . . . . . . . . . . . . . . . . . . OFF Note: When the COMMERCIAL pb-sw is set to OFF, the normal cabin lighting goes off. Minimum cabin lighting is recovered when the EMER EXIT LT selector is set to ON.
MAINTENANCE PROCEDURE Refer to AMM 24-51-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.15 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-26
Galley and Commercial Supply System
24-26-03
Commercial Supply System
24-26-03A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
If the AVNCS SMOKE emergency procedure is applied or if the AVIONICS SMOKE alert is displayed on the EWD replace the action to set the COMMERCIAL pb-sw to OFF by the following actions: - BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF - GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF The F/O PFDU, the F/O NDU, and the ECAM lower display are lost. - If the smoke persists: - GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On When the GEN 2 pb-sw is set to on, all the electrical busses are recovered but the TR 2 remains inoperative - BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . AUTO Before the landing gear extension: - GEN 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On When the GEN 2 pb-sw is set to on, all the electrical busses are recovered but the TR 2 remains inoperative - BUS TIE pb . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
24-28-01 24-28-01A
Static Inverter AC Generation 1
1
Must be operative.
A320/321 MEL/CDL
01.24.16 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-32
DC Main Generation (TR 1, TR 2)
24-32-01
24-32-01A
DC Main Generation (TR 1, TR 2) TR1 inoperative A
2
1
(O)(FD) TR 1 may be inoperative provided repairs are made within two flight days. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING PRELIMINARY COCKPIT PREPARATION TR 1/CNTOR/SPLY (125VU CF01) C/B · · · · · · · · · Pull On the ELEC SD page, check that the TR 2 and the ESS TR voltages are both equal to or above 27 V. On the battery voltage indicator, check that the BAT 1 and the BAT 2 voltages are both equal to or above 25.5 V. The batteries must be set to OFF during this check.
24-32-01B
TR 2 inoprative A
2
1
(O)(M) TR 2 may be inoperative provided that: (FD) 1) The AC ESS FEED control is checked operative every day, and 2) The ISIS airspeedindication is operative, and 3) The ISIS altitude indication is operative, and 4) The ISIS aircraft attitude indication is operative, and 5) The standby compass is operative, and 6) Repairs are made with two flight days. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.17 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-32
DC Main Generation (TR 1, TR 2)
24-32-01
DC Main Generation (TR 1, TR 2)
24-32-01B
(Cont’d)
OPERATING PROCEDURES(Cont’d) DURING PRELIMINARY COCKPIT PREPARATION TR 2/CNTOR/SPLY (124VU BC01) C/B· · · · · · · · · Pull On the ELEC SD page, check that the TR 1 and the ESS TR voltages are both equal to or above 27 V. On the battery voltage indicator, check that the BAT 1 and the BAT 2 voltages are both equal to or above 25.5 V. The batteries must be set to OFF during this check. AC ESS FEED pb-sw · · · · · · · · · · · · · · · · · · · · · ALTN IN FLIGHT -
In the case of failure of the AC BUS 2, all DUs are lost. In this case: AC ESS FEED pb-sw· · · · · · · · · · · · · · · · · · · · · · Norm
-
In the case of failure of the AC BUS 1: RAT MAN ON pb-sw (on HYD overhead panel)....................................................................Set
MAINTENANCE PROCEDURE Refer to AMM 24-30-00-040-002 24-34
DC Emergency Generation (ESS TR)
24-34-01
24-34-01A
DC Emergency Generation (ESS TR) 1
1
Must be operative.
A320/321 MEL/CDL
01.24.18 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-35
DC Essential and Normal Generation Switching
24-35-01
DC TIE Contactor 1PC1 (DC BUS 1-DC BAT BUS), 4PC (DC ESS BUSDC BAT BUS)
24-35-01A 24-35-02
C
1
One may be inoperative in the open position.
1
1
Must be operative.
2
2
Must be operative.
DC TIE Contactor 1PC2 (DC BUS 2-DC BAT BUS)
24-35-02A 24-38
2
DC Battery Generation
24-38-01 24-38-01A
BAT 1(2) Channel
12 FEB 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.24.19 ELECTRICAL POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-38
DC Battery Generation
24-38-02
Battery Charger Limiter (BCL)
24-38-02A
A
2
1
(O)(M) One may be inoperative for 10 flights provided that: (FD) 1) No APU start is attempted neither on ground nor in flight, and 2) Both AC main generations are operative, and 3) The refueling is made with an external power unit connected, and 4) The battery associated with the inoperative BCL is charged before each flight. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Do not use the APU. Use a ground power unit to start the engines on ground. DURING PRELIMINARY COCKPIT PREPARATION -
If BAT 1 is affected: BAT 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
If BAT 2 is affected: BAT 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
MAINTENANCE PROCEDURE Refer to AMM 24-30-00-040-001 24-38-03 24-38-03A
Battery Voltmeter C
2
0
One or both may be inoperative provided that the associated voltage indication is operative on the ELEC SD page.
A320/321 MEL/CDL
01.24.20 ELECTRICAL POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
24 ELECTRICAL POWER 24-41
AC External Power Control
24-41-01
Ground Power Control Unit (GPCU)
24-41-01A
C
1
0
May be inoperative provided APU Generator is operative. Note: When the GPCU and the APU Generator are both inoperative, the engines cannot be started.
24-41-02 24-41-02A
External Power Receptacle C
1
0
(M)
May be inoperative provided that the receptacle is placarded inoperative and not used. Note: When the GPCU and the APU Generator are both inoperative, the engines cannot be started. MAINTENANCE PROCEDURE Refer to AMM 24-41-00-040-001
*
*
*
A320/321
01.25.01 EQUIPMENT/ FURNISHINGS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-07
Indications on the DOOR/OXY SD page
25-07-01
Passenger Door Slide Permanently Indicated Armed (A320)
25-07-01A
(M)
Note: The correct indication may be recovered by performing the AMM task 52-70-00040-07.
C
4
0
(O)
One or more may be permanently indicated in the armed position provided that the associated slide is visually checked to be armed before each flight. OPERATING PROCEDURES ON GROUND Cabin crew must confirm before each flight that the associated slide is armed.
25-07-01
25-07-01A
Cabin Passenger Door / Emergency Exit Slide Permanently Indicated Armed (A321)
(M)
Note: The correct indication may be recovered by performing the AMM task 52-70-00040-07.
C
8
0
(O)
One or more may be permanently indicated in the armed position provided that the associated slide is visually checked to be armed before each flight. OPERATING PROCEDURES ON GROUND Cabin crew must confirm before each flight that the associated slide is armed.
A320/321
01.25.02 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-07
Indications on the DOOR/OXY SD page
25-07-02
25-07-02A
Passenger Door Slide Permanently Indicated Not Armed (A320) Associated door considered operative
(M)
Note: The correct indication may be recovered by performing the AMM task 52-70-00040-07.
C
4
0
(O)(FD) One or more may be permanently indicated in the not armed position provided that: 1) The aircraft is not operated at night, and 2) The associated slide is visually checked to be armed before each flight. OPERATING PROCEDURES ON GROUND Cabin crew must confirm before each flight that the associated slide is armed.
25-07-02
25-07-02A
Cabin Passenger Door / Emergency Exit Slide Permanently Indicated Not Armed (A321) Associated door considered operative
C
8
0
(O)(FD) One or more may be permanently indicated in the not armed position provided that: 1) The aircraft is not operated at night, and 2) The associated slide is visually checked to be armed before each flight. OPERATING PROCEDURES ON GROUND Cabin crew must confirm before each flight that the associated slide is armed.
A320/321
01.25.03 EQUIPMENT/ FURNISHINGS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-07
Indications on the DOOR/OXY SD page
25-07-03
Overwing Emergency Exit Slide Permanently Indicated Armed
25-07-03A
Note: The correct indication may be recovered by performing the AMM task 52-70-00040-07. C
2
0
(M)
One or both may be permanently indicated in the armed position provided that the associated slide is visually checked to be armed before the first flight of the day. MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-008
25-07-04
25-07-04A
Overwing Emergency Exit Slide Permanently Indicated Not Armed Overwing emergency exits considered operative
Note: The correct indication may be recovered by performing the AMM task 52-70-00040-07. C
2
0
(M)(FD) One or both may be permanently indicated in the not armed position provided that: 1) The aircraft is not operated at night, and 2) The associated slide is visually checked to be armed before the first flight of the day. MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-009
A320/321
01.25.04 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-11
Pilot Seats
25-11-01
Pilot Seat Manual Horizontal Adjustment
25-11-01A 25-11-02
2
2
Both must be operative.
Pilot Seat Manual Vertical Adjustment
25-11-02A
Associated electrical control operative
C
2
0
One or both may be inoperative provided that the associated electrical control is operative.
25-11-02B
Associated electrical control inoperative
C
2
0
One or both may be inoperative provided that the seating position is acceptable to the affected crewmember.
C
2
0
25-11-03
Pilot Seat Recline Adjustment
25-11-03A
(M)
One or both may be inoperative provided that the seat is secured in an upright position acceptable to the affected crewmember. MAINTENANCE PROCEDURE Refer to AMM 25-11-00-040-001
25-11-04
25-11-04A
Pilot Seat Other Manual Adjustments C
2
0
One or more may be inoperative provided that the seating position is acceptable to the affected crewmember.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.05 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-11
Pilot Seats
25-11-05
Pilot Seat Electrical Adjustment
25-11-05A
C
2
0
(M)
One or both may be inoperative provided that the electrical adjustment of the associated seat is deactivated. MAINTENANCE PROCEDURE Refer to AMM 25-11-00-040-002
25-11-06 25-11-06A
Pilot Seat Shoulder Harness A
2
1
(O)(FD) May be inoperative on the F/O seat for three flights. OPERATING PROCEDURES BEFORE TAKEOFF The takeoff briefing should include the status of the affected seat and the position to be adopted by the F/O in the case of RTO. To cope with any potential RTO: The F/O must tightly fasten operative harness strap. DURING FLIGHT For any phase of flight in turbulence atmosphere: The F/O must fasten the belts accordingly. BEFORE LANDING The landing briefing should include the status of the affected seat and the position to be adopted by the F/O in the case of high deceleration at landing. To cope with any potential high deceleration at landing: The F/O must tightly fasten operative harness straps.
A320/321
01.25.06 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-11
Pilot Seats
25-11-07
Pilot Seat Fifth Strap
25-11-07A
C
2
0
(O)
One or both may be inoperative. OPERATING PROCEDURES DURING FLIGHT To cope with any potential turbulence situation: The crewmember of the affected seat must tightly fasten the operative harness straps.
25-11-08
Pilot Sidestick Armrest Height Adjustment
25-11-08A
25-11-09
25-11-10A
2
1
One may be inoperative provided that the associated armrest position is acceptable to the affected crewmember.
C
2
1
One may be inoperative provided that the associated armrest position is acceptable to the affected crewmember.
C
2
0
One or both may be inoperative.
Pilot Sidestick Armrest Pitch Adjustment
25-11-09A
25-11-10
C
Pilot Sidestick Armrest Memory Position Display
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.07 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-11
Pilot Seats
25-11-11
Pilot Inboard Armrest Vertical Adjustment
25-11-11A 25-11-12
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
1
0
(FD)
May be inoperative provided that the seat is in its stowed position.
C
1
0
(FD)
May be inoperative provided that the seat is not occupied during takeoff and landing.
Pilot Seat Headrest
25-11-12A 25-12
C
Third and Fourth Occupant Seats
25-12-01 25-12-01A 25-12-02
25-12-02A
Third Occupant Seat Seat stowed Third Occupant Seat Shoulder Harness
A320/321
01.25.08 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-12
Third and Fourth Occupant Seats
25-12-03
Third Occupant Seat Abdominal Belt
25-12-03A
C
1
0
(FD)
May be inoperative provided that: 1) The seat is placarded inoperative, and 2) The seat is not occupied.
25-12-04
Third Occupant Seat Fifth Strap
25-12-04A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES With any potential turbulance situation the crewmember must lightly fasten the operative straps.
25-12-05 25-12-05A 25-12-06
Fourth Occupant Seat Seat stowed
25-12-07A
1
0
May be inoperative provided that the seat is in its stowed position.
C
1
0
(FD)
May be inoperative provided that the seat is not occupied during takeoff and landing.
C
1
0
(FD)
May be inoperative provided that:
Fourth Occupant Seat Shoulder Harness
25-12-06A 25-12-07
C
Fourth Occupant Seat Abdominal Belt
1) The seat is placarded inoperative, and 2) The seat is not occupied.
A320/321
01.25.09 EQUIPMENT/ FURNISHINGS
MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-12
Third and Fourth Occupant Seats
25-12-08
Fourth Occupant Seat Fifth Strap
25-12-08A
D
1
0
(O)
May be inoperative. OPERATING PROCEDURES With any potential turbulance situation the crewmember must lightly fasten the operative straps.
25-13
Lining and Furnishings
25-13-01
Pilot Sliding Table
25-13-01A 25-13-02
25-20-01
C
2
0
One or both may be inoperative in its stowed position.
C
4
0
One or more may be inoperative in its stowed position.
Pilot Retractable Footrest
25-13-02A 25-20
Table stowed
Footrest stowed
Cabin Seats Passenger Seat
25-20-01A (A320)
C 132 86 C 116 70
(A321)
C 165 100
(FD)
May be inoperative provided: a) Seat does not block and Emergency Exit, b) seat does not restrict any passenger from access to the main aircraft aisle, and c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”. Note 1: A seat with an inoperative seat belt is considered inoperative. (Cont’d on next page)
A320/321
01.25.10 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-20
Cabin Seats
25-20-01 25-20-01A
Passenger Seat (Cont’d)
Note 2: Inoperative seats do not affect the required number of Flight Attendants.
Note 3: Affected seat(s) may include the seat(s) behind and/or adjacent outboard seats.
25-20-03
Cabin Attendant Seat
Note: A cabin attendant seat with an inoperative or missing seat belt or harness should be considered inoperative. (Cont’d on next page)
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.11 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-20
Cabin Seats
25-20-03 25-20-03B
Cabin Attendant Seat (cont’d) Required C cabin attendant seat (A320)
5
4
(O)(M) One required cabin attendant seat may be inoperative or (FD) not usable provided that: 1) The cabin attendant assigned to affected seat occupies a passenger seat as close to or closer than nearest seated passenger to the associated exit, and 2) The passenger seat to be used by cabin attendant is correctly placarded, and
(A321)
C
7
5
3) The cabin attendant can reach assigned exit and emergency equipment in nearly the same time as from normally assigned seat, and 4) The direct view of passenger cabin by flight attendants is not impaired, and 5) The alternate procedures are established for displaced flight attendant according to national regulations, and 6) The affected seat is secured in its stowed position or removed. OPERATING PROCEDURES Captin brief all cabin crew regarding the passenger seat that occupie by assigned flight attendant. MAINTENANCE PROCEDURE Refer to AMM 25-22-00-040-001
A320/321
01.25.12 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-28
Overhead Storage
25-28-01
Overhead Storage Bin(s)/Cabin and Galley storage Compartment/ Closets
25-28-01A
(A320)
C
74
68 (M)
May be inoperative provided:
(A321)
C
87
80
a) Associated bin or compartment is placarded DO NOT USE, b) Any emergency equipment located in affected compartment is removed or considered inoperative, and c) Cabin crew must be notified NOTE: These provisions are not intended to prohibit inspections by crew members. MAINTENANCE PROCEDURE Refer to AMM 25-20-00-040-001
25-35
Galley Equipment
25-35-01
25-35-01A
Galley Waste Compartment Flapper Door C
3
0
(O)(M) One or more may be inoperative or missing provided that: 1) The galley waste compartment is empty, and 2) The associated access is secured in the closed position to prevent waste introduction. Note: Non-safety related galley equipment is not listed in this MEL. (Cont’d on next page)
A320/321
01.25.13 EQUIPMENT/ FURNISHINGS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-35
Galley Equipment
25-35-01
Galley Waste Compartment Flapper Door
25-35-01A (cont’d)
OPERATING PROCEDURES Inform cabin crew to essure adequate galley waste storage capacity is maintained during periods of flight when affected containers are secured empty. MAINTENANCE PROCEDURE Refer to AMM 25-35-00-040-001
25-40
Lavatories
25-40-01
25-40-01A
Toilet Waste Compartment Flapper Door C
3
2
(O)(M) One may be inoperative or missing provided that: (FD) 1) The toilet waste compartment is empty, and 2) The associated access is secured in the closed position to prevent waste introduction. Note: Non-safety related toilet equipment is not listed in this MEL. OPERATING PROCEDURES -
Lavatory door placarded “INOPERATIVE-DO NOT ENTER”.
-
Lavatory is used only by crew members.
-
Ensure that affected lavatory is kept locked and is not entered exept for crew member.
MAINTENANCE PROCEDURE Refer to AMM 25-40-00-040-001
A320/321
01.25.14 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-40
Lavatories
25-40-02
Exterior Lavatory Ashtray
25-40-02A
D
4
0
One or more may be damaged or missing provided that the flight is non-smoking.
25-40-03A
Lavatory fire C extinguishing system operative
3
0
One or more may be damaged or missing provided that the associated lavatory fire extinguishing system is operative.
25-40-03B
Lavatory C locked closed
3
2
(FD)
One may be damaged or missing provided that the associated lavatory is locked closed and placarded inoperative.
2
0
(FD)
May be inoperative provided Ramp Load Control Supervisor must check and confirm to the flight crew that cargo compartments are loaded normally.
25-40-03
25-50
Interior Lavatory Ashtray
Cargo Compartments
25-50-01 25-50-01A
Cargo Loading System D
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.15 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-50
Cargo Compartments
25-50-02
Decompression Panels in the Cargo Compartments
25-50-02A
25-50-03
25-50-03A
25-50-04
25-50-04A
C
23 0
(FD)
One or more may be damaged or missing provided that the associated cargo compartment is empty or does not contain flammable or combustible materials.
C
41 0
(FD)
One or more may be damaged provided that the associated cargo compartment is empty or does not contain flammable or combustible materials.
C
5
Sidewall Linings and Ceiling Panels in the Cargo Compartments Damaged panel Cargo Compartment Restraint Components (Nets, Attach Points, Stanchions) 0
One or more may be missing or damaged provided that the remaining operative ones are enough to secure the load in the affected compartment.
A320/321
01.25.16 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
4.
25 EQUIPMENT/FURNISHINGS 25-62
Cabin Escape Facilities
25-62-01
25-62-01A
25-62-02
25-62-02A
25-62-03
25-62-03A
NUMBER REQUIRED FOR DISPATCH
Cabin Passenger Door Slide or Slide Raft Slide inoperative
4
4
2
2
4
4
Overwing Emergency Exit Slide or Slide Raft (A320) Slide inoperative
Emergency Exit Slide or Slide Raft (A321) Slide inoperative
REMARKS OR EXCEPTIONS
12 FEB 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.17 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-62
Cabin Escape Facilities
25-62-04
SLIDE ARMED light (A320)
25-62-04A 25-62-04
6
0
One or more may be inoperative provided maintenance confirm that it’s only lit problem.
C
8
0
One or more may be inoperative provided maintenance confirm that it’s only lit problem.
4
4
Must be attached to each required life raft for over water flying.
4
0
SLIDE ARMED light (A321)
25-62-04A 25-62-05
C
Survival Kit
25-62-05A 25-62-06
25-62-06A
Passenger Door CHECK SLIDE PRESSURE Message on Flight Attendant Panel (FAP) (A320) C
(M)
One or more messages may be displayed provided that the slide bottle pressure is checked before the first MMEL dispatch and then every 600 flight hours or every 4 months, whichever occurs first. MAINTENANCE PROCEDURE Refer to AMM 25-62-00-040-009
A320/321
01.25.18 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-62
Cabin Escape Facilities
25-62-06
Passenger Door CHECK SLIDE PRESSURE Message on Flight Attendant Panel (FAP) (A321)
25-62-06A
C
8
0
(M)
One or more messages may be displayed provided that the slide bottle pressure is checked before the first MMEL dispatch and then every 600 flight hours or every 4 months, whichever occurs first. MAINTENANCE PROCEDURE Refer to AMM 25-62-00-040-009
25-62-07
25-62-07A
Overwing Emergency Exit CHECK SLIDE PRESSURE Message on Flight Attendant Panel (FAP) (A320) Check of the slide bottle pressure
C
2
0
(M)
One or both messages may be displayed provided that the associated slide bottle pressure is checked before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 25-62-00-040-005
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.19 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-62
Cabin Escape Facilities
25-62-08
Overwing Escape Life Line
25-62-08B
25-63
Non extended C overwater flight
2
0
(FD)
One or both may be inoperative or missing provided that extended overwater flight is not conducted.
1
0
(O)
May be inoperative.
Evacuation Signaling Equipment
25-63-01
25-63-01A
Emergency Evacuation Signaling System (COMMAND pbsw, HORN SHUT OFF pb, CAPT&PURS and CAPT sw) B
OPERATING PROCEDURES GENERAL INFORMATION If necessary, the information will be given through the passenger address system or the cabin interphone system.
A320/321
01.25.20 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-64
First Aid Equipment
25-64-01 25-64-01A
First Aid Kit A
3
2
One may be incomplete, missing or used provided: 1) Affected FAK is identifiable as a unit that could not be mistaken for a fully serviceable unit, and 2) Repairs or replacements are made within 3 flight cycles. Note: - One serviceable Firs Aid Kit is required on ferry flights. - A first Aid Kit is considered serviceable when Kit contains the following contents Adhesive bandage compresses, 1-inch
16
Antiseptic swabs Ammonia inhalants Bandage compresses, 4-inch Triangular bandage compresses, 4-inch Arm splint, non inflatable Leg splint, non inflatable Roller bandage, 4-inch Adhesive tape, 1-inch standard roll
20 10 8 5 1 1 4 2
Bandage scissors
1
Protective latex gloves or equivalent nonpermeable gloves
1 Pair
A320/321
01.25.21 EQUIPMENT/ FURNISHINGS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-64
First Aid Equipment
25-64-02 25-64-02A
Emergency Medical Kit 1
1
Must be carried for all passenger flight. Must also be carried for ferry flights where the aircraft is being repositioned for a passenger flight.
Note: Ferry flight terminating in JED do not require the Doctor’s Emergency Kit. In addition, ferry flight to other stations besides Jeddah do not requir the Doctor’s Emergency Kit if advance coordination is none to ensure that a Doctro’s Emergency Kit is available at the terminatijng station to be installed prior to the aircraft resuming passenger service.
A320/321
01.25.22 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-64
First Aid Equipment
25-64-03
25-64-03A
Automated External Defibrillator (AED)
1
1
(M)
Must be carried for all passenger flights. MAINTENANCE PROCEDURES: Refer to maintenance task.
30 JUN 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.25.23 EQUIPMENT/ FURNISHINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-65
Emergency Equipment
25-65-01
Cockpit Flashlight
25-65-01A
25-65-02
0
May be inoperative or missing provided flight deck member assigned to associated station has a flashlight with equivalent characteristics readily available.
C
6
0
May be inoperative or missing provided cabin crewmember assigned to associated seat has a flashlight with equivalent characteristics readily available.
1
1
Must be available.
Crash Axe/Crowbar
25-65-03A 25-65-04
4
Cabin Flashlight
25-65-02A
25-65-03
C
Emergency Locator Transmitter (ELT)
25-65-04A
Survival Type ELTs
1
1
25-65-04B
Fixed ELTs
1
1
Must be operative.
A320/321
01.25.24 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-64
First Aid Equipment
25-65-05
Fireproof Gloves
25-65-05A
All damaged or missing
25-65-05B
One available
25-65-06
C
1
One may be damaged or missing.
1
1
One must be available.
2
2
Must be available and operative.
Megaphone
25-65-06A 25-66
2
Floatation and Survival Equipment
25-66-01 25-66-01A
25-66-02 25-66-02A
Life Vest (A320)
C 125 125 (FD) C 154 154
(A321)
C 180 180
Life vest required for all over water flight , and a life vest must be available for each passenger and crew on board.
Supplementary Life Raft C
1
1
(FD)
Must be available for all over water flight.
A320/321
01.25.25 EQUIPMENT/ FURNISHINGS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-70
Non-Essential Equipment & furnishings
25-70-01
Non-Essential Equipment & furnishings (NEF)
25-70-01A
25-70-01B 25-70-01C 25-70-01D 25-70-01E 25-70-01F 25-70-01J
Coffee Makers Ovens Air Chillers Hot Cups Hot Jugs
D 17
9
(FD)
Nonessential Equipment & Furnishings (NEF) are those items installed on the aircrfaft as part of the original certification, supplemental type certificate, or engineering order that have no effect on the safe operation of flight and would not be required by the applicable certification rules or operational rules. They are those items that if inoperative, damaged or missing have no effect on the aircraft ability to be operated safely under all operational conditions. these Nonessential items may be installed in areas including, but not limited to, the passenger compartment, flight deck area,service areas, cargo areas,crew rest areas,lavatories, and galley areas. Items addressed elsewhere in this MEL are not included.
5 6 2 1 1 2
3 4 1 0 0 1
(FD)
Any number or combination of galley equipment may be inoperative provided the in-flight supervisor/purser is notified and determines that the operative galley equipment available is adequate to support the associated passenger service throughout the flight(s).
D D D D D Bun Warmers D
Note: Captain will brief the FAIC of the location of the inoperative galley equipment, not to use the inoperative galley equipment and that the inoperative galley oven(s) must remain empty.
A320/321
01.25.26 EQUIPMENT/ FURNISHINGS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
25 EQUIPMENT/FURNISHINGS 25-70
Non-Essential Equipment & furnishings
25-70-04
Movie/stereo Equipment
25-70-04A
25-70-05 25-70-05A
D
1
0
Overhead Readig Lamp (A320)
C 116 C 132
0 0
(A321)
C 165
0
Any number may be inoperative
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.01 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-00
MAINTENANCE Message on the STATUS SD page
26-00-01
SMOKE MAINTENANCE Message
26-00-01A 26-01
C
1
-
SMOKE MAINTENANCE message may be displayed on the STATUS SD page.
C
16
8
A maximum of four bulbs or LEDs may be inoperative in each ENG FIRE-PUSH pb-sw.
One inoperative C on each engine
4
2
Overhead Panels
26-01-01
FIRE Overhead Panel
26-01-01-01 Bulb/LED in the ENG FIRE-PUSH pb-sw 26-01-01-01A 26-01-01-02 ENG AGENT pb DISCH light 26-01-01-02A
(M)
One may be inoperative on each engine provided that the associated bottle is checked before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-21-00-040-001
26-01-01-02B
One inoperative A on one engine
4
2
(M)
Both may be inoperative on one engine for four flights or 15 flight hours, whichever occurs first, provided that the associated bottles are checked before each flight. MAINTENANCE PROCEDURE Refer to AMM 26-21-00-040-001
A320/321 MEL/CDL
01.26.02 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-01
Overhead Panels
26-01-01
FIRE Overhead Panel
26-01-01-03 ENG AGENT pb SQUIB light 26-01-01-03A
C
4
2
(M)
One may be inoperative for each engine provided Engine extinguishing system firing circuit is checked operative before the first flight of the day. MAINTENANCE PROCEDURE Refer to AMM 26-21-00-040-003
26-01-01-04 Bulb/LED in the APU FIRE-PUSH pb-sw 26-01-01-04A
A maximum of four bulbs or LEDs inoperative
C
8
4
26-01-01-04B
Five or more bulbs or LEDs inoperative
C
8
0
A maximum of four bulbs or LEDs may be inoperative.
(M)
Five or more bulbs or LEDs may be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
26-01-01-05 APU AGENT pb DISCH light 26-01-01-05A
Check of bottle C pressure
1
0
(M)
May be inoperative provided that the bottle is checked before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-004
26-01-01-05B
APU deactivated
C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.03 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-01
Overhead Panels
26-01-01
FIRE Overhead Panel
26-01-01-06 APU AGENT pb SQUIB light 26-01-01-06A
C
1
0
(M)
May be inoperative provided that the APU extinguishing system firing circuit is checked operative before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-005
26-01-01-06B
C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
26-01-01-31 ENG FIRE TEST pb 26-01-01-31
C
2
1
(M)
One may be inoperative provided that the associated engine fire extinguishing and detection systems are checked operative before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-21-00-040-002
A320/321 MEL/CDL
01.26.04 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-01
Overhead Panels
26-01-01
FIRE Overhead Panel
26-01-01-32 APU FIRE TEST pb 26-01-01-32A
Daily check
C
1
0
(M)
May be inoperative provided that the APU extinguishing system firing circuit and the bottle low pressure detection system are checked operative before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-012
26-01-01-32B
APU deactivated
C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
26-01-01-33 APU FIRE PUSH pb-sw 26-01-01-33A
C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
26-01-01-34 APU AGENT pb 26-01-01-34A
C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.05 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-01
Overhead Panels
26-01-02
CARGO SMOKE Overhead Panel
26-01-02-01 CARGO SMOKE DISCH light 26-01-02-01A
Check of bottle C weight
2
0
(M)
May be inoperative provided that the associated bottle weight is checked before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-23-00-040-001
26-01-02-01B
26-12
26-12-01
Associated bottle considered inoperative
B
2
1
May be inoperative provided that the associated bottle is considered inoperative. Refer to Item 26-23-01 Cargo Agent Bottle
Engine Fire and Overheat Detection Engine Fire Detection Loop A on the Engine 1
26-12-01
C
1
0
One may be inoperative provided that: 1) The associated detection loop B is operative, and 2) The engine fire test is made before each flight.
26-12-02
26-12-02
Engine Fire Detection Loop A on the Engine 2 C
1
0
May be inoperative provided that the engine fire test is made before each flight.
A320/321 MEL/CDL
01.26.06 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-12
Engine Fire and Overheat Detection
26-12-03
Engine Fire Detection Loop B on the Engine 1
26-12-03A 26-12-04
0
May be inoperative provided that the engine fire test is made before each flight.
C
1
0
One may be inoperative provided that the engine fire test is made before each flight.
C
2
0
One or both may be inoperative.
C
1
0
One may be inoperative provided that:
FIRE light on the ENG MASTER Panel
26-12-05A 26-13
1
Engine Fire Detection Loop B on the Engine 2
26-12-04A 26-12-05
C
APU Fire and Overheat Detection
26-13-01
26-13-01A
APU Fire Detection Loop A
1) The associated detection loop B is operative and, 2) The APU fire test is made before each APU start, and 3) During APU operations on ground, APU condition is continuously monitored in the cockpit.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.07 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-13
APU Fire and Overheat Detection
26-13-01
APU Fire Detection Loop A
26-13-01B
C
1
0
26-13-02A
C
1
0
26-13-02B
C
1
0
(M)
A
1
0
(O)(FD) May be inoperative.
26-13-02
26-15
(M)
One may be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
APU Fire Detection Loop B One may be inoperative provided that the APU fire test is made before each APU start. One may be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
Avionics Compartment Smoke Detection
26-15-01
26-15-01A
Avionics Smoke Detection System
OPERATING PROCEDURES ON GROUND OR IN FLIGHT Disregard the BLOWER pb-sw FAULT light and the CAB FANS pb-sw FAULT light illuminated on the VENTILATION overhead panel. IN FLIGHT In the case of an electrical smoke: Apply the AVNCS SMOKE emergency procedure. Refer to the QRH/ABN-26-FIRE PROTECTION.
A320/321 MEL/CDL
01.26.08 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-16
Cargo Compartment Smoke Detection
26-16-01
Smoke Detector in the FWD Cargo Compartment (A320)
Note: i.
The cargo smoke detection function is part of the CIDS Smoke Detection Function (CIDS-SDF). Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
ii. Failure of a single detector in the cavity is indicated by a MAINTENANCE message on the STATUS SD page. Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message iii. Depending on applicable regulation, smoke detection system may be required for dispatch. 26-16-01A
Empty FWD cargo compartment
C
2
0
(O)(FD) Both detectors in the cavity may be inoperative provided that the FWD cargo compartment is empty. OPERATING PROCEDURES Refer to item 26-16-01D for operating procedure.
26-16-01D
Check of liner integrity
B
2
0
(O)(FD) Both detectors in the cavity may be inoperative provided procedure are established and used to verify associated cargo compartment remains empty or contains only empty cargo containers, cargo handling equipment, pallets, ballast (ballast may be loaded in ULD's). OPERATING PROCEDURES Ramp Load Control Supervisor to physically check and confirm to the flight crew that cargo compartment(s) are either empty or only contain empty cargo containers, pallets, cargo restraint components
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
26 FIRE PROTECTION 26-16
01.26.09 FIRE PROTECTION
REMARKS OR EXCEPTIONS
Cargo Compartment Smoke Detection
26-16-01
Smoke Detector in the FWD Cargo Compartment (A321)
Note: i.
The cargo smoke detection function is part of the CIDS Smoke Detection Function (CIDS-SDF). Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
ii. Failure of a single detector in the cavity is indicated by a MAINTENANCE message on the STATUS SD page. Refer to SDCU/SMOKE Message
26-16-01A
B
4
0
Item 26-00-01 MAINTENANCE
(O)(FD) Both detectors in one or both cavities may be inoperative provided that the FWD cargo compartment is empty or does not contain flammable or combustible materials.
OPERATING PROCEDURES Ramp Load Control Supervisor to physically check and confirm to the flight crew that cargo compartment(s) are either empty or only contain empty cargo containers, pallets, cargo restraint components
A320/321 MEL/CDL
01.26.10 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-16
Cargo Compartment Smoke Detection
26-16-02
Smoke Detector in the AFT and the BULK Cargo Compartments (A321)
Note: i.
The cargo smoke detection function is part of the CIDS Smoke Detection Function (CIDS-SDF). Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
ii. Failure of a single detector in the cavity is indicated by a MAINTENANCE message on the STATUS SD page. Refer to Item 26-00-01 SDCU/SMOKE MAINTENANCE Message
26-16-02A
B
6
0
(O)(FD) Both detectors in one or more cavities may be inoperative provided that the AFT and the BULK cargo compartments are empty or do not contain flammable or combustible materials.
OPERATING PROCEDURES Ramp Load Control Supervisor to physically check and confirm to the flight crew that cargo compartment(s) are either empty or only contain empty cargo containers, pallets, cargo restraint components
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.11 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-16
Cargo Compartment Smoke Detection
26-16-02
Smoke Detector in the AFT and the BULK Cargo Compartments (A320)
26-16-02C
C
4
2
(O)
Both detectors in one or both cavities may be inoperative provided that the AFT cargo ventilation is closed. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Life animal not allowed to be on associated cargo. DURING COCKPIT PREPARATION AFT ISOL VALVE pb-sw . . . . . . . . . . . . . . . . . . . . OFF
26-16-02E
Check of liner integrity
B
4
0
(O)
Both detectors in one or both cavities may be inoperative provided that: 1) The liner integrity in the AFT and the BULK cargo compartments is checked before each flight, and 2) The AFT cargo ventilation is closed. OPERATING PROCEDURES Refer to MEL item 26-16-02C
A320/321 MEL/CDL
01.26.12 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-17
Lavatory Smoke Detection
26-17-01
Lavatory Smoke Detection System
Note: The lavatory smoke detection function is part of CIDS Smoke Detection Function (CIDS-SDF). Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
26-17-01A
Associated lavatory fire extinguishing system operative
C
3
1
(O)
One or two may be inoperative provided that: 1) The associated lavatory fire extinguishing system is operative, and 2) A procedure is used to periodically check absence of smoke in the associated lavatory. OPERATING PROCEDURES PIC request the cabin purser to Ensure that the affected lavatory is inspected and checked by crewmembers periodically during flight.
26-17-01B
Associated lavatory not used
C
3
2
(O)(FD) One may be inoperative provided that: 1) The associated lavatory waste receptacle is empty, and 2) The associated lavatory door is locked closed and placarded inoperative, and 3) The lavatory is not used for storage or for any other purpose, and 4) A procedure is used to periodically check the absence of smoke in the associated lavatory. 5) Refer to the NOTE in Operating Procedure (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.13 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-17
Lavatory Smoke Detection
26-17-01
Lavatory Smoke Detection System
26-17-01B
Associated lavatory not used (cont’d)
OPERATING PROCEDURES The associated lavatory is periodacally checked for the absence of smoke by crewmembers.
NOTE: In case foreword lavatory placarded extra pilot should be assigned to operate the flight as a safety pilot to relieve the pilot when leaving the cockpit for personal reasons.
26-22
APU Fire Extinguishing
26-22-01
26-22-01A
APU Automatic Fire Extinguishing Control on Ground APU operations C on ground monitored
1
0
May be inoperative provided that the APU condition is continuously monitored in the cockpit during APU operations on ground .
A320/321 MEL/CDL
01.26.14 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-22
APU Fire Extinguishing
26-22-02
26-22-02A
APU Fire Extinguisher Overpressure Indication (Red Disc)
C APU Fire extinguisher bottle pressure switch operative
1
0
(M)
May be damaged or missing provided that the APU fire extinguisher bottle pressure switch is checked operative before the fist flight of each day.
MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-007
26-22-02B
APU deactivated
C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.15 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-22
APU Fire Extinguishing
26-22-03
26-22-03A
Squib of the APU Fire Extinguisher Bottle One inoperative
C
2
1
(M)
One may be inoperative provided that the remaining squib is checked operative before the fist flight of each day. MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-008
26-22-03B
Both inoperative
C
2
0
(M)
Both may be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
26-22-04
26-22-04A
APU Fire Extinguisher Bottle C
1
0
(M)
May be inoperative provided that the APU is deactivated. Refer to Item 49-10-01C Power Plant (APU)
A320/321 MEL/CDL
01.26.16 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-22
APU Fire Extinguishing
26-22-05
APU AUTO EXTING TEST pb-sw on the Maintenance Panel
26-22-05A
C
1
0
May be inoperative provided that the APU automatic fire extinguishing control on ground is considered inoperative. Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground
26-22-06
26-22-06A
26-22-06B
APU FIRE light on the External Power Panel APU Automatic C fire extinguishing control on ground operative
1
APU Automatic C fire extinguishing control on ground considered inoperative
1
0
(M)
May be inoperative provided that the APU automatic fire extinguishing control on ground is checked operative. MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-010
0
May be inoperative provided that the APU automatic fire extinguishing control on ground is considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.17 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-22
APU Fire Extinguishing
26-22-07
APU SHUT OFF pb on the External Power Panel
26-22-07A
26-22-07B
APU Automatic C fire extinguishing control on ground operative
1
APU Automatic C fire extinguishing control on ground considered inoperative
1
0
(M)
May be inoperative provided that the APU automatic fire extinguishing control on ground is checked operative. MAINTENANCE PROCEDURE Refer to AMM 26-22-00-040-011
0
May be inoperative provided that the APU automatic fire extinguishing control on ground is considered inoperative.
Refer to Item 26-22-01 APU Automatic Fire Extinguishing Control on Ground 26-23
26-23-01
Cargo Compartment Fire Extinguishing Cargo Agent Bottle
Note: The cargo smoke detection function is part of CIDS Smoke Detection Function (CIDS-SDF). Refer to Item 23-73-10-01 Smoke Detection Function (CIDS-SDF)
(Cont’d on next page)
A320/321 MEL/CDL
01.26.18 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-23
Cargo Compartment Fire Extinguishing
26-23-01
26-23-01A
Cargo Agent Bottle (cont’d)
No flammable C or combustible materials
1
0
(O)(FD) May be inoperative provided that the cargo compartments are empty or do not contain flammable or combustible materials.
OPERATING PROCEDURES Ramp Load Control Supervisor to physically check and confirm to the flight crew that cargo compartment(s) are either empty or only contain empty cargo containers, pallets, cargo restraint components.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.26.19 FIRE PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-23
Cargo Compartment Fire Extinguishing
26-23-02 26-23-02A
Squib of the Cargo Bottle 1 No flammable C or combustible materials
2
0
(O)(FD) One or both may be inoperative provided that the associated cargo compartment is empty or does not contain flammable or combustible materials. OPERATING PROCEDURES Ramp Load Control Supervisor to physically check and confirm to the flight crew that cargo compartment(s) are either empty or only contain empty carfo containers, pallets, cargo restraint components.
26-24-01 26-24-01A
Portable Fire Extinguisher C
4
3
One may be inoperative in the cabin or missing provided: 1) Inoperative fire extinguisher is tagged inoperative, removed from installed location, and placed out of sight so it cannot be mistaken for a functional unit, and 2 ) Required distribution is maintained. Note: The fire extnguisher located in the cockpit must always be operative.
A320/321 MEL/CDL
01.26.20 FIRE PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
26 FIRE PROTECTION 26-24
Portable Fire Extinguisher
26-25
Lavatory Fire Extinguishing
26-25-01
Lavatory Waste Bin Fire Extinguishing System
26-25-01A
C
3
0
26-25-01B
C
3
2
One or more may be inoperative provided associated lavatory smoke detection system is operative. (O)(M) One may be inoperative provided: (FD) 1) Lavatory waste receptacle is emty, 2) Lavatory door is locked closed and placarded " "INOPERATVIE DONT ENTER", and 3) lavatory is used only by crewmembers. 4) Refer to the NOTE in Operating Procedure. NOTE: These provisos are not intented to prohibit lavatory use or inspection by crewmembers. OPERATING PROCEDUERS Ensure that the affected lavatory is kept locked and is not entered except for inspection by crewmembers. NOTE: In case foreword lavatory placarded extra pilot should be assigned to operate the flight as a safety pilot to relieve the pilot when leaving the cockpit for personal reasons. *
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.01 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-00
MAINTENANCE Messages on the STATUS SD page
27-00-01
F/CTL MAINTENANCE Message
27-00-01A 27-00-02
1
-
F/CTL MAINTENANCE message may be displayed on the STATUS SD page.
C
1
-
SFCS MAINTENANCE message may be displayed on the STATUS SD page.
C
2
1
One may be inoperative.
C
2
0
One or both may be inoperative.
C
3
2
One may be inoperative.
SFCS MAINTENANCE Message
27-00-02A 27-01
C
Overhead Panels
27-01-01
FLT CTL Overhead Panel
27-01-01-01 ELAC pb-sw FAULT light 27-01-01-01A 27-01-01-02 ELAC pb-sw OFF light 27-01-01-02A 27-01-01-03 SEC pb-sw FAULT light 27-01-01-03A
A320/321 MEL/CDL
01.27.02 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-01
Overhead Panels
27-01-01
FLT CTL Overhead Panel
27-01-01-04 SEC pb-sw OFF light 27-01-01-04A 27-07
C
3
0
One or more may be inoperative.
C
4
0
One or more may be inoperative.
C
2
1
Indications on SD pages
27-07-01
Aileron Actuator Indication on the F/CTL SD page
27-07-01A 27-07-02
27-07-02A
Aileron Position Indication on the F/CTL SD page (O)(FD) One may be inoperative provided that the deflection of the affected aileron through each servo-control is visually checked before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.03 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-02
27-07-02A
Aileron Position Indication on the F/CTL SD page (Cont’d)
OPERATING PROCEDURES(Cont’d) -
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the aileron control through the ELACs: Put the aircraft in the test configuration: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON - ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On - ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On Check of the aileron control through the ELAC 1: - Move the CAPT stick from right stop to left stop. - Visually check the full travel of the ailerons. CAUTION If the expected aileron movement does not occur, do not attempt any reset. Contact the maintenance. (Cont’d on next page)
A320/321 MEL/CDL
01.27.04 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-02
27-07-02A
Aileron Position Indication on the F/CTL SD page (Cont’d)
OPERATING PROCEDURES(Cont’d) Check of the aileron control through the ELAC 2: -
ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF
-
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
-
Visually check the full travel of the ailerons. CAUTION
If the expected aileron movement does not occur, do not attempt any reset. Contact the maintenance. Return to normal configuration:
27-07-03
27-07-03A
-
YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off
-
BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . Off
-
ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
Elevator Actuator Indication on the F/CTL SD page C
4
0
One or more may be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.05 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-04
27-07-04A
Elevator Position Indication on the F/CTL SD page C
2
1
(O)
One may be inoperative provided that the deflection of the affected elevator is visually checked before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the elevator control: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON (Cont’d on next page)
A320/321 MEL/CDL
01.27.06 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-04
27-07-04A
27-07-05
27-07-05A
Elevator Position Indication on the F/CTL SD page (Cont’d)
OPERATING PROCEDURES (Cont’d) -
Establish communication with the ground crew.
-
Move the CAPT or the F/O stick to the maximum nose down position.
-
Visually check that both elevators move down.
-
Move the CAPT or the F/O stick to the maximum nose up position.
-
Visually check that both elevators move up.
-
Move the CAPT or the F/O stick to the neutral position.
-
Visually check that both elevators go back to the neutral position.
-
YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off
-
BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . Off
Pitch Trim Position Indication on the F/CTL SD page C
1
0
(O)
May be inoperative provided that the pitch trim handwheel and the stabilizer are visually checked to synchronously operate before each flight. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.07 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-05
27-07-05A
Pitch Trim Position Indication on the F/CTL SD page (Cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the stabilizer control: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - Establish communication with the ground crew. - Move the pitch trim handwheel to the full DN position. - Visually check that the stabilizer moves to the full down position. - Move the pitch trim handwheel to the full UP position. - Visually check that the stabilizer moves to the full up position. - Move the pitch trim handwheel to the required position. - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
A320/321 MEL/CDL
01.27.08 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-06
27-07-06A
Rudder Position Indication on the F/CTL SD page B
1
0
(O)
May be inoperative provided that the deflection of the rudder is visually checked before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
Check of the rudder control: -
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
Establish communication with the ground crew.
-
On the CAPT or the F/O side, apply left rudder.
-
Visually check that the rudder moves to the left.
-
On the CAPT or the F/O side, apply right rudder.
-
Visually check that the rudder moves to the right.
-
On the CAPT or the F/O side, release the pedals.
-
Visually check that the rudder moves to the neutral position.
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.09 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-07
Rudder Trim Position Indication on the F/CTL SD page
27-07-07A
C Rudder trim position indication operative on the center pedestal
1
0
May be inoperative provided that the rudder trim position indication is operative on the center pedestal .
27-07-07B
Rudder position C checked at zero
1
0
May be inoperative provided that the rudder position is checked at zero on the F/CTL SD page before takeoff.
C
1
0
May be inoperative.
C
2
1
One may be inoperative.
C
3
0
One or more may be inoperative.
27-07-08
Rudder Travel Limiter Position Indication on the F/CTL SD page
27-07-08A 27-07-09
ELAC Indication on the F/CTL SD page
27-07-09A 27-07-10
27-07-10A
SEC Indication on the F/CTL SD page
A320/321 MEL/CDL
01.27.10 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-11
27-07-11A
Spoilers/ Speedbrakes Indication on the F/CTL SD page C
10 0
(O)
One or more may be inoperative provided that the deflection of the affected surface is visually checked before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available:
-
-
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If surface 1 indication is inoperative: CAUTION The aircraft must be stopped during the check. -
YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON
-
PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
-
SPEEDBRAKES lever . . . . . . . . . . . . . . . . . . FULL
-
Visually check that surface 1 slightly extends (approximately 6°). (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.11 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-11
27-07-11A
Spoilers/ Speedbrakes Indication on the F/CTL SD page (Cont’d)
OPERATING PROCEDURES(Cont’d) - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . Off -
If surface 3 indication is inoperative: - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON - Move the stick from left stop to right stop. - Visually check the correct movement of surface 3. - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off
-
If surface 2, 4, or 5 indication is inoperative: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - Move the stick from left stop to right stop and visually check the correct movement of surfaces 2, 4 and 5. - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
27-07-12
27-07-12A
Spoilers/ Speedbrakes Indication on the WHEEL SD page C
10
0
(O)
One or more may be inoperative provided that the deflection of the affected surface is visually checked before each flight. (Cont’d on next page)
A320/321 MEL/CDL
01.27.12 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-12
27-07-12A
Spoilers/ Speedbrakes Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available:
-
-
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If surface 1 indication is inoperative: CAUTION The aircraft must be stopped during the check. -
YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON
-
PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
-
SPEEDBRAKES lever . . . . . . . . . . . . . . . . . . FULL
-
Visually check that surface 1 slightly extends (approximately 6°).
-
YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . Off (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.13 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-07
Indications on SD pages
27-07-12
Spoilers/ Speedbrakes Indication on the WHEEL SD page
27-07-12A
(Cont’d)
OPERATING PROCEDURES(Cont’d) -
If surface 3 indication is inoperative: - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON - Move the stick from left stop to right stop. - Visually check the correct movement of surface 3. - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off
-
If surface 2, 4, or 5 indication is inoperative: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - Move the stick from left stop to right stop and visually check the correct movement of surfaces 2, 4 and 5. - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
27-08
Indications on the EWD
27-08-01
Flap Position Indication on the EWD
27-08-01A 27-08-02
27-08-02A
1
1
Must be operative.
1
1
Must be operative.
Slat Position Indication on the EWD
A320/321 MEL/CDL
01.27.14 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-14
Aileron and Hydraulic Actuation
27-14-01
27-14-01A
Left Aileron Blue Servo-Control (Controlled by ELAC 1) A
1
0
(O)(M) May be inoperative provided that: 1) It is electrically disconnected, and 2) It remains mechanically connected and hydraulically supplied (damping function is not affected), and 3) The left aileron green servo-control (controlled by ELAC 2) is operative, and 4) The right aileron blue servo-control (controlled by ELAC 2) is operative, and 5) All roll spoilers are operative, and 6) The TR 1 and TR 2 are operative, and 7) The DC TIE contactor 1PC1 is checked closed, and 8) Repaire with in three flight days. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check that DC TIE contactor 1 is closed: -
Supply the electrical network from the APU or the external power.
-
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
MAINTENANCE PROCEDURE Refer to AMM 27-14-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.15 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-14
Aileron and Hydraulic Actuation
27-14-02
Left Aileron Green ServoControl (Controlled by ELAC 2)
27-14-02A
C
1
0
(M)
May be inoperative provided that: 1) It is electrically disconnected, and 2) It remains mechanically connected and hydraulically supplied (damping function is not affected), and 3) All roll spoilers are operative. MAINTENANCE PROCEDURE Refer to AMM 27-14-00-040-001
27-14-03
27-14-03A
Right Aileron Green ServoControl (Controlled by ELAC 1) A
1
0
(O)(M) May be inoperative provided that: 1) It is electrically disconnected, and 2) It remains mechanically connected and hydraulically supplied (damping function is not affected), and 3) The right aileron blue servo-control (controlled by ELAC 2) is operative, and 4) The left aileron green servo-control (controlled by ELAC 2) is operative, and 5) All roll spoilers are operative, and 6) The TR 1 and TR 2 are operative, and 7) The DC TIE contactor 1PC1 is checked closed, and 8) Repaire with in three flight days. (Cont’d on next page)
A320/321 MEL/CDL
01.27.16 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-14
Aileron and Hydraulic Actuation
27-14-03
27-14-03A
Right Aileron Green ServoControl (Controlled by ELAC 1) (Cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION Check that DC TIE contactor 1 is closed: -
Supply the electrical network from the APU or the external power.
-
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
MAINTENANCE PROCEDURE Refer to AMM 27-14-00-040-001 27-14-04
27-14-04A
Right Aileron Blue ServoControl (Controlled by ELAC 2) C
1
0
(M)
May be inoperative provided that: 1) It is electrically disconnected, and 2) It remains mechanically connected and hydraulically supplied (damping function is not affected), and 3) All roll spoilers are operative. MAINTENANCE PROCEDURE Refer to AMM 27-14-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.17 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-21
Rudder Mechanical Control
27-21-01
Rudder Pedal Adjustment System
27-21-01A
C
2
1
(O)
One may be inoperative provided that: 1) The rudder pedals can be secured in a position which meets individual pilot requirements, and 2) The full and unrestricted movement of the rudder pedals and brake pedals deflection is possible at both pilot stations. OPERATING PROCEDURES DURING COCKPIT PREPARATION Simultaneously apply loads on both pedals (in rudder control movement direction) to make sure that the secured position is reached. For that purpose, the effort shall be equivalent to a full rudder deflection.
27-22
Rudder Trim Actuation
27-22-01 27-22-01A
Rudder Trim System Rudder trim system 1 inoperative
C
2
1
(O)
Rudder Trim System 1 may be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II.
27-22-01B
Rudder trim system 2 inoperative
C
2
1
(O)
Rudder Trim System 2 may be inoperative. OPERATING PROCEDURES Refer to MEL item 27-22-01A
A320/321 MEL/CDL
01.27.18 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-22
Rudder Trim Actuation
27-22-02
Manual Rudder Trim Reset Function
27-22-02A 27-22-03
0
May be inoperative provided that one rudder trim position indication is operative.
C
1
0
May be inoperative.
C
2
1
One may be inoperative.
4
4
All must be operative.
Artificial feel and rudder travel limiting actuation
27-23-01
Rudder Travel Limiter System (Including Rudder and Pedals Travel Limiter Units)
27-23-01A 27-34
1
Rudder Trim Position Indication on the Center Pedestal
27-22-03A 27-23
C
Elevator and Hydraulic Actuation
27-34-01 27-34-01A
Elevator ServoControl
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.19 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-34
Elevator and Hydraulic Actuation
27-34-02
Elevator ServoControl Position Transducer
27-34-02A
C
4
2
(M)
One transducer per servo-control must be operative. MAINTENANCE PROCEDURE Refer to AMM 27-34-00-040-001
27-40
Trimmable Horizontal Stabilizer (THS)
27-40-01
Stabilizer Mechanical Control
27-40-01A 27-40-02
1
1
Must be operative.
Stabilizer Actuator Electric Motor
27-40-02A
Electric motor 3 C inoperative
3
2
The stabilizer actuator electrical motor 3 may be inoperative.
27-40-02-B
Electric motor 2 C inoperative
3
2
The stabilizer actuator electric motor 2 may be inoperative provided that ELAC 1 pitch channel is considered inoperative. Refer to Item 27-93-01 ELAC 1
A320/321 MEL/CDL
01.27.20 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
27-51
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
Flaps Electrical Control and Monitoring
27-51-01 27-51-01A
SFCC Flap Channel B
2
1
(O)(M) SFCC 2 flap channel may be inoperative provided that: 1) It is deactivated, and 2) The slats and flaps are checked operative on SFCC 1, and 3) The SFCC 1 flap WTB is checked operative before each flight, and 4) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS are operative, and 5) The minimum idle on ground is considered inoperative. Refer to Item 73-20-05 Minimum Idle on Ground OPERATING PROCEDURES GENERAL INFORMATION ENG 2 APPR IDLE ONLY message is displayed on the STATUS SD page. FLAPS SLOW message is displayed on the STATUS SD page. DURING COCKPIT PREPARATION Disregard and clear the F/CTL FLAP SYS 2 FAULT alert displayed on the EWD. MAINTENANCE PROCEDURE Refer to AMM 27-51-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.21 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-51
Flaps Electrical Control and Monitoring
27-51-02
SFCC Slat Channel
27-51-02A
B
2
1
(O)(M) SFCC 2 slap channel may be inoperative provided that: 1) It is deactivated, and 2) The slats and flaps are checked operative on SFCC 1, and 3) The SFCC 1 slat WTB is checked operative before each flight, and 4) All ELACs, SECs, LGCIUs, RAs, FACs and ADIRS are operative, and 5) Takeoff is not performed in CONF 1+F. OPERATING PROCEDURES GENERAL INFORMATION SLATS SLOW message is displayed on the STATUS SD page. DURING COCKPIT PREPARATION Disregard and clear the F/CTL SLAT SYS 2 FAULT alert displayed on the EWD. MAINTENANCE PROCEDUR Refer to AMM 27-51-00-040-005
27-51-03 27-51-03A
Flap Wing Tip Brakes Solenoid B
4
2
(M)
One or two solenoids associated with the SFCC 2 may be inoperative provided that the SFCC 1 flap WTB is checked operative before each flight. MAINTENANCE PROCEDURE Refer to AMM 27-51-00-040-004
A320/321 MEL/CDL
01.27.22 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-54
Flaps Hydraulic Actuation and Power Transmission
27-54-01
Flap Hydraulic Motor
27-54-01A
Green motor inoperative
C
2
1
Green motor may be inoperative.
27-54-01B
Yellow motor inoperative
C
2
1
Yellow motor may be inoperative provided that the blue slat motor is operative.
B
2
1
The valve block associated with SFCC 2 may be inoperative provided that the SFCC 2 flap channel is considered inoperative.
27-54-02
Flap PCU Valve Block
27-54-02A
Refer to Item 27-51-01 SFCC Flap Channel
27-54-03 27-54-03A
Flap PressureOff Brake 2
2
Both must be operative.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.23 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-64
Spoiler Hydraulic Actuation
27-64-01
Spoiler 5
27-64-01A
C
2
0
(O)(M) The pair of spoilers 5 may be inoperative provided that: 1) The affected spoiler is deactivated in the retracted position, and 2) The pairs of spoilers 1, 2, 3, and 4 are operative. OPERATING PROCEDURES AFTER ENGINE START On the HYD SD page, check the absence of amber data. Note: No performance penalty applies when the pair of spoilers 5 is inoperative. MAINTENANCE PROCEDURE Refer to AMM 27-64-00-040-001
27-64-02 27-64-02A
Spoiler 1 or 3 C
4
2
(O)(M) One pair of spoilers 1 or 3 may be inoperative provided (FD) that: 1) The affected spoiler is deactivated in the retracted position, and 2) The pairs of spoilers 2, 4, and 5 are operative, and 3) The Flight Manual performance penalties are applied. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch. (Cont’d on next page)
A320/321 MEL/CDL
01.27.24 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-64
Spoiler Hydraulic Actuation
27-64-02 27-64-02A
Spoiler 1 or 3 (Cont’d)
OPERATING PROCEDURES (Cont’d)
Landing performance computation: Increase the landing distances by 10 %. AFTER ENGINE START On the HYD SD page, check the absence of amber data. FOR TAKEOFF Performed the takeoff using full thrust (TOGA).
MAINTENANCE PROCEDURE Refer to AMM 27-64-00-040-001
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.25 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS
27-64
Spoiler Hydraulic Actuation
27-64-03 27-64-03A
Spoiler 2 or 4 C
4
2
(O)(M) One pair of spoilers 2 or 4 may be inoperative in the (FD) retracted position provided that: 1) The affected spoiler is deactivated in the retracted position, and 2) The pairs of spoilers 1, 3, and 5 are operative, and 3) The SFCC 2 flap channel is operative, and 4) The Flight Manual performance penalties are applied. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS For performance penalties, Refer Procedures 27-64-02A Spoiler 1 or 3
to
Operating
AFTER ENGINE START On the HYD SD page, check the absence of amber data.
MAINTENANCE PROCEDURE Refer to AMM 27-64-00-040-001
A320/321 MEL/CDL
01.27.26 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-64
Spoiler Hydraulic Actuation
27-64-04 27-64-04A
Spoilers 1 and 2 B
4
0
(O)(M) The pairs of spoilers 1 and 2 may be inoperative in the (FD) retracted position provided that: 1) The affected spoilers are deactivated in the retracted position, and 2) The pairs of spoilers 3, 4, and 5 are operative, and 3) The SFCC 2 flap channel is operative, and 4) The Flight Manual performance penalties are applied. OPERATING PROCEDURES (A321) FLIGHT PREPARATION/LIMITATIONS For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch. Landing performance computation: Increase the landing distances by 5 %.
DURING COCKPIT PREPARATION -
SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
(Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.27 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-64
Spoiler Hydraulic Actuation
27-64-04 27-64-04A
Spoilers 1 and 2 (cont’d)
OPERATING PROCEDURES (A321) cont’d FOR TAKEOFF Performed the takeoff using full thrust (TOGA).
IN FLIGHT -
In the case of further failure of SEC 1 and SEC 2: - Autoland is not permitted. - Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is disengaged when the three SECs are failed, it cannot be engaged again. - Maximum landing capability is CAT I
(Cont’d on next page)
A320/321 MEL/CDL
01.27.28 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-64
Spoiler Hydraulic Actuation
27-64-04 27-64-04A
Spoilers 1 and 2 (cont’d)
OPERATING PROCEDURES (A320) FLIGHT PREPARATION/LIMITATIONS For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch . Landing performance computation: Increase the landing distances by 10 %. DURING COCKPIT PREPARATION -
SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
FLIGHT CONTROLS/SEC3/SPLY (121VU Q19) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull
FOR TAKEOFF Performed the takeoff using full thrust (TOGA). IN FLIGHT -
In the case of further failure of SEC 1 and SEC 2: -
Autoland is not permitted.
-
Disengage the AP at 500 ft RA before landing in direct law. As soon as the AP is disengaged when the three SECs are failed, it cannot be engaged again.
-
Maximum landing capability is CAT I
MAINTENANCE PROCEDURE Refer to AMM 27-64-00-040-001
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.29 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27FLIGHT CONTROLS 27-64
Spoiler Hydraulic Actuation
27-64-05 27-64-05A
Spoilers 3 and 4 C
4
0
(O)(M) The pairs of spoilers 3 and 4 may be inoperative in the (FD) retracted position provided that: 1) The affected spoilers are deactivated in the retracted position, and 2) The pairs of spoilers 1, 2, and 5 are operative, and 3) The TR 1 and TR 2 are operative, and 4) The DC TIE contactor 1PC1 is checked closed, and 5) The SFCC 2 flap channel is operative, and 6) The Flight Manual performance penalties are applied. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS For performance penalties Refer to Procedures 27-64-04A Spoilers 1 and 2
Operating
DURING COCKPIT PREPARATION Check that the DC TIE contactor 1 is closed: - Supply the electrical network from the APU or the external power. - On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS. IN FLIGHT Do not use the speedbrakes.
MAINTENANCE PROCEDURE Refer to AMM 27-64-00-040-001
A320/321 MEL/CDL
01.27.30 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
.27 FLIGHT CONTROLS 27-81
Slats Electrical Control and Monitoring
27-81-01
Slat Wing Tip Brakes Solenoids
27-81-01A
C
4
2
(M)
One or two solenoids associated with the SFCC 2 may be inoperative provided that the SFCC 1 slat WTB is checked operative before each flight. MAINTENANCE PROCEDURE Refer to AMM 27-81-00-040-001
27-84
Slats Hydraulic Actuation and Power Transmission
27-84-01
Slats Hydraulic Motor
27-84-01A 27-84-02
C
2
1
One may be inoperative.
C
2
1
The valve block associated with SFCC 2 may be inoperative provided that the SFCC 2 slat channel is considered inoperative.
Slat PCU Valve Block
27-84-02A
Refer to MEL Item 27-51-02 SFCC Slat Channel 27-84-03 27-84-03A
Slat PressureOff Brake 2
2
Both must be operative.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
27 FLIGHT CONTROLS 27-92
01.27.31 FLIGHT CONTROLS
REMARKS OR EXCEPTIONS
Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-01 27-92-01B
Speedbrake Control System Speedbrake 2 B or speedbrakes 3 and 4 inoperative
1
1
(O)(FD) Speedbrake 2 or speedbrakes 3 and 4 may be inoperative provided that the Flight Manual performance penalties associated with one or two pairs of spoilers inoperative are applied. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS -
If speedbrake n° 2 is inoperative: Apply performance penalties associated with the pair of spoilers 2 inoperative. Refer to Operating Procedures 27-64-03A Spoiler 2 or 4
-
If speedbrakes n° 3 and n° 4 are inoperative: Apply performance penalties associated with two pairs of spoilers inoperative. Refer to Operating Procedures 27-64-04A Spoilers 1 and 2
IN FLIGHT -
If speedbrakes n° 3 and n° 4 are inoperative: Do not use the speedbrakes.
A320/321 MEL/CDL
01.27.32 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-92
Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-02 27-92-02A
Ground Spoiler Control System Ground spoiler A control system inoperative
1
0
(O)(FD) May be inoperative provided that: 1) Both thrust reversers are not taken into account for performance computation, and 2) The autobrake function is not used, and 3) The Flight Manual performance penalties are applied, and 4) Repair must be made within three flight legs. OPERATING PROCEDURES (A321) GENERAL INFORMATION The autobrake function is not available. Refer to Operating Procedures 32-42-05A AUTO/BRK Function CAUTION One or both thrust reversers may not deploy at landing. Consequently, for performance determination, do not take into account the credit of the thrust reversers. FLIGHT PREPARATION/LIMITATIONS For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch. Landing performance computation: Increase the landing distances by 20 %. FOR TAKEOFF Performed the takeoff using full thrust (TOGA). (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
27 FLIGHT CONTROLS 27-92
2.
01.27.33 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-02 27-92-02A
Ground Spoiler Control System (Cont’d)
OPERATING PROCEDURES (A320)
GENERAL INFORMATION The autobrake function is not available. Refer to Operating Procedures 32-42-05A AUTO/BRK Function
CAUTION One or both thrust reversers may not deploy at landing. Consequently, for performance determination, do not take into account the credit of the thrust reversers.
FLIGHT PREPARATION/LIMITATIONS For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch .
Landing performance computation: Increase the landing distances by 35 %. FOR TAKEOFF Performed the takeoff using full thrust (TOGA).
A320/321 MEL/CDL
01.27.34 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
27 FLIGHT CONTROLS 27-92
30 JUN 12 MEL
REMARKS OR EXCEPTIONS
Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-02 27-92-02B
Ground Spoiler Control System Spoilers 5 inoperative
C
1
1
(O)
The pair of spoilers 5 may be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS For performance penalties, Refer to Operating Procedures 27-64-01A Spoiler 5
27-92-02C
Spoilers 1 and C 2, or spoilers 3 and 4 inoperative
1
1
(O)
The pairs of spoilers 1 and 2 or the pairs of spoilers 3 and 4 may be inoperative provided that the Flight Manual performance penalties are applied. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS
27-92-03 27-92-03A
-
If the pairs of spoilers 1 and 2 are inoperative: For performance penalties, Refer to Operating Procedures 27-64-04A Spoilers 1 and 2
-
If the pairs of spoilers 3 and 4 are inoperative: For performance penalties, Refer to Operating Procedures 27-64-05A Spoilers 3 and 4
SIDESTICK PRIORITY light 4
4
All must be operative.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.35 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-92
Electrical Flight Control System (EFCS) Control Inputs and Power Supply
27-92-04
Sidestick Dual Input Visual Warnings
27-92-04A 27-92-05
2
1
One may be inoperative.
C
1
0
May be inoperative.
B
1
0
Sidestick Dual Input Aural Warning
27-92-05A 27-93
C
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (O)(M) ELAC 1 or any ELAC 1 function may be inoperative (FD) provided that: 1) All SECs, SFCCs, LGCIUs, RAs, ADIRS and FACs are operative, and 2) The pairs of spoilers 2, 3, 4, and 5 are operative, and 3) The TR 1 and the TR 2 are operative, and 4) Both accelerometers associated with the ELAC 2 are checked operative before each flight, and 5) All sidesticks transducers associated with the ELAC 2 and the three SECs are checked operative before each flight, and 6) The DC TIE contactor 1PC1 is checked closed, before each flight, and 7) The elevators and roll spoilers control is checked operative through the SECs before each flight. (Cont’d on next page)
A320/321 MEL/CDL
01.27.36 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
Note: F/O take-over pb cannot disengage AP1. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS If the AP 1 is engaged for landing: Maximum landing capability is CAT I. If the AP 2 is engaged for landing: Landing capability is CAT II. DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available:
-
-
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If the F/CTL ELAC 1 FAULT alert is displayed on the EWD: (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.37 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) Note: i.
After application of the maintenance procedure, the following ECAM alerts remain displayed on the EWD: C/B TRIPPED R ELEC BAY alert , and C/B TRIPPED ON OVHD PNL alert, and F/CTL ELAC 1 FAULT alert.
ii. After first engine start, the F/CTL ALTN LAW alert may be spuriously displayed. It normally disappears after second engine start. Check of the elevator and the roll spoilers control through the SECs: Put the aircraft in the test configuration: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON Note: If the Yellow Electric Pump is not available, pressurize the Yellow Hydraulic System with a Ground Cart or with the Yellow Engine 2 Pump with the Engine 2 running. - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON (Cont’d on next page)
A320/321 MEL/CDL
01.27.38 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) -
ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
SEC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
SEC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
Wait 5 s
Check of the elevator control through the SEC 1 and the spoilers control through the secretary 1 and the SEC 3: -
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuit depressurization.
-
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
-
Wait 5 s
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
-
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators. (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.39 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) CAUTION If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance. Check of the elevator control through the SEC 2 and of the spoilers control through the SEC 2 and the SEC 3: -
ELAC 1 & 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
Wait 5 s
-
YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuits depressurization.
-
On the F/CTL SD page, check that the yellow and the green elevator actuators symbols become amber.
-
Wait 5 s
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators.
-
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators. (Cont’d on next page)
A320/321 MEL/CDL
01.27.40 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) CAUTION If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance. Return to normal configuration: -
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · OFF
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · OFF
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On Check that the DC TIE contactor 1 is closed:
-
-
Supply the electrical network from the APU or the external power.
-
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
If the F/CTL ELAC 1 PITCH FAULT alert is displayed on the EWD: Note: After first engine start: -
The F/CTL ALTN LAW alert may be spuriously displayed on the EWD. It normally disappears after few seconds when ELAC 2 auto test is accomplished. (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.41 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) Check of the elevator and the roll spoilers control through the SECs: Put the aircraft in the test configuration: -
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
-
BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO
-
BLUE PUMP OVRD pb · · · · · · · · · · · · · · · · · · · · · · ON
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
Wait 5 s
Check of the elevator control through the SEC 1 and of the spoilers control through the SEC 1 and the SEC 3: -
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuit depressurization.
-
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
-
Wait 5 sincerely
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF (Cont’d on next page)
A320/321 MEL/CDL
01.27.42 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) -
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators.
-
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators. CAUTION If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance.
Check of the elevator control through the SEC 2 and of the spoilers control through the SEC 2 and the SEC 3: -
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
Wait 5 s
-
YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuits depressurization.
-
On the F/CTL SD page, check that the yellow and the green elevator actuators symbols become amber.
-
Wait 5 s
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.43 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) -
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators.
-
Move the F/O stick from right stop to left stop, then from forward stop to aft stop.
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators. CAUTION If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance.
Return to normal configuration: -
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On (Cont’d on next page)
A320/321 MEL/CDL
01.27.44 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-01 27-93-01A
ELAC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) Check that the DC TIE contactor 1 is closed: -
Supply the electrical network from the APU or the external power.
-
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
BEFORE ENGINE START -
AP 1 pb · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
CAPT take-over pb · · · · · · · · · · · · · · · · · · · · · · · Press
-
Check that the AP OFF message is displayed on the EWD. Note: Due to the fact that the ELAC 1 is not electrically supplied, the F/O take-over pb cannot disengage the AP 1.
IN APPROACH -
If the AP 1 is used for the approach: The captain must be the PF.
MAINTENANCE PROCEDURE Refer to AMM 27-93-00-040-001 27-93-02 27-93-02A
ELAC 2 1
1
Must be operative.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.45 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-93
ELAC System (Elevator Aileron Computer)
27-93-03
Pitch Normal Law
27-93-03A 27-94
1
1
1
0
Must be operative.
SEC System (Spoiler and Elevator Computer)
27-94-01 27-94-01A
SEC 1 B
(O)(M) May be inoperative provided that: (FD) 1) It is deactivated, and 2) The SEC 2 and the SEC 3 are operative, and 3) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRS are operative, and 4) The SFCC 2 flap channel is operative, and 5) All aileron servo-controls associated with the operative SECs are operative, and 6) The TR 1 and TR 2 are operative, and 7) The sidestick transducers associated with the ELACs and the operative SECs are checked operative before each flight, and 8) The DC TIE contactor 1PC1 is checked closed, before each flight, and 9) The elevators control through the SEC 2 and the ELACs and the roll spoilers control through the operative SECs are checked operative before each flight, and 10) The Flight Manual performance penalties for the pairs of spoilers 3 and 4 inoperative are applied. (Cont’d on next page)
A320/321 MEL/CDL
01.27.46 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-01 27-94-01A
SEC 1 (Cont’d)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS For performance penalties, Refer to Procedures 27-64-05A Spoilers 3 and 4
Operating
DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure. Note:
After application of the maintenance procedure, the C/B TRIPPED R ELEC BAY and the C/B TRIPPED ON OVHD PNL alerts are displayed on the EWD. (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.47 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-01 27-94-01A
SEC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) Check of the elevator control through the operative computers: Put the aircraft in the test configuration: - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . . ON - ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On - ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On - SEC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On - SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . On - Wait 5 s Check of the elevator control through the ELAC 1: -
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuit depressurization.
-
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
-
Wait 5 s
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from forward stop to aft stop.
-
On the F/CTL SD page, check the full travel of both elevators. (Cont’d on next page)
A320/321 MEL/CDL
01.27.48 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-01 27-94-01A
SEC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) CAUTION If an expected elevator movement does not occur, do not attempt any reset. Contact the maintenance. Check of the elevator control through the SEC 2: -
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
Wait 5 s
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuits depressurization.
-
On the F/CTL SD page, check that the yellow and the green elevator actuators symbols become amber.
-
Wait 5 s
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators.
-
Move the F/O stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.49 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-01 27-94-01A
SEC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) -
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2 and 5 and the full travel of both elevators. CAUTION If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance. Return to normal configuration: - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off - ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On - ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
Check that the DC TIE contactor 1 is closed: -
Supply the electrical network from the APU or the external power.
-
On the ELEC SD page, check the link between the DC BUS 1 and the DC BAT BUS.
(Cont’d on next page)
A320/321 MEL/CDL
01.27.50 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-01 27-94-01A
SEC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d)
IN FLIGHT Do not use the speedbrakes. -
If the SEC 2 and the SEC 3 fail during the flight: Autoland is not permitted. Maximum landing capability is CAT I Disengage the AP at 500 ft RA before landing in direct law. When the AP is disengaged with the three SECs failed, it cannot be engaged again.
MAINTENANCE PROCEDURE Refer to AMM 27-94-00-040-002
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.51 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-02 27-94-02A
SEC 2 B
1
0
(O)(M) May be inoperative provided that: 1) It is deactivated, and 2) The SEC 1 and the SEC 3 are operative, and 3) All ELACs, SFCCs, LGCIUs, RAs, FACs and ADIRS are operative, and 4) All aileron servo-controls and roll spoilers associated with the operative SECs are operative, and 5) The sidestick transducers associated with the ELACs and the operative SECs are checked operative before each flight, and 6) The elevators control through the SEC 1 and the ELACs and the roll spoilers control through the operative SECs are checked operative before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure. (Cont’d on next page)
A320/321 MEL/CDL
01.27.52 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-02 27-94-02A
SEC 2 (Cont’d)
OPERATING PROCEDURES (Cont’d) Note: After application of the maintenance procedure, the C/B TRIPPED REAR PNL N-R alert is displayed on the EWD. Check of the elevator control through the operative computers: Put the aircraft in the test configuration: -
YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . ON
-
PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
-
BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . AUTO
-
BLUE PUMP OVRD pb . . . . . . . . . . . . . . . . . . . ON
-
ELAC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
ELAC 2 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
SEC 1 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . On
-
Wait 5 s
Check of the elevator control through the ELAC 1: -
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuit depressurization.
-
On the F/CTL SD page, check that blue elevator actuator symbol becomes amber.
-
Wait 5 s
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.27.53 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-02 27-94-02A
SEC 2 (Cont’d)
OPERATING PROCEDURES (Cont’d) -
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from forward stop to aft stop.
-
On the F/CTL SD page, check the full travel of both elevators. CAUTION If an expected elevator movement does not occur, do not attempt any reset. Contact the maintenance.
Check of the elevator control through the SEC 1: -
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
SEC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
Wait 5 s
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
Wait for hydraulic circuits depressurization.
-
On the F/CTL SD page, check that the blue elevator actuator symbols becomes amber.
-
Wait 5 s
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
Move the CAPT stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators. (Cont’d on next page)
A320/321 MEL/CDL
01.27.54 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-02 27-94-02A
SEC 2 (Cont’d)
OPERATING PROCEDURES (Cont’d) -
Move the F/O stick from right stop to left stop, then from forward stop to aft stop. Each stop must be applied during 3 s
-
On the F/CTL SD page, check the correct movement of the pairs of spoilers 2, 3, and 4 and the full travel of both elevators. CAUTION If an expected spoiler or elevator movement does not occur, do not attempt any reset. Contact the maintenance.
Return to normal configuration: -
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
-
ELAC 1 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
-
ELAC 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · On
AFTER ENGINE START Note: The F/CTL ELEV SERVO FAULT alert may be displayed on the EWD if the PTU is inhibited and only one engine is operating. This alert must disappear when the PTU or the second engine is started. (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.55 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-02 27-94-02A
SEC 2 (Cont’d)
OPERATING PROCEDURES (Cont’d) IN FLIGHT -
If the SEC 1 and the SEC 3 fail during the flight: Autoland is not permitted. Maximum landing capability is CAT I
Disengage the AP at 500 ft RA before landing in direct law. When the AP is disengaged with the three SECs failed, it cannot be engaged again. MAINTENANCE PROCEDURE Refer to AMM 27-94-00-040-002 27-94-03 27-94-03A
SEC 3 C
1
0
(O)
May be inoperative provided that: 1) The SEC 1 and SEC 2 are operative, and 2) The SFCC 2 flap channel is operative, and 3) All aileron servo-controls and roll spoilers associated with the operative SECs are operative, and 4) The Flight Manual performance penalties for the pairs of spoilers 1 and 2 inoperative are applied.
(Cont’d on next page)
A320/321 MEL/CDL
01.27.56 FLIGHT CONTROLS 1.
ITEM
SYSTEM & SEQUENCE OF ITEMS
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-94-03
SEC 3
27-94-03A (cont’d)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS For performance penalties, Refer to Procedures 27-64-04A Spoilers 1 and 2
Operating
DURING COCKPIT PREPARATION Deactivation of the SEC 3: -
SEC 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
-
FLIGHT CONTROLS/SEC 3/SPLY (121VU Q19) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull
IN FLIGHT -
If the SEC 1 and the SEC 2 fail during the flight: Autoland is not permitted. Maximum landing capability is CAT I Disengage the AP at 500 ft RA before landing in direct law. When the AP is disengaged with the three SECs failed, it cannot be engaged again.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.27.57 FLIGHT CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROLS 27-94
SEC System (Spoiler and Elevator Computer)
27-95-01
FCDC 1
27-95-01A 27-95-02 27-95-02A
1
1
1
0
Must be operative.
FCDC 2 C
(O)
May be inoperative. OPERATING PROCEDURES DURING COCKPIT PREPARATION FLIGHT CONTROLS/FCDC2/SPLY (121VU Q20) C/B · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · Pull *
*
*
A320/321 MEL/CDL
01.27.58 FLIGHT CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.01 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-00
MAINTENANCE Message on the STATUS SD page
28-00-01
FUEL MAINTENANCE Message
28-00-01A 28-01
C
1
-
FUEL MAINTENANCE message may be displayed on the STATUS SD page.
C
4
0
One or more may be inoperative provided that the corresponding pump is set to OFF when the associated tank is empty.
C
4
0
One or more may be inoperative provided that the corresponding pump indication is operative on the FUEL SD page.
C
1
0
May be inoperative provided that the X FEED indication is operative on the FUEL SD page.
C
1
0
May be inoperative provided that the X FEED indication is operative on the FUEL SD page.
Overhead Panels
28-01-01
FUEL Overhead Panel
28-01-01-01 Wing TK PUMP pb-sw FAULT light 28-01-01-01A
28-01-01-02 Wing TK PUMP pb-sw OFF light 28-01-01-02A
28-01-01-03 X FEED pb-sw ON light 28-01-01-03A 28-01-01-04 X FEED pb-sw OPEN light 28-01-01-04A
A320/321 MEL/CDL
01.28.02 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-01
Overhead Panels
28-01-01
FUEL Overhead Panel
28-01-01-05 CTR TK PUMP pb-sw FAULT light (A320) 28-01-01-05A
C
2
0
One or both may be inoperative provided that the corresponding pump is set to OFF when there is no fuel in the center tank.
C
2
0
One or both may be inoperative provided that the corresponding transfer valve is set to OFF when there is no fuel in the center tank.
C
2
0
One or both may be inoperative provided that the corresponding pump indication is operative on the FUEL SD page.
C
2
0
One or both may be inoperative provided that the corresponding transfer valve indication is operative on the FUEL SD page.
28-01-01-05 CTR TK XFR pbsw FAULT light (A321) 28-01-01-05A
28-01-01-06 CTR TK PUMP pb-sw OFF light (A320) 28-01-01-06A
28-01-01-06 CTR TK XFR pbsw OFF light (A321) 28-01-01-06A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.03 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-01
Overhead Panels
28-01-01
FUEL Overhead Panel
28-01-01-07 FUEL MODE SEL pb-sw FAULT light (A320) 28-01-01-07A
C
1
0
(O)
May be inoperative provided that all tank pumps indications are operative on the FUEL SD page. OPERATING PROCEDURES AFTER ENGINE START -
If there is fuel in the center tank and with the slats retracted: On the FUEL SD page, check that the center tank pumps indications are in line.
-
With the slats extended: On the FUEL SD page, check that the center tank pumps indications are cross line.
AFTER TAKEOFF -
If there is fuel in the center tank and with the slats retracted: On the FUEL SD page, check that the center tank pumps indications are in line.
28-01-01-07 FUEL MODE SEL pb-sw FAULT light (A321) 28-01-01-07B
C
1
0
May be inoperative provided that all wing tank pumps and center tank transfer valves indications are operative on the FUEL SD page.
A320/321 MEL/CDL
01.28.04 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-01
Overhead Panels
28-01-01
FUEL Overhead Panel
28-01-01-08 ACT pb-sw FAULT light (A320) (ACTs) 28-01-01-08A
C
1
0
(O)
May be inoperative provided that the fuel quantity indications of the ACT(s) and of the center tank are operative on the FUEL SD page. OPERATING PROCEDURES IN FLIGHT -
If a manual transfer from the ACT to the CTR tank is necessary: -
Refer to FCOM/PRO-ABN-28 ACT XFR FAULT PROC.
-
On the FUEL SD page, monitor the fuel transfer.
28-01-01-09 ACT pb-sw FWD light (A320) (ACTs) 28-01-01-09A
C
1
0
May be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.05 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-01 Fuel On Board (FOB) Indication on the FUEL SD page 28-07-01-01A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES AFTER ENGINE START Check that /FF is selected on the MCDU FUEL PRED page. - If /FF is not selected on the MCDU FUEL PRED page: Insert the FOB. The FOB may be calculated either using the indications on the refuel control panel (if available) or by using the Manual Magnetic Indicators (MMIs):Refer to FCOM/LOD-FUL-FUEL-C USE OF MANUAL MAGNETIC INDICATIOR (MMI)
A320/321 MEL/CDL
01.28.06 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page 28-07-01-02A
(A320 ACTs)
C
6
0
(A320)
C
5
0
(A321)
C
3
0
(O)
One or more FQI may be in the degraded mode (with dashes on the two last digits) provided that the loss of accuracy is taken into account for the fuel planning for each affected tank. Note: The Fuel On Board indication is also in the degraded mode. OPERATING PROCEDURES (A320) ON GROUND The FQI is in degraded mode when the FOB indication is displayed with two dashes across the two last digits on the EWD. -
When the FQI is in degraded mode: On the FUEL SD page, determine which tank is affected. The resulting loss of accuracy must be taken into account by using the two following parameters: 1. Fq : The extra fuel quantity to be loaded. 2. W: The weight to be added to the total fuel weight for TOW calculation only. Fq and W parameters are given as follows : (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.28.07 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page 28-07-01-02A
(Cont’d)
OPERATING PROCEDURES(Cont’d) Applicable to (A320) LOSS OF ACCURACY DUE TO THE FUEL QUANTITY INDICATION IN DEGRADED MODE (Values in kg) Fq(kg)
W (kg)
OUTER TANK
20
200
INNER TANK
110
110
CENTER TANK
130
130
ALL TANKS
390
750
-
When the auto refuel stops: - Preselect the fuel quantity required for the mission : Fm - Enter the table and determine Fq and W values for the affected tank. - Start again the auto refuel with the new preselected quantity which corresponds to the total FOB : Fm+Fq (Cont’d on next page)
A320/321 MEL/CDL
01.28.08 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page 28-07-01-02A
(Cont’d)
OPERATING PROCEDURES (A320) Note: If all tanks reach high level before having loaded the complete Fq value, this shows that all tanks are volumetrically full but the necessary fuel mass for the mission is not guaranteed since the fuel quantity indication varies with the fuel density. Therefore the mission or the aircraft load must be amended to match the minimum fuel quantity known to be onboard. -
When the auto refuel stops again: The FOB value to be considered for TOW calculation is: FOB = Fm+Fq+W -
-
If all tanks reach high level before having loaded Fq value: - The extra fuel quantity known to be onboard is Fq* with: Fq* < Fq - The FOB value to be considered for TOW calculation is: FOB = Fm+Fq *+W
If the resulting TOW is higher than the MTOW: The aircraft load must be reduced. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.28.09 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page 28-07-01-02A
(Cont’d)
OPERATING PROCEDURES (A321) ON GROUND The FQI is in degraded mode when the FOB indication is displayed with two dashes across the two last digits on the EWD. -
When the FQI is in degraded mode: On the FUEL SD page, determine which tank is affected. The resulting loss of accuracy must be taken into account by using the two following parameters: 1. Fq : The extra fuel quantity to be loaded. 2. W: The weight to be added to the total fuel weight for TOW calculation only. (Cont’d on next page)
A320/321 MEL/CDL
01.28.10 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page 28-07-01-02A
(Cont’d)
OPERATING PROCEDURES (A321) (Cont’d) Fq and W parameters are given as follows : LOSS OF ACCURACY DUE TO THE FUEL QUANTITY INDICATION IN DEGRADED MODE (Values in kg) Fq(kg)
W (kg)
WING TANK
130
310
CENTER TANK
130
130
ALL TANKS
390
750
-
When the auto refuel stops: -
Preselect the fuel quantity required for the mission : Fm
-
Enter the table and determine Fq and W values for the affected tank.
-
Start again the auto refuel with the new preselected quantity which corresponds to the total FOB : Fm+Fq (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.28.11 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-02 Fuel Quantity Indication (FQI) in Degraded Mode on the FUEL SD page 28-07-01-02A
(Cont’d)
OPERATING PROCEDURES (Cont’d) Applicable to (A321) Note: If all tanks reach high level before having loaded the complete Fq value, this shows that all tanks are volumetrically full but the necessary fuel mass for the mission is not guaranteed since the fuel quantity indication varies with the fuel density. Therefore the mission or the aircraft load must be amended to match the minimum fuel quantity known to be onboard. -
When the auto refuel stops again: The FOB value to be considered for TOW calculation is: FOB = Fm+Fq+W - If all tanks reach high level before having loaded Fq value: The extra fuel quantity known to be onboard is Fq* with: Fq* < Fq The FOB value to be considered for TOW calculation is: FOB = Fm+Fq *+W
-
If the resulting TOW is higher than the MTOW: The aircraft load must be reduced.
A320/321 MEL/CDL
01.28.12 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-03 Outer Tank Fuel Quantity Indication on the FUEL SD page (A320) 28-07-01-03A
Check of fuel C quantity in the associated tank after refueling
2
1
(O)(M) One may be inoperative provided that: 1) The fuel quantity in the associated tank is checked after each refueling by the corresponding fuel quantity indicator on the refuel/defuel control panel, and 2) The associated fuel used indication is operative, and 3) The associated inner tank indication is operative. OPERATING PROCEDURES AFTER REFUELING To check the fuel quantity in the associated tank: Refer to FCOM/PER-LOD-FUL-FUEL-A. GENERAL INFORMATION. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-003
28-07-01-03B
High level fuel C detection system checked operative before refueling and associated inner tank indication operative
2
1
(M)
One may be inoperative provided that: 1) The high level fuel detection system is checked operative before refueling, and 2) The tanks in both wings are full, and 3) The associated fuel used indication is operative, and 4) The associated inner tank indication is operative. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-003
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.13 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-03 Outer Tank Fuel Quantity Indication on the FUEL SD page (A320) 28-07-01-03C
B Check of fuel quantity in the associated wing after refueling/ defueling
2
1
(O)(M) One may be inoperative provided that: 1) The fuel quantity in the associated wing (inner and outer tanks) is checked after each refueling/defueling by the corresponding fuel quantity indicator on the refuel/defuel control panel, and 2) The associated fuel used indication is operative. OPERATING PROCEDURES Refer to MEL item 28-07-01-03A MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-003
28-07-01-03D
High level fuel B detection system checked operative before refueling
2
1
(M)
One may be inoperative provided that: 1) The high level fuel detection system is checked operative before refueling, and 2) The tanks in both wings are full, and 3) The associated fuel used indication is operative. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-003
A320/321 MEL/CDL
01.28.14 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-04 Inner Tank Fuel Quantity Indication on the FUEL SD page (A320) 28-07-01-04A
Check of fuel C quantity in the associated tank after refueling
2
1
(O)(M) One may be inoperative provided that: 1) The fuel quantity in the associated tank is checked after each refueling by the corresponding fuel quantity indicator on the refuel/defuel control panel, and 2) The associated fuel used indication is operative. OPERATING PROCEDURES AFTER ENGINE START Check that /FF is selected on the MCDU FUEL PRED page. -
If /FF is not selected on the MCDU FUEL PRED page: Insert the FOB. The FOB may be calculated either using the indications on the refuel control panel (if available) or by using the Manual Magnetic Indicators (MMIs): Refer to FCOM/PER-LOD-FUL-FUEL-C. MANUAL MAGNETIC INDICATOR (MMI)
MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-005
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.15 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-04 Inner Tank Fuel Quantity Indication on the FUEL SD page (A320) 28-07-01-04B
High level fuel C detection system checked operative before refueling
2
1
(M)
One may be inoperative provided that: 1) The high level fuel detection system is checked operative before refueling, and 2) The tanks in both wings are full, and 3) The associated fuel used indication is operative.
MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-005
A320/321 MEL/CDL
01.28.16 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-04 Wing Tank Fuel Quantity Indication on the FUEL SD page (A321) 28-07-01-04A
Check of fuel C quantity in the associated tank after refueling
2
1
(O)(M) One may be inoperative provided that: 1) The fuel quantity in the associated tank is checked after each refueling by the manual magnetic indicators or by the corresponding fuel quantity indicator on the refuel/defuel control panel, and 2) The associated fuel used indication is operative. OPERATING PROCEDURES AFTER ENGINE START Check that /FF is selected on the MCDU FUEL PRED page. -
IIf /FF is not selected on the MCDU FUEL PRED page: Insert the FOB. The FOB may be calculated either using the indications on the refuel control panel (if available) or by using the Manual Magnetic Indicators (MMIs): Refer to FCOM/PER-LOD-FUL-FUEL-C. MANUAL MAGNETIC INDICATOR (MMI).
MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-005
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.17 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-05 Center Tank Fuel Quantity Indication on the FUEL SD page (A320) 28-07-01-05A
Check of fuel quantity after refueling
C
1
0
(O)(M) May be inoperative provided that: 1) The fuel quantity in the center tank is checked after each refueling by the manual magnetic indicators or by the corresponding fuel quantity indicator on the refuel/defuel control panel, and 2) All wing tanks fuel quantity indications are operative, and 3) Both fuel used indications are operative. OPERATING PROCEDURES AFTER REFUELING To check the fuel quantity in the associated tank: Refer to FCOM/PER-LOD-FUL-FUEL-C. MANUAL MAGNETIC INDICATOR (MMI). MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-006
28-07-01-05B
Fuel in the C center tank not usable
1
0
May be inoperative provided that there is no fuel in the center tank or the fuel in this tank is considered as not usable and as part of the ZFW and is taken into account for CG determination.
A320/321 MEL/CDL
01.28.18 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page Note:
28-07-01-05 Center Tank Fuel Quantity Indication on the FUEL SD page (A320) (ACTs)
This failure will result in the display of the FUEL ACT XFR FAULT alert while the automatic transfer is still operative. Refer to Item 28-09-03 FUEL ACT XFR FAULT Alert
28-07-01-05A
Check of fuel quantity after refueling
C
1
0
(O)(M) May be inoperative provided that: (FD) 1) The fuel quantity in the center tank is checked after each refueling by the manual magnetic indicators or by the corresponding fuel quantity indicator on the refuel/defuel control panel, and 2) All wing tanks and ACT(s) fuel quantity indications are operative, and 3) Both fuel used indications are operative, and 4) The forward transfer from ACT(s) to the center tank is monitored during the flight. OPERATING PROCEDURES AFTER REFUELING To check the fuel quantity in the associated tank: Refer to FCOM/PER-LOD-FUL-FUEL-A.GENERAL INFORMATION.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.19 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-05 Center Tank Fuel Quantity Indication on the FUEL SD page (A320) (ACTs) 28-07-01-05A
(Cont’d)
OPERATING PROCEDURES (Cont’d) AT TOP OF CLIMB -
Check on the FUEL SD page that the fuel is transferred from one additional center tank (from ACT 2 if ACT 2 is installed and not empty) to the center tank.
-
Check that the fuel quantity in one additional center tank has decreased (from ACT 2 if ACT 2 is installed and not empty).
-
If the automatic transfer has not started: - After 30 minutes of flight: ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD If necessary perform a descent to FL 270.
-
When ACT (both ACTs if two ACTs installed) empty: ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-006
28-07-01-05B
Fuel in the C center tank not usable
1
0
May be inoperative provided there is no fuel in the center tank or the fuel in this tank is considered as not usable and as part of the ZFW and is taken into account for CG determination.
A320/321 MEL/CDL
01.28.20 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page Note:
28-07-01-06 ACT Fuel Quantity Indication on the FUEL SD page (A320) (ACTs) 28-07-01-06B
Fuel in the ACT C
This failure will result in the inhibition of the FUEL ACT XFR FAULT alert. Refer to Item 28-09-03 FUEL ACT XFR FAULT Alert 1
0
(O)(FD) One fuel quantity indication may be inoperative provided that: 1) All wing tanks and center tank and the other ACT fuel quantity indications are operative, and 2) Both fuel used indications are operative, and 3) The forward transfer from ACT(s) to the center tank is monitored during the flight. OPERATING PROCEDURES AT TOP OF CLIMB Check of the fuel transfer from one additional center tank (from ACT 2 if ACT 2 is installed and not empty) to the center tank: On the FUEL SD page, check that the transfer indication (arrow) is displayed or check that the total fuel indicated is above the actual fuel indicated after refuel minus FU. -
If the automatic transfer has not started: -
After 30 minutes of flight: - ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD - If necessary perform a descent to FL 270. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.21 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-01
Fuel Quantity Indications on the FUEL SD page
28-07-01-06 ACT Fuel Quantity Indication on the FUEL SD page (A320) (ACTs) 28-07-01-06B
(Cont’d)
OPERATING PROCEDURES (Cont’d) -
28-70-01-06C
ACT empty
C
1
0
When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
One may be inoperative provided that there is no fuel in any ACT.
A320/321 MEL/CDL
01.28.22 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-02
Fuel Temperature Indications on the FUEL SD page
28-07-02-01 Fuel Temperature Indication on the FUEL SD page (A320) 28-07-02-01A
C
4
2
One in each wing or both in one wing may be inoperative.
C
2
1
One may be inoperative.
28-07-02-01 Fuel Temperature Indication on the FUEL SD page (A321) 28-07-02-01A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.23 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-03
Tank Pump Indications on the FUEL SD page
28-07-03-01 Wing Tank Pump Indication on the FUEL SD page 28-07-03-01A
C
4
0
One or more may be inoperative.
C
2
0
One or both may be inoperative.
C
2
0
28-07-03-02 Center Tank Pump Indication on the FUEL SD page (A320) 28-07-03-02A 28-07-04
Valve Indications on the FUEL SD page
28-07-04-01 Engine LP Fuel Valve Indication on the FUEL SD page 28-07-04-01A
(M)
One or both may be inoperative provided that the associated LP valve is checked operative before each flight. MAINTENANCE PROCEDURE Refer to AMM 28-24-00-040-001
A320/321 MEL/CDL
01.28.24 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-04
Valve Indications on the FUEL SD page
28-07-04-02 APU LP Fuel Valve Indication on the FUEL SD page 28-07-04-02A
C
1
0
(M)
May be inoperative provided that: 1) The APU LP valve is secured in the closed position and, 2) The APU is not used. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-001
28-07-04-03 Crossfeed Valve Indication on the FUEL SD page 28-07-04-03A
C
1
0
(M)
May be inoperative provided that operation of the crossfeed valve is checked before the first flight of each day. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-002
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.25 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-04
Valve Indications on the FUEL SD page
28-07-04-04 Wing Transfer Valve Indication on the FUEL SD page (A320) 28-07-04-04A
C
2
0
(O)(M) One or both may be inoperative provided that: 1) The fuel quantity indications of the associated inner and outer tanks are operative, and 2) The transfer valve operation is checked before each flight and when used in flight.
OPERATING PROCEDURES IN FLIGHT -
When any inner tank fuel quantity reaches 750 kg of fuel: On the FUEL SD page, check the associated outer tank transfer.
MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-004
A320/321 MEL/CDL
01.28.26 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-07
Indications on the FUEL SD page
28-07-04
Valve Indications on the FUEL SD page
28-07-04-05 Center Tank Transfer Valve Indication on the FUEL SD page (A321) 28-07-04-05A
C
2
0
One or both may be inoperative.
C
1
0
May be inoperative provided that the fuel quantity indications (both FQI if both ACTs installed) of the ACT(s) and of the center tank are operative on the FUEL SD page.
28-07-04-06 ACT to CTR TK Transfer (Arrow) Indication on the FUEL SD page (A320) (ACTs) 28-07-04-06A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.27 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-01
28-09-01A
FUEL L(R) INNER(OUTER) TK HI TEMP Alert (A320) One or two inoperative
C
4
2
(O)
One in each wing or both in one wing may be displayed provided that: 1) The fuel temperature indications of the non affected tanks are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. OPERATING PROCEDURES ON GROUND OR IN FLIGHT On the FUEL SD page, monitor the fuel temperature before takeoff and periodically during the flight. Note: For fuel temperature limits, Refer to FCOM LIMITATION. -
If fuel temperature reaches limits: - Before takeoff: Delay takeoff and shut down the engine on the affected side. - In flight: Increase the engine fuel flow on the affected side. If necessary use the APU GEN and switch off the IDG on the affected side (if the opposite GEN is available).
A320/321 MEL/CDL
01.28.28 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-01
28-09-01B
FUEL L(R) INNER(OUTER) TK HI TEMP Alert (A320) One or more inoperative
C
4
0
(O)
One or more may be displayed provided that: 1) The fuel temperature indications are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. OPERATING PROCEDURES Refer to MEL item 28-09-01A (A320)
28-09-01
28-09-01A
FUEL L(R) WING TK HI TEMP Alert (A321) One inoperative C
2
1
(O)
One may be displayed provided that: 1) The fuel temperature indications of the opposite wing are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.29 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-01
28-09-01A
FUEL L(R) WING TK HI TEMP Alert (A321) (Cont’d)
OPERATING PROCEDURES ON GROUND OR IN FLIGHT On the FUEL SD page, monitor the fuel temperature before takeoff and periodically during the flight. Note: For fuel temperature limits, Refer to FCOM LIMITATION. -
If fuel temperature reaches limits: - Before takeoff: Delay takeoff and shut down the engine on the affected side. - In flight: Increase the engine fuel flow on the affected side. If necessary use the APU GEN and switch off the IDG on the affected side (if the opposite GEN is available).
28-09-01B
Two inoperative C
2
0
(O)
One or both may be displayed provided that: 1) The fuel temperature indications are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. OPERATING PROCEDURES Refer to MEL item 28-09-01A (A321)
A320/321 MEL/CDL
01.28.30 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-02
28-09-02A
FUEL L(R) INNER(OUTER) TK LO TEMP Alert (A320) One or two inoperative
C
4
2
(O)
One in each wing or both in one wing may be displayed provided that: 1) The fuel temperature indications of the non affected tanks are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. OPERATING PROCEDURES ON GROUND OR IN FLIGHT On the FUEL SD page, monitor the fuel temperature before takeoff and periodically during the flight. Note: For fuel temperature limits, Refer to FCOM LIMITATION. -
If fuel temperature reaches limits: -
Before takeoff: Delay takeoff.
-
In flight: Consider descending to a lower altitude and/or increasing the mach to increase the TAT.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.31 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-02
28-09-02B
FUEL L(R) INNER(OUTER) TK LO TEMP Alert (A320) One or more inoperative
C
4
0
(O)
One or more may be displayed provided that: 1) The fuel temperature indications are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. OPERATING PROCEDURES Refer to MEL item 28-09-02A (A320)
28-09-02
28-09-02A
FUEL L(R) WING TK LO TEMP Alert (A321) One inoperative C
2
1
(O)
One may be displayed provided that: 1) The fuel temperature indications of the opposite wing are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. (Cont’d on next page)
A320/321 MEL/CDL
01.28.32 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-02
28-09-02A
FUEL L(R) WING TK LO TEMP Alert (A321) (Cont’d)
OPERATING PROCEDURES ON GROUND OR IN FLIGHT On the FUEL SD page, monitor the fuel temperature before takeoff and periodically during the flight. Note: For fuel temperature limits, Refer to FCOM LIMITATION. -
If fuel temperature reaches limits: -
Before takeoff: Delay takeoff.
-
In flight: Consider descending to a lower altitude and/or increasing the mach to increase the TAT.
28-09-02B
Both inoperative
C
2
0
(O)
One or both may be displayed provided that: 1) The fuel temperature indications are operative on the FUEL SD page, and 2) The fuel temperature is monitored before takeoff and during the flight. Note: For fuel temperature limitations, Refer to FCOM LIMITATION. OPERATING PROCEDURES Refer to MEL item 28-09-02A (A321)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.33 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-09
ECAM Alerts
28-09-03
FUEL ACT XFR FAULT Alert (A320) (ACTs)
28-09-03A
ACT empty
C
1
0
28-09-03B
ACT fuel transfer monitored
C
1
0
May be displayed provided that there is no fuel in any ACT. (O)
May be displayed provided that the forward transfer from the ACT(s) to the center tank is monitored during the flight. OPERATING PROCEDURES Refer to Operating Procedures 28-07-01-05A Center Tank Fuel Quantity Indication on the FUEL SD page
28-12
Tank Venting System
28-12-01
28-12-01A
Overpressure Protector between the Inner and the Outer Tank (A320) Inner tank temperature monitored
C
2
0
(O)
One or both may be broken or missing provided that the fuel temperature of the inner tank is monitored. OPERATING PROCEDURES GENERAL INFORMATION The dispatch condition results in an unusual distribution of the fuel quantity: the outer tank of the affected wing will be partially empty with the transfer valves normally closed. FLIGHT PREPARATION/LIMITATIONS Fuel management should be performed with care. (Cont’d on next page)
A320/321 MEL/CDL
01.28.34 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-12
Tank Venting System
28-12-01
28-12-01A
Overpressure Protector between Inner and Outer Tank (A320) (Cont’d)
OPERATING PROCEDURES(Cont’d) ON GROUND AND IN FLIGHT -
After a long taxi or if the outside air temperature is high, with the outer tank of the affected wing empty: The FUEL L(R) OUTER TK HI TEMP alert may be displayed on the EWD. -
If the FUEL L(R) OUTER TK HI TEMP alert is displayed on the EWD: - Disregard the FUEL L(R) OUTER TK HI TEMP alert. - Monitor the inner tank fuel temperature during taxi and in flight to ensure that it decreases and remains within the temperature limitations. Note:
For fuel temperature limitations, Refer to FCOM LIMITATION. If the inner tank fuel temperature exceeds the temperature limitations, apply the FUEL L(R) INNER TK HI TEMP procedure: Refer to Operating Procedres 28-09-01A(B) FUEL L(R) INNER(OUTER)/WING TK HI TEMP Alert. 28-12-01B
Transfer valves C secured open
2
0
(O)(M) One or both may be broken or missing provided that the associated transfer valves are secured in the open position after each refueling. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.28.35 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-12
Tank Venting System
28-12-01
28-12-01B
Overpressure Protector between Inner and Outer Tank (A320) (Cont’d)
OPERATING PROCEDURES GENERAL INFORMATION The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in the outer tank on the affected side will transfer to the inner tank even when the inner tank is not empty. ON GROUND Do not re-select the refuel power or open the refuel door. Note: The transfer valve latch circuit will send order to de-latch them and the valves will close again (they will then operate normally and open at low level). MAINTENANCE PROCEDURE Refer to AMM 28-12-00-040-003
A320/321 MEL/CDL
01.28.36 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-12
Tank Venting System
28-12-02
Overpressure Protector in the Vent Surge Tank
28-12-02A
C
2
1
(O)
One may be broken or missing. OPERATING PROCEDURES ON GROUND AND IN FLIGHT
28-12-03
28-12-03A
Avoid lateral accelerations in order to reduce the possibility of fuel spill during taxi and climb out.
-
In cruise check that no fuel spillage occurred.
-
Check that the FOB is sufficient to reach the destination with the adequate reserve.
Overpressure Protector in the Inner Tank (A320)
28-12-03A 28-12-03
-
2
2
Both must be operative.
2
2
Both must be operative.
Overpressure Protector in the Wing Tank (A321)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.37 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-12
Tank Venting System
28-12-04
Overpressure Protector between the Center and the Inner Tank (A320)
28-12-04A
28-12-04
28-12-05A
1
Must be operative.
1
1
Must be operative.
1
0
May be broken or missing provided that the ACT auto transfer system is considered inoperative.
Overpressure Protector between the Center and the Wing Tank (A321)
28-12-04A
28-12-05
1
Overpressure Protector in the ACT (A320) (ACTs) C
Refer to Item 28-28-01 ACT Auto Transfer System
A320/321 MEL/CDL
01.28.38 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-15
Intercell Transfer System
28-15-01
28-15-01A
LH Wing Transfer Valve (A320) One or both inoperative open
C
2
0
(O)
One or both may be inoperative in the open position.
OPERATING PROCEDURES GENERAL INFORMATION The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in the outer tank on the affected side will transfer to the inner tank even when the inner tank is not empty. 25-15-01C
One inoperative C closed
2
1
(O)(M) One may be inoperative in the closed position provided that the remaining LH wing transfer valve is secured in the open position after each refueling. OPERATING PROCEDURES Refer to MEL item 28-15-01A.
MAINTENANCE PROCEDURE Refer to AMM 28-15-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.39 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-15
Intercell Transfer System
28-15-02
28-15-02A
RH Wing Transfer Valve (A320) One or both inoperative open
C
2
0
(O)(FD) One or both may be inoperative in the open position.
OPERATING PROCEDURES GENERAL INFORMATION The dispatch condition results in an unusual distribution of the fuel quantity: the fuel in the outer tank on the affected side will transfer to the inner tank even when the inner tank is not empty. 28-15-02C
One inoperative C closed
2
1
(O)(M) One may be inoperative in the closed position provided that the remaining RH wing transfer valve is secured in the open position after each refueling.
OPERATING PROCEDURES Refer to MEL item 28-15-02A
MAINTENANCE PROCEDURE Refer to AMM 28-15-00-040-002
A320/321 MEL/CDL
01.28.40 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-20
Distribution
28-20-01
Automatic Fuel Feed System (A320)
28-20-01A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES ON GROUND -
-
28-21
If the center tank is empty for the flight : -
MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . MAN
-
CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF
If the center tank is not empty for the flight: -
Before engine start: MODE SEL pb-sw . . . . . . . . . . . . . . . . . . . . . MAN
-
3 min after engine start : CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF
-
After slats retraction and when the fuel in one wing is less than 5 000 kg: CTR TK PUMP 1 and 2 pb-sw. . . . . . . . . . . . . . On
-
When the FUEL CTR TK PUMPS LO PR alert is displayed on the EWD: CTR TK PUMP 1 and 2 pb-sw . . . . . . . . . . . . OFF
Main Fuel Pump System
28-21-01 28-21-01A
Wing Tank Pump JP4/JET B not used
C
4
3
One pump may be inoperative provided that JP4/JET B is not used.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.41 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-21
Main Fuel Pump System
28-21-01 28-21-01B
Wing Tank Pump Use of JP4/ JET B
C
4
3
(M)
Pump 2 LH or pump 2 RH may be inoperative when JP4/JET B is used provided that: 1) The fuel return valve is checked operative before each flight, and 2) The fuel temperature is less than 30 °C.
MAINTENANCE PROCEDURE Refer to AMM 28-21-00-040-001 28-21-02
28-21-02A
Center Tank Pump (A320) (ACTs) One inoperative C
2
1
(O)(FD) One may be inoperative provided that the flight routes permit a landing at a suitable airport if the remaining center tank pump fails with fuel in the center tank and in any ACT(s). OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS In the case of dispatch with fuel in the center tank, the remaining center tank pump failure must be considered for the flight planning. Operator has to ensure that, from any point of the first part of the route where the center tank is not empty the aircraft may reach a suitable airport considering the fuel quantity (FQ) contained in the center tank as definitely not usable for the flight planning (as a consequence of the failure of the remaining center tank pump). (Cont’d on next page)
A320/321 MEL/CDL
01.28.42 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-21
Main Fuel Pump System
28-21-02
28-21-02A
Center Tank Pump (A320) (ACTs) (Cont’d)
OPERATING PROCEDURES (Cont’d) DURING COCKPIT PREPARATION -
X FEED pb-sw · · · · · · · · · · · · · · · · · · · · · · CHECK Off
-
Affected CTR TK PUMP pb-sw · · · · · · · · · · · · · · · OFF
< If the fuel quantity in the center tank is less than 200 kg: -
Operative CTR TK PUMP pb-sw · · · · · · · · · · · · · · OFF
< If the fuel quantity in the center tank is more than 200 kg: -
Operative CTR TK PUMP pb-sw · · · · · · · · · · · · · · · On
IN FLIGHT < If the fuel quantity in the center tank is less than 200 kg: -
Operative CTR TK PUMP pb-sw· · · · · · · Maintain OFF
< If the fuel quantity in the center tank is more than 200 kg: The fuel in the center tank can be completely used if the operative center tank pump does not fail before the center tank is empty. If the operative center tank pump fails before the center tank is empty, consider the fuel quantity remaining and the time to destination to decide either to continue the flight or to divert.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.28.43 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-21
Main Fuel Pump System
28-21-02
28-21-02A
Center Tank Pump (A320) (ACTs) (Cont’d)
OPERATING PROCEDURES (Cont’d)
· When the fuel quantity in the first wing inner tank is less than 4 500 kg: Operative CTR TK PUMP pb-sw . . . . . . . . . . . . . . . . . OFF X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
· When the fuel quantity in the first wing inner tank increases above 5 500 kg: X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off Operative CTR TK PUMP pb-sw . . . . . . . . . . . . . . . . . OFF
· When the fuel quantity in the center tank is less than 250 kg: X FEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Off
A320/321 MEL/CDL
01.28.44 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-21
Main Fuel Pump System
28-21-02
28-21-02A
Center Tank Pump (A320) One inoperative C
2
1
(O)(FD) One may be inoperative in the closed position provided that the flight routes permit a landing at a suitable airport if the remaining center tank transfer valve fails with fuel in the center tank. OPERATING PROCEDURES IN FLIGHT -
Disregard the FUEL L(R) XFR VALVE FAULT alert displayed on the EWD.
-
MODE SEL pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · Auto
-
Operative CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · On
-
Affected CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · OFF
-
When differences between fuel quantities in two wings is above 1 500 kg: Monitor the fuel imbalance. Note: Apply the FUEL IMBALANCE FCOM procedure as required provided that no fuel leak is suspected. -
28-21-03
28-21-03A
Until the fuel is balanced: L(R) TK PUMPS (on the lighter side) pb-sw . . OFF
Wing Tank Pump Sequence Valve (A320) C
4
3
One may be inoperative provided that the associated pump is set to OFF when the center tank is feeding.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.45 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-22
APU Fuel Pump System
28-22-01
APU Fuel Pump
28-22-01A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES FOR APU START OPERATION Pressurize the LH fuel manifold with at least one fuel tank pump.
28-22-01B
A
1
0
(O)(FD) May be inoperative for four flights.
OPERATING PROCEDURES Refer to MEL item 28-22-01A
28-23
Crossfeed System
28-23-01 28-23-01A
Crossfeed Valve 1
1
Must be operative.
A320/321 MEL/CDL
01.28.46 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-24
Engine LP Fuel Shutoff
28-24-01
Engine LP Fuel Valve Electrical Motor
28-24-01A
C
4
3
(M)
One may be inoperative on one engine provided that: 1) The affected motor is deactivated, and 2) The remaining motor is checked operative. MAINTENANCE PROCEDURE Refer to AMM 28-24-00-040-002
28-25
Refuel/Defuel System
28-25-01
Fuel Quantity Preselector
28-25-01A 28-25-02
28-25-02A
28-25-03 28-25-03A
C
1
0
May be inoperative.
(A320 ACTs)
C
8
0
(A320)
C
7
0
One or more indications may be inoperative provided that the fuel quantity is continuously monitored on the FUEL SD page during refueling and defueling.
(A321)
C
5
0
C
3
0
Fuel Quantity on the Refuel/Defuel Control Panel
Refuel Valve Manual refueling
(M)
One or more may be inoperative provided that the aircraft is manually refueled.
MAINTENANCE PROCEDURE Refer to AMM 28-25-00-040-005
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.47 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-25
Refuel/Defuel System
28-25-03 28-25-03B
28-25-04
Refuel Valve Gravity refueling
C
3
0
C
1
0
One or more may be inoperative provided that overwing gravity refueling is performed. Refer to FCOM/PER-LOD-FUL OVERWING GRAVITY REFUELING
Transfer Defuel Valve
28-25-04A
(M)
May be inoperative provided that the valve is secured in the closed position. MAINTENANCE PROCEDURE Refer to AMM 28-25-00-040-004
28-25-05
28-25-05A
Exterior Refuel/Defuel Control Panel (A320) Cockpit Fuel Quantity preselector operative
C
1
0
(M)
May be inoperative provided that the cockpit fuel quantity pre-selector is operative. MAINTENANCE PROCEDURE Refer to AMM 28-25-00-040-008
28-25-05
28-25-05A
Exterior Refuel/Defuel Control Panel (A321) C
1
0
(M)
May be inoperative provided that the aircraft is manually refueled. MAINTENANCE PROCEDURE Refer to AMM 28-25-00-040-008
A320/321 MEL/CDL
01.28.48 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-26
Main Transfer System
28-26-01
28-26-01B
Center Tank Transfer Valve (A321) One Inoperative C Closed
2
1
(O)
One may be inoperative in the closed position provided that the flight routes permit a landing at a suitable airport if the remaining center tank valve fails with fuel in the center tank. OPERATING PROCEDURES IN FLIGHT -
Disregard the FUEL L(R) XFR VALVE FAULT alert displayed on the EWD.
-
MODE SEL pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · Auto
-
Operative CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · On
-
Affected CTR TK L(R) XFR pb-sw· · · · · · · · · · · · · OFF
· When differences between fuel quantities in two wings is above 1 500 kg: Monitor the fuel imbalance. Note: Apply the FUEL IMBALANCE FCOM procedure as required provided that no fuel leak is suspected. Refer to FCOM/PRO-ABN-28 FUEL IMBALANCE. · Until the fuel is balanced: L(R) TK PUMPS (on the lighter side) pb-sw . . . . . . . . OFF
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.49 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System
28-28-01
ACT Auto Transfer System (A320) (ACTs)
28-28-01A
ACT empty
C
1
0
(FD)
May be inoperative provided that there is no fuel in any ACT.
28-28-01B
Manual fuel transfer operative
C
1
0
(O)(FD) May be inoperative provided that: 1) The manual transfer from the ACT(s) to the center tank is operative, and 2) The fuel quantity indications of the ACT(s) and of the center tank are operative on the FUEL SD page.
OPERATING PROCEDURES DURING COCKPIT PREPARATION 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done.
(Cont’d on next page)
A320/321 MEL/CDL
01.28.50 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-01 28-28-01B
ACT Auto Transfer System (Cont’d)
OPERATING PROCEDURES (Cont’d) 2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. -
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD
-
On the FUEL SD page, check that the fuel is transferred from one ACT (from ACT 2 if ACT 2 is installed and not empty) to the center tank.
-
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
30 MIN AFTER TAKEOFF
28-28-01C
ACT fuel not usable
C
1
0
-
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD
-
On the FUEL SD page, check that the fuel is transferred from the ACTs to the center tank.
-
If necessary perform a descent to FL 270.
-
When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
(O)(M) May be inoperative provided that: (FD) 1) The fuel in the ACT(s) is considered as not usable and as part of the ZFW and is taken into account for CG determination, and 2) The ACT transfer valve is secured in the closed position. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.51 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-01 28-28-01C
ACT Auto Transfer System (Cont’d)
OPERATING PROCEDURES ON GROUND OR IN FLIGHT When there is less than 3 000 kg of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD. MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-009
28-28-02
ACT Transfer Valve
28-28-02A
Valve closed with the ACT empty
C
1
0
(FD)
May be inoperative in the closed position provided that there is no fuel in any ACT.
28-28-02C
Valve closed C with the ACT fuel not usable
1
0
(O)(M) May be inoperative provided that: (FD) 1) It is secured in the closed position, and 2) The fuel in the ACT(s) is considered as not usable and as part of the ZFW and is taken into account for CG determination. OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
When there is less than 3 000 kg of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD.
MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-010
A320/321 MEL/CDL
01.28.52 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-03
ACT Transfer Pump
28-28-03A 28-28-04
C
1
0
C
1
0
May be inoperative.
ACT Air Shutoff Valve
28-28-04A
(FD)
May be inoperative provided that the ACT auto transfer system is considered inoperative. Refer to Item 28-28-01 ACT Auto Transfer System
28-28-05
28-28-05A
ACT Inward Pressure Relief Valve Valve open with C fuel in the ACT
1
0
(O)(FD) May be inoperative in the open position provided that: 1) The manual transfer from the ACT(s) to the center tank is operative, and 2) The fuel quantity indications of the ACT(s) and of the center tank are operative on the FUEL SD page. OPERATING PROCEDURES DURING COCKPIT PREPARATION 1. The refuel panel door must be open to check the operation of the manual transfer on the ground using the FUEL SD page. Establish ground communications and ensure that the refuel panel door is open during following check and closed after the check is done. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.53 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-05
28-28-05A
ACT Inward Pressure Relief Valve OPERATING PROCEDURES (Cont’d)
Valve open with fuel in the ACT(Cont’d)
2. The manual transfer may be performed only if the center tank is not full (center tank high level sensor dry). If the center tank is full, the high level sensor may be overridden by keeping pressed in the HI LVL pb test of the refuel panel. When the high level sensor is overridden, take care to not overfill the center tank. Otherwise, fuel may spill out from the surge tanks. -
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · FWD
-
On the FUEL SD page, check that the fuel is transferred from one ACT (from the ACT 2 if the ACT 2 is installed and not empty) to the center tank.
-
ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
AT TOP OF CLIMB Check that the fuel is transferred from the ACTs to the center tank. -
If the automatic transfer has not started: - After 30 min of flight: ACT pb-sw . . . . . . . . . . . . . . . . . . . . . . . . FWD If necessary perform a descent to FL 270.
-
28-28-05B
ACT empty
C
1
0
(FD)
When ACT (both ACTs if two ACTs installed) is empty: ACT pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
May be inoperative provided that there is no fuel in any ACT.
A320/321 MEL/CDL
01.28.54 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-06 28-28-06A
ACT Vent Valve Use of ACT fuel C
1
0
(O)(M) May be inoperative in the open position provided that: 1) The manual transfer from the ACT(s) to the center tank is operative, and 2) The fuel quantity indications of the ACT(s) and of the center tank are operative on the FUEL SD page. OPERATING PROCEDURES Refer to Operating Procedures 28-28-01B ACT Auto Transfer System (Manual transfer from the ACT(s) to the center tank operative) MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-003
28-28-06B
ACT fuel not usable
C
1
0
(O)(M) May be inoperative provided that: (FD) 1) The fuel in the ACT(s) is considered as not usable and as part of the ZFW and is taken into account for CG determination, and 2) The ACT transfer valve is secured in the closed position. OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
When there is less than 3 000 kg of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD.
MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-011
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.55 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-06 28-28-06E 28-28-07
ACT Vent Valve ACT empty
C
1
0
C
1
0
(FD)
May be inoperative provided that there is no fuel in any ACT.
ACT Refuel Valve
28-28-07A
May be inoperative. Note: If the refuel valve is inoperative in the closed position, the ACT cannot be refuelled.
28-28-08 28-28-08A
ACT Integrated Impact Wall Heat shield not C damaged
1
1
(M)
The protection cover of the ACT integrated impact wall may be damaged provided that the heat shield is not damaged. MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-006
A320/321 MEL/CDL
01.28.56 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-09
ACT 1 Inlet Valve
28-28-09B
All ACTs empty C
1
0
(FD)
28-28-09C
ACTs fuel not usable
1
0
(O)(M) May be inoperative in the closed position provided that: (FD) 1) The fuel in the ACT is considered as not usable and as part of the ZFW and is taken into account for CG determination, and
C
May be inoperative in the closed position provided that there is no fuel in the ACT.
2) The ACT transfer valve is secured in the closed position.
OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
When there is less than 3 000 kg of fuel in the center tank: Disregard and clear the FUEL ACT XFR FAULT alert displayed on the EWD.
MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-008
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.57 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System (A320) (ACTs)
28-28-09 28-28-09D
ACT 1 Inlet Valve Use of ACT fuel C
1
0
(M)
May be inoperative in the open position provided that the ACT transfer valve is checked operative before each flight when the ACT is used. MAINTENANCE PROCEDURE Refer to AMM 28-28-00-040-004
28-29
APU LP Fuel Shutoff
28-29-01 28-29-01A
APU LP Fuel Valve Checked closed C on FUEL SD page
1
0
(O)
May be inoperative provided that: 1) It is checked closed on the FUEL SD page, and 2) The APU is not used.
OPERATING PROCEDURES BEFORE ENGINE START The APU is not available. APU MASTER SW pb-sw. . . . . . . . . . . . . . . . . . . . . . . . Off
(Cont’d on next page)
A320/321 MEL/CDL
01.28.58 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-28
Additional Center Tank Transfer System
28-29
APU LP Fuel Shutoff
28-29-01 28-29-01A
APU LP Fuel Valve (Cont’d)
OPERATING PROCEDURES (Cont’d) Note: i.
No APU bleed air will be available for the Main Engine Start (MES) or the air conditioning.
ii. No electrical power will be available from the APU generator. On the FUEL SD page, check that the APU LP valve is indicated closed: Refer to FCOM/DSC-28-20 ECAM FUEL PAGE.
28-29-01B
Secured closed C
1
0
(M)
May be inoperative provided that: 1) It is secured in the closed position, and 2) The APU is not used.
MAINTENANCE PROCEDURE Refer to AMM 28-29-00-040-002
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.59 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-43
Manual Magnetic Indicators
28-43-01
Manual Magnetic Indicators (A320)
28-43-01A
Associated fuel C quantity indication operative on the FUEL SD page
9
0
28-43-01B
High level fuel detection and fuel used indication operative
C
9
0
One or more may be inoperative provided that the associated fuel quantity indication is operative on the FUEL SD page.
(M)
One or more may be inoperative provided that: 1) The high level fuel detection system is checked operative before refueling, and 2) The tanks in both wings are full, and 3) The associated fuel used indication is operative. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-012
28-43-01
Manual Magnetic Indicators (A321)
28-43-01A
Associated fuel C quantity indication operative on the FUEL SD page
7
0
28-43-01B
High level fuel detection and fuel used indication operative
7
0
C
One or more may be inoperative provided that the associated fuel quantity indication is operative on the FUEL SD page.
(M)
One or more may be inoperative provided that: 1) The high level fuel detection system is checked operative before refueling, and 2) The tanks in both wings are full, and 3) The associated fuel used indication is operative. MAINTENANCE PROCEDURE Refer to AMM 28-40-00-040-012
A320/321 MEL/CDL
01.28.60 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-46
Tank Level Sensing
28-46-01
High Level Detection System in the Inner Tank (A320)
28-46-01A
28-46-01
28-46-02A
2
0
One or both may be inoperative provided that the fuel quantity is continuously monitored during refueling.
C
2
0
One or both may be inoperative provided that the fuel quantity is continuously monitored during refueling.
C
1
0
May be inoperative provided that the fuel quantity is continuously monitored during refueling.
High Level Detection System in the Wing Tank (A321)
28-46-01A
28-46-02
C
High Level Detection System in the Center Tank
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.28.61 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-46
Tank Level Sensing
28-46-02
High Level Detection System in the Center Tank (A320) (ACTs)
28-46-02A
C
1
0
May be inoperative provided that: 1) The fuel quantity is continuously monitored during refueling, and 2) The ACT auto inoperative.
transfer
system
is
considered
Refer to Item 28-28-01 ACT Auto Transfer System 28-46-03
High Level Detection System in the ACT (A320) (ACTs)
28-64-03A
28-46-04
28-64-04A
C
1
0
May be inoperative provided that the fuel quantity is continuously monitored during refueling.
C
2
1
One may be inoperative.
Low Level Detection System in the Inner Tank (A320)
A320/321 MEL/CDL
01.28.62 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-46
Tank Level Sensing
28-46-04
Low Level Detection System in the Wing Tank (A321)
28-46-04A 28-46-05
C
2
1
One may be inoperative.
C
1
0
May be inoperative provided that the ACT auto transfer system is considered inoperative.
Low Level Detection System in the ACT (A320) (ACTs)
28-46-05A
Refer to Item 28-28-01 ACT Auto Transfer System 28-50
Fuel Management
28-50-01
28-51-01A
Fuel Quantity Indicating Computer (FQIC) Channel A
2
1
(O)
One may be inoperative for 10 calendar days. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS 1. Ensure that correct weights are entered in the FMGC associated with the affected FQIC channel. 2. In the case of failure in-flight of the remaining FQIC channel, all fuel quantities indications on the EWD are lost. *
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.29.01 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-01
Overhead Panels
29-01-01
HYD Overhead Panel
29-01-01-01 B(Y) ELEC PUMP pb-sw FAULT light 29-01-01-01A
C
2
0
One or both may be inoperative provided that the associated reservoir quantity indication is operative on the HYD SD page. Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the ENG 1(2) PUMP pb-sw FAULT light with engines off may be due to a failed engine oil low pressure switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative. Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert
29-01-01-02 B ELEC PUMP pbsw OFF light 29-01-01-02A
C
1
0
May be inoperative.
1
0
May be inoperative.
29-01-01-03 Y ELEC PUMP pbsw ON light 29-01-01-03A
C
A320/321 MEL/CDL
01.29.02 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-01
Overhead Panels
29-01-01
HYD Overhead Panel
29-01-01-04 G(Y) ENG 1(2) PUMP pb-sw FAULT light 29-01-01-04A
C
2
0
One or both may be inoperative provided that the associated reservoir quantity indication is operative on the HYD SD page. Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the ENG 1(2) PUMP pb-sw FAULT light with engines off may be due to a failed engine oil low pressure switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative. Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert
29-01-01-05 G(Y) ENG 1(2) PUMP pb-sw OFF light 29-01-01-05A
C
2
0
One or both may be inoperative.
C
1
0
May be inoperative provided that the quantity indications of the yellow and green reservoir are operative on the HYD SD page.
C
1
0
May be inoperative.
29-01-01-06 PTU pb-sw FAULT light 29-01-01-06A
29-01-01-07 PTU pb-sw OFF light 29-01-01-07A
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-01
Overhead Panels
29-01-02
Maintenance HYD Overhead Panel
29-01-02-01 G(B)(Y) LEAK MEASUREMENT VALVES pb-sw OFF light 29-01-02-01A 29-07
C
3
0
One or more may be inoperative.
C
1
0
May be inoperative.
C
3
0
One or more may be inoperative.
C
2
0
One or both may be inoperative.
Indications on the HYD SD page
29-07-01
Yellow ELEC Pump Indication on the HYD SD page
29-07-01A 29-07-02
Pump Indication on the HYD SD page
29-07-02A 29-07-03
29-07-03A
Fire Valve Indication on the HYD SD page
01.29.03 HYDRAULIC POWER
A320/321 MEL/CDL
01.29.04 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-07
Indications on the HYD SD page
29-07-04
PTU Indication on the HYD SD page
29-07-04A 29-07-05
C
1
0
C
3
2
May be inoperative.
Reservoir Quantity Indication on the HYD SD page
29-07-05A
(M)
One may be inoperative provided that: 1) The associated HYD B(G)(Y) RSVR LO LVL alert is checked operative, and 2) The associated reservoir quantity is checked before each flight. MAINTENANCE PROCEDURE Refer to AMM task
29-07-06
RAT Indication on the HYD SD page
29-07-06A 29-07-07
29-07-07A
C
1
0
C
3
0
May be inoperative provided that the RAT is visually checked to be stowed before each flight.
System Label Indication on the HYD SD page (O)
One or more may be inoperative provided that the associated system pressure is checked available before each flight. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.29.05 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-07
Indications on the HYD SD page
29-07-07
29-07-07A
System Label Indication on the HYD SD page (Cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: - A Ground cart, or with - The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
-
Move the CAPT stick left or right.
-
On the F/CTL SD page, check the pairs of spoilers movement.
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · OFF
A320/321 MEL/CDL
01.29.06 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-07
Indications on the HYD SD page
29-07-08
29-07-08A
System Pressure Indication on the HYD SD page C
3
2
(O)
One may be inoperative provided that the associated system label indication is checked operative before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available:
-
-
Pressurize the Yellow Hydraulic System with: A Ground cart, or with The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
If the blue system pressure inoperative: Check of the system label:
indication
is
- On the HYD SD page, check that the BLUE system label is amber. - BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . AUTO - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON - On the HYD SD page, check that the BLUE system label is white and that the arrow is green. - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . Off (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.29.07 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-07
Indications on the HYD SD page
29-07-08
29-07-08A
System Pressure Indication on the HYD SD page (Cont’d)
OPERATING PROCEDURES (Cont’d) -
If the yellow system pressure indication is inoperative: Check of the system label: - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off - On the HYD SD page, check that the YELLOW system label is amber. - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - On the HYD SD page, check that the YELLOW system label is white and that the arrow is green. - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
-
If the green system pressure inoperative: Check of the system label:
indication
is
- On the HYD SD page, check that the GREEN system label is amber. - YELLOW ELEC PUMP pb-sw. . . . . . . . . . . . . . . ON - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO - On the HYD SD page, check that the GREEN system label is white and that the arrow is green. - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off
A320/321 MEL/CDL
01.29.08 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-09
ECAM Alerts
29-09-01
HYD B(Y) ELEC PUMP LO PR Alert
29-09-01A 29-09-02
29-09-03A
2
0
One or both may be displayed provided that the associated system pressure indication is operative.
C
2
0
One or both may be displayed.
C
2
0
HYD B(Y) ELEC PUMP OVHT Alert
29-09-02A 29-09-03
C
HYD G(Y) ENG 1(2) PUMP LO PR Alert (O)
One or both may be displayed provided that: 1) The associated system pressure indications are operative, and 2) The engine pumps are checked operative before each flight. OPERATING PROCEDURES AFTER ENGINE START Check of the engines pumps: -
PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
-
On the HYD SD page, check that the green and the yellow hydraulic systems pressures are correct. A correct pressure is 3 000 PSI ( ± 200 PSI).
-
PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.29.09 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-09 29-09-03
ECAM Alerts HYD G(Y) ENG 1(2) PUMP LO PR Alert
29-09-03A (Cont’d))
OPERATING PROCEDURES (Cont’d) Note: On the HYD SD page, the PTU remains indicated running . TAXI Note: Due to a false HYD G(Y) ENG 1(2) PUMP LO PR alert displayed on the EWD, the “T.O CONFIG NORMAL” line will not replace the “T.O CONFIG . . TEST” line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST except a false HYD G(Y) ENG 1(2) PUMP LO PR alert. CAUTION: The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert except a false HYD G(Y) ENG 1(2) PUMP LO PR alert.
A320/321 MEL/CDL
01.29.10 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-09
ECAM Alerts
29-09-04
HYD G(B)(Y) RSVR LO AIR PR Alert
29-09-04A
C
3
2
(M)
One may be inoperative provided that the air pressure is checked on the associated reservoir before each flight. MAINTENANCE PROCEDURE Refer to AMM task
29-09-05
29-09-05A
HYD G(B)(Y) RSVR LO LVL Alert C
3
2
One may be displayed provided that the associated reservoir quantity is checked on the HYD SD page before each flight. Note: i.
When the alert is displayed on the EWD, the associated PUMP pb-sw FAULT light and the PTU pb-sw FAULT light (if the green or the yellow system is affected) may simultaneously come on. Refer to Item 29-01-01-01 B(Y) ELEC PUMP pb-sw FAULT light, and Refer to Item 29-01-01-04 G(Y) ENG 1(2) PUMP pb-sw FAULT light, and Refer to Item 29-01-01-06 PTU pb-sw FAULT light
ii. If the blue reservoir is affected, EMER GEN may appear in the INOP SYS column on the STATUS SD page before engine start.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.29.11 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-09
ECAM Alerts
29-09-06
HYD G(B)(Y) RSVR OVHT Alert
29-09-06A 29-09-07 29-09-07A
C
3
2
C
1
0
The HYD G RSVR OVHT alert or the HYD Y RSVR OVHT alert may be displayed.
HYD PTU FAULT Alert (O)
May be displayed provided that the PTU is checked operative before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: - A Ground cart, or with - The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure. (Cont’d on next page)
A320/321 MEL/CDL
01.29.12 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-09
ECAM Alerts
29-09-07 29-09-07A
HYD PTU FAULT Alert (Cont’d)
OPERATING PROCEDURES (Cont’d) Check of the PTU:
29-09-08
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
-
On the HYD SD page, check that the green hydraulic system pressure indication is green. If the green hydraulic system pressure indication is not available, check on the HYD SD page that the GREEN system label is white and the arrow is green.
-
YELLOW ELEC PUMP pb-sw· · · · · · · · · · · · · · · · · Off
HYD RAT FAULT Alert
29-09-08A
C
1
0
(M)
May be displayed provided that the RAT integrity is checked before each flight. MAINTENANCE PROCEDURE Refer to AMM task
29-09-09
29-09-09A
HYD G(B)(Y)(B+G)(G+ Y)(B+Y) SYS LO PR Alert C
3
0
(O)
One or more may be displayed provided that the associated system pressure is checked available before each flight. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.29.13 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-09
ECAM Alerts
29-09-09
29-09-09A
HYD G(B)(Y)(B+G)(G+Y) (B+Y) SYS LO PR Alert (Cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION Note: If the Yellow Electric Pump is not available: -
Pressurize the Yellow Hydraulic System with: - A Ground cart, or with - The Yellow Engine 2 Pump with the Engine 2 running.
-
Replace any action on the YELLOW ELEC PUMP pb-sw by a similar action on the Ground Cart or on the YELLOW ENG 2 PUMP pb-sw in the following procedure.
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · ON
-
BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · AUTO
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · ON
-
PTU pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · AUTO
-
On the CAPT or the F/O side, move the stick left or right.
-
On the F/CTL SD page, check the pairs of spoilers movement.
-
YELLOW ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · Off
-
BLUE PUMP OVRD pb-sw · · · · · · · · · · · · · · · · · · · Off
A320/321 MEL/CDL
01.29.14 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-10
Main Hydraulic Power
29-10-01
Engine Driven Pump
29-10-01A 29-10-02
29-10-03A
2
Both must be operative.
C
2
1
One may be inoperative.
C
1
1
Engine Driven Pump Depressurizatio n Function
29-10-02A 29-10-03
2
Blue System Electric Pump (O)
The automatic control may be inoperative provided that the pump is manually operated. OPERATING PROCEDURES DURING PRELIMINARY COCKPIT PREPARATION -
If the blue electric pump continuously runs: At electrical power supply application: BLUE ELEC PUMP pb-sw · · · · · · · · · · · · · · · · · · · OFF
AFTER ENGINE START BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . . . . . AUTO -
If the blue electric pump does not automatically start: - BLUE PUMP OVRD pb-sw . . . . . . . . . . . . . . . . . ON - On the HYD SD page, check that the blue hydraulic circuit pressure is available.
AFTER ENGINE SHUTDOWN BLUE ELEC PUMP pb-sw . . . . . . . . . . . . . . . . . . . OFF
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.29.15 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-10
Main Hydraulic Power
29-10-04 29-10-04A
Hydraulic System Accumulator No hydraulic fluid leakage
C
3
0
(M)
One or more may be inoperative provided that it is checked that there is no hydraulic fluid leakage in the accumulator nitrogen charging circuit. MAINTENANCE PROCEDURE Refer to AMM 29-10-00-040-007
29-10-04B
Accumulator deactivated
C
3
0
(M)
One or more may be inoperative provided that the affected accumulator is deactivated. MAINTENANCE PROCEDURE Refer to AMM task
29-10-05
Yellow Brake Accumulator
29-10-05A 29-10-07
1
Must be operative.
2
2
Both must be operative.
Engine Pump Fire Valve
29-10-07A 29-10-08
1
Hydraulic System Filter
29-10-08A
One LP filter inoperative
C
8
7
One LP filter may be inoperative.
29-10-08B
Reservoir filling C filter inoperative
8
7
The reservoir filling filter may be inoperative.
A320/321 MEL/CDL
01.29.16 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-10
Main Hydraulic Power
29-10-09
Hydraulic Case Drain Filter
29-10-09A
C
3
2
(M)
One may be inoperative provided that it is removed. MAINTENANCE PROCEDURE Refer to AMM task
29-22
Blue Auxiliary Hydraulic Power
29-22-01
Ram Air Turbine
29-22-01A
29-23
1
1
1
1
Must be operative.
Power Transfer
29-23-01 29-23-01A
Power Transfer Unit (PTU) C
(O)
PTU may continuously run when set to AUTO provided that the operation of the PTU in both directions is checked before the first flight of each day.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.29.17 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-23
Power Transfer
29-23-01 29-23-01A
Power Transfer Unit (PTU) (cont’d)
OPERATING PROCEDURES AFTER ENGINE START Check of the PTU operation: - GREEN ENG 1 PUMP pb-sw . . . . . . . . . . . . . . OFF - On the HYD SD page, check that the green system pressure is correct. A correct pressure is 3 000 PSI (± 200 PSI). - Check the PTU arrow indication. - GREEN ENG 1 PUMP pb-sw . . . . . . . . . . . . . . . On - PTU pb-sw. . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF - YELLOW ENG 2 PUMP pb-sw . . . . . . . . . . . . . OFF - YELLOW ELEC PUMP pb-sw . . . . . . . . . . . . . . . Off - Let the pressure in the yellow hydraulic system decrease to 200 PSI or less. - If the pressure is not below 200 PSI, the indications on the HYD SD page will not be displayed. - PTU pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
(Cont’d on next page)
A320/321 MEL/CDL
01.29.18 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-23
Power Transfer
29-23-01 29-23-01A
Power Transfer Unit (PTU) (Cont’d)
OPERATING PROCEDURES (Cont’d) -
On the HYD SD page, check that the yellow system pressure is correct. A correct pressure is 3 000 PSI (± 200 PSI).
-
Check the PTU arrow indication.
-
YELLOW ENG 2 PUMP pb-sw · · · · · · · · · · · · · · · · On Note: i.
The PTU pressurizes the system to a nominal value of 3 000 PSI PSI (± 200 PSI), but if no consumers are operated the pressure is not constant. The PTU operates in a cycle which keeps the pressure in the hydraulic systems between 2 100 PSI and 3 200 PSI.
ii. For passengers comfort, the PTU may be set to OFF during the taxi after landing provided that both engines hydraulic pumps are operative and running. The PTU must be set back to AUTO before leaving the aircraft. 29-24
Yellow Auxiliary Hydraulic Power
29-24-01 29-24-01A
Yellow System Electric Pump C
1
0
(O)
May be inoperative provided that the associated pb-sw is set to off. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.29.19 HYDRAULIC POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
29 HYDRAULIC POWER 29-24
Yellow Auxiliary Hydraulic Power
29-24-01 29-24-01A
Yellow System Electric Pump (Cont’d)
OPERATING PROCEDURES ON GROUND -
If the pump continuously runs and does not stop when set to off: DOORS/CARGO (T12 on 122 VU) C/B · · · · · · · · · Pull
-
If unsuccessful: - Y HYD/ELEC PUMP/NORM (AB 03 on 123 VU) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Pull - Y HYD/ELEC/PUMP (AB 06 on 123 VU) C/B. . . Pull Note: i.
If the pump continuously runs on the ground, there is a potential overheat situation.
ii. The reset of the C/Bs must be limited to the time required to open or close the cargo doors. *
*
*
A320/321 MEL/CDL
01.29.20 HYDRAULIC POWER 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.30.01 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-00
MAINTENANCE Message on the STATUS SD page
30-00-01
ICE DETECT MAINTENANCE Message
30-00-01A 30-01
One inoperative C
1
-
2
1
ICE DETECT MAINTENANCE message may be displayed on the STATUS SD page.
Overhead Panels
30-01-01
ANTI ICE Overhead Panel
30-01-01-01 ANTI ICE ENG 1(2) pb-sw FAULT light 30-01-01-01A
One inoperative C
(FD)
One may be inoperative provided that the associated engine anti-ice valve is considered inoperative in the closed position. Refer to Item 30-21-01A Engine Anti-Ice Valve
30-01-01-01B
One or both inoperative
C
2
0
(FD)
One or both may be inoperative provided that the associated engine anti-ice valve is considered inoperative in the open position. Refer to Item 30-21-01 Engine Anti-Ice Valve
30-01-01-02
30-01-01-02A
ANTI ICE ENG 1(2) pb-sw ON light C
2
0
One or both may be inoperative.
A320/321
01.30.02 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-01
Overhead Panels
30-01-01
ANTI ICE Overhead Panel
30-01-01-03 ANTI ICE WING pb-sw FAULT light 30-01-01-03A
C
1
0
(O)
May be inoperative provided that the anti-ice “arrow” symbols are operative on the BLEED SD page . OPERATING PROCEDURES DURING COCKPIT PREPARATION Check of the anti-ice "arrow" symbol: - Make sure that the engine bleed air supply system is available. - ANTI ICE WING pb-sw . . . . . . . . . . . . . . . . . . . . ON - On the BLEED SD page, check that the anti-ice "arrow" symbols are displayed amber and disappear after 30 s. - ANTI ICE WING pb-sw . . . . . . . . . . . . . . . . . . . . Off
30-01-01-03B
C
1
0
(M)(FD) May be inoperative provided that the wing anti-ice control valves are deactivated in the closed position and considered inoperative. Refer to Item 30-11-01 Wing Anti-Ice Control Valve MAINTENANCE PROCEDURE Refer to AMM 30-11-00-040-002
30-01-01-04 ANTI ICE WING pb-sw ON light 30-01-01-04A
C
1
0
May be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.30.03 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-01
Overhead Panels
30-01-02
WIPER Overhead Panel
30-01-02-01 Wiper High Speed Function (FAST Position) 30-01-02-01A
C
2
0
One or both may be inoperative provided that the associated low speed function is operative.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
30-01-02-02 Wiper Low Speed Function (SLOW Position) 30-01-02-02A
30-07
Indications on the BLEED SD page
30-07-01
ANTI ICE Indication on the BLEED SD page
30-07-01A 30-07-02
30-07-02A
Arrow Indication on the BLEED SD page
A320/321
01.30.04 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-11
Wing Ice Protection
30-11-01 30-11-01A
Wing Anti-Ice Control Valve Inoperative in the open position
C
2
1
(O)(M) The RH valve may be inoperative in the open position (FD) provided that the associated ECAM procedure is applied. OPERATING PROCEDURES (A321) FLIGHT PREPARATION/LIMITATIONS Flight planning: Increase fuel consumption by: Zp(ft)
5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 4.5%
4.0%
5.0%
4.0%
4.0%
3.5%
3.0%
2.5%
Single engine cruise: Decrease drift down ceilings by: 600 ft when OAT £ ISA 2 300 ft when OAT > ISA Approach climb performance: - When the engine bleed air supply system is closed: No penalty. - When the engine bleed air supply system is open: Decrease maximum climb limiting weight by: 1 100 kg when OAT £ ISA + 5° C 4 500 kg when OAT > ISA + 5° C DURING COCKPIT PREPARATION -
After application of the maintenance procedure: On the BLEED SD page, check that the anti-ice arrow symbol is displayed. The anti-ice arrow symbol may be displayed amber or green. The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.30.05 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-11
Wing Ice Protection
30-11-01 30-11-01A
Wing Anti-Ice Control Valve (Cont’d)
OPERATING PROCEDURES (A321) (Cont’d) BEFORE ENGINE START -
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
-
Start the engine 1.
-
Maintain the X BLEED selector at SHUT during the start of engine 1.
-
Use the CROSS BLEED ENGINE START (Refer to FCOM/PRO-SLP-70 Cross Bleed Engine Start)
-
Apply the procedure associated with the WING ANTI ICE R VALVE OPEN alert displayed on the EWD.
AFTER TAKEOFF -
When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
IN FLIGHT -
In the case of failure of a Bleed Air Supply System: PACK (affected side) pb-sw· · · · · · · · · · · · · · · · · · OFF
AFTER LANDING -
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
A320/321
01.30.06 ICE AND RAIN PROTECTION
MEL/CDL
1.
ITEM
SYSTEM & SEQUENCE OF ITEMS
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-11
Wing Ice Protection
30-11-01
Wing Anti-Ice Control Valve
30-11-01A (cont’d)
OPERATING PROCEDURES (A320) FLIGHT PREPARATION/LIMITATIONS Flight planning: Increase fuel consumption by: Zp(ft)
5 000 10 000 15 000 20 000 25 000 30 000 35 000 40 000
Fuel penalties 4.5%
4.5%
6.0%
4.5%
3.5%
2.5%
2.5%
2.5%
Single engine cruise: Decrease drift down ceilings by: 1100 ft when OAT £ ISA 4500 ft when OAT > ISA Approach climb performance: - When the engine bleed air supply system is closed: No penalty. - When the engine bleed air supply system is open: Decrease maximum climb limiting weight by: 800 kg when OAT £ ISA + 5° C 4 900 kg when OAT > ISA + 5° C DURING COCKPIT PREPARATION -
After application of the maintenance procedure: On the BLEED SD page, check that the anti-ice arrow symbol is displayed. The anti-ice arrow symbol may be displayed amber or green. The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
ITEM
SYSTEM & SEQUENCE OF ITEMS
2.
01.30.07 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-11 30-11-01
Wing Ice Protection Wing Anti-Ice Control Valve
30-11-01A (cont’d)
OPERATING PROCEDURES (A320) (cont’d) BEFORE ENGINE START -
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
-
Start the engine 1.
-
Maintain the X BLEED selector at SHUT during the start of engine 1.
-
Use the CROSS BLEED ENGINE START (Refer to FCOM/PRO-SLP-70 Cross Bleed Engine Start)
-
Apply the procedure associated with the WING ANTI ICE R VALVE OPEN alert displayed on the EWD.
AFTER TAKEOFF -
When above 1 500 ft: Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
IN FLIGHT -
In the case of failure of a Bleed Air Supply System: PACK (affected side) pb-sw· · · · · · · · · · · · · · · · · · OFF
AFTER LANDING -
Apply the automatic recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
MAINTENANCE PROCEDURE Refer to AMM 30-11-00-040-004
A320/321
01.30.08 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-11
Wing Ice Protection
30-11-01 30-11-01B
Wing Anti-Ice Control Valve Inoperative in the closed position
C
2
0
(M)(FD) One or both may be inoperative in the closed position provided tha the aircraft is not operated in known or forecast icing conditions.
MAINTENANCE PROCEDURE Refer to AMM 30-11-00-040-001
30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01A
Engine Anti-Ice Valve Inoperative in the closed position
C
2
1
(M)(FD) One may be inoperative in the closed position provided that the aircraft is not operated in known or forecast icing conditions.
MAINTENANCE PROCEDURE Refer to AMM 30-21-00-040-001
A320/321 1.
SYSTEM & SEQUENCE OF ITEMS
01.30.09 ICE AND RAIN PROTECTION
MEL/CDL
30 JUN 12 MEL 2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01B
Engine Anti-Ice Valve Inoperative in the open position
C
2
0
(O)(M) One or both may be inoperative in the open position (FD) provided that the Flight Manual performance penalties are applied. OPERATING PROCEDURES (A321) GENERAL INFORMATION An higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the open position. FLIGHT PREPARATION/LIMITATIONS Note: i.
For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch or use the following penalties for takeoff and landing performance determination if MTTL charts are not available.
ii. Performance penalties apply whatever one or both valves are inoperative. Takeoff performance: Perform the takeoff using full thrust (TOGA). (Cont’d on next page)
A320/321
01.30.10 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01B
Engine Anti-Ice Valve (Cont’d)
OPERATING PROCEDURES (A321) (Cont’d) Apply the following reductions on the MTOW and the speeds : OAT(°C)
£ISA+10°C
>ISA+10°C
Weight decrement (kg)
900
5100
V1, VR and V2 decrement (kg)
1
5
Flight planning: Increase fuel consumption by: Zp (ft)
2 Valves blocked OPEN
1 Valve blocked OPEN
5 000
7.0%
3.5%
10 000
5.0%
2.5%
15 000
5.5%
3.0%
20 000
4.0%
2.0%
25 000
4.0%
2.0%
30 000
3.5%
2.0%
35 000
3.5%
2.0%
40 000
3.5%
2.0%
Single engine cruise: Decrease drift down ceilings by: 300 ft when OAT£ ISA + 5°C 2 400 ft when OAT > ISA + 5°C (Cont’d on next page)
A320/321 1.
SYSTEM & SEQUENCE OF ITEMS
01.30.11 ICE AND RAIN PROTECTION
MEL/CDL
12 FEB 12 MEL
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01B
Engine Anti-Ice Valve (Cont’d)
OPERATING PROCEDURES (A321) (Cont’d) Approach climb performance: Decrease maximum climb limiting weight by: 700 kg when OAT £ ISA + 10 °C 5 900 kg when OAT > ISA + 10°C DURING COCKPIT PREPARATION ANTI ICE ENG (affected) pb-sw. . . . . . . . . . . . . . . ON AFTER ENGINE START The FADEC commands the continuous ignition on the affected engine.
OPERATING PROCEDURES (A320)
GENERAL INFORMATION An higher idle speed is set on both engines when an engine anti-ice valve is inoperative in the open position.
(Cont’d on next page)
A320/321
01.30.12 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01B
Engine Anti-Ice Valve (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d)
FLIGHT PREPARATION/LIMITATIONS
Note: i.
For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch or use the following penalties for takeoff and landing performance determination if MTTL charts are not available.
ii. Performance penalties apply whatever one or both valves are inoperative. Takeoff performance: Perform the takeoff using full thrust (TOGA). Apply the following reductions on the MTOW and the speeds : OAT(°C)
£ISA+10°C
ISA+10°C< OAT£ ISA+20°C
>ISA+20°C
Weight decrement (kg)
1100
2000
3200
V1, VR and V2 decrement (kg)
1
1
2
(Cont’d on next page)
A320/321 1.
SYSTEM & SEQUENCE OF ITEMS
01.30.13 ICE AND RAIN PROTECTION
MEL/CDL
12 FEB 12 MEL
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01B
Engine Anti-Ice Valve (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d) Flight planning: Increase fuel consumption by: Zp (ft)
2 Valves blocked OPEN
1 Valve blocked OPEN
5 000
5.5%
3.0%
10 000
4.5%
2.5%
15 000
4.0%
2.0%
20 000
3.0%
1.5%
25 000
3.0%
1.5%
30 000
2.0%
1.0%
35 000
2.0%
1.0%
40 000
2.0%
1.0%
Single engine cruise: Decrease drift down ceilings by: 400 ft when OAT£ ISA + 5°C 3 700 ft when OAT > ISA + 5°C Approach climb performance: Decrease maximum climb limiting weight by: 300 kg when OAT £ ISA + 10 °C 4 400 kg when OAT > ISA + 10°C (Cont’d on next page)
A320/321
01.30.14 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-21
Engine Air Intake Ice Protection
30-21-01 30-21-01B
Engine Anti-Ice Valve (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d) DURING COCKPIT PREPARATION ANTI ICE ENG (affected) pb-sw. . . . . . . . . . . . . . . ON AFTER ENGINE START The FADEC commands the continuous ignition on the affected engine.
MAINTENANCE PROCEDURE Refer to AMM 30-21-00-040-002 30-31
Probe Ice Protection
30-31-01 30-31-01A
Probe Heat Computer (PHC) Associated probe heating operative
C
3
2
(M)
One may be inoperative provided that the associated probe heating is checked operative before each flight. MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-001
A320/321 1.
SYSTEM & SEQUENCE OF ITEMS
01.30.15 ICE AND RAIN PROTECTION
MEL/CDL
12 FEB 12 MEL 2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-31
Probe Ice Protection
30-31-01 30-31-01B
Probe Heat Computer (PHC) F/O PHC inoperative
B
3
2
(O)(M) The F/O PHC may be inoperative provided that the ADRs, heaters and failure alerts associated with the operative computers are checked operative every day. OPERATING PROCEDURES DURING COCKPIT PREPARATION AIR DATA selector· · · · · · · · · · · · · · · · · · · · · · · · F/O 3 IN FLIGHT -
If icing conditions are encountered: ADR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
CAUTION When ADR 2 is set to OFF, takeoff in CONF 1+F is not permitted. The ADR 2 pb-sw must remain set to OFF for the remainder of the flight.
MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-005
A320/321
01.30.16 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-31
Probe Ice Protection
30-31-01 30-31-01C
Probe Heat Computer (PHC) STBY PHC inoperative
C
3
2
(M)(FD) The STBY PHC may be inoperative provided that: 1) The ADRs, heaters and failure alerts associated with the operative computers are checked operative every day, and 2) The aircraft is not operated in visible moisture or in known or forecast icing conditions, and 3) The OAT at the departure airport is above 5 °C when the taxiway or the runway are contaminated with water or slush. MAINTENANCE PROCEDURE AMM 30-31-00-040-005
30-31-02 30-31-02A
Pitot Heater F/O pitot heater B inoperative
3
2
(O)(M) The F/O pitot heater may be inoperative provided that the (FD) ADRs, heaters and failure alerts associated with the CAPT and the STBY probes (pitot, static, AOA, TAT) are checked operative every day. OPERATING PROCEDURES Refer to Operations Procedures 30-31-01B Probe Heat Computer MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-002
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.30.17 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-31
Probe Ice Protection
30-31-02 30-31-02B
Pitot Heater CAPT pitot heater inoperative
B
3
2
(M)(FD) The CAPT pitot heater may be inoperative provided that: 1) The ADRs, heaters and failure alerts associated with the F/O and the STBY probes (pitot, static, AOA, TAT) are checked operative every day, and 2) The aircraft is not operated in visible moisture or in known or forecast icing conditions.
MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-002
30-31-02C
STBY pitot heater inoperative
B
3
2
(M)(FD) The STBY pitot heater may be inoperative provided that: 1) The ADRs, heaters and failure alerts associated with the CAPT and the F/O probes (pitot, static, AOA, TAT) are checked operative every day, and 2) The aircraft is not operated in visible moisture or in known or forecast icing conditions.
MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-002
A320/321
01.30.18 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-31
Probe Ice Protection
30-31-03
Static Ports Heater
30-31-03A
One STBY static port heater inoperative
C
6
5
One STBY static ports heater may be inoperative.
30-31-03B
Both STBY static port heater inoperative
C
6
4
(M)(FD) Both STBY static ports heaters may be inoperative provided that: 1) The ADRs, heaters and failure alerts associated with the CAPT and the F/O probes (pitot, static, AOA, TAT) are checked operative every day, and 2) The OAT at the departure airport is above 5 °C when the runway is contaminated with water or slush. MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-003
30-31-03C
One or both F/O static port heater inoperative
C
6
5
(O)
One F/O static port heaters may be inoperative provided that the ADRs, heaters and failure alerts associated with the CAPT and the STBY probes (pitot, static, AOA, TAT) are checked operative every day. OPERATING PROCEDURES Refer to Operations Procedures 30-31-01B Probe Heat Computer
30-31-03D
One or both CAPT static port heater inoperative
C
6
5
(M)(FD) One CAPT static port heaters may be inoperative provided that: 1) The ADRs, heaters and failure alerts associated with the F/O and the STBY probes (pitot, static, AOA, TAT) are checked operative every day, and 2) The OAT at the departure airport is above 5 °C when the runway is contaminated with water or slush. MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-003
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.30.19 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-31
Probe Ice Protection
30-31-04
30-31-04A
Angle of Attack (AOA) Probes Heating F/O AOA inoperative
C
3
2
(O)(M) The F/O AOA probes heating may be inoperative provided (FD) that the ADRs, heaters and failure alerts associated with the CAPT and the STBY probes (pitot, static, AOA, TAT) are checked operative every day. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability CAT II, if icing conditions are encountered during the flight. RVSM operation are not permitted. DURING COCKPIT PREPARATION AIR DATA selector· · · · · · · · · · · · · · · · · · · · · · · · F/O 3 MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-004
30-31-04B
STBY AOA inoperative
C
3
2
(O)(M) The STBY AOA probes heating may be inoperative provided that the ADRs, heaters and failure alerts associated with the CAPT and the F/O probes (pitot, static, AOA, TAT) are checked operative every day OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-004
A320/321
01.30.20 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-31
Probe Ice Protection
30-31-04
30-31-04C
Angle of Attack (AOA) Probes Heating CAPT AOA inoperative
C
3
2
(O)(M) The CAPT AOA probes heating may be inoperative (FD) provided that: 1) The ADRs, heaters and failure alerts associated with the F/O and the STBY probes (pitot, static, AOA, TAT) are checked operative every day, and 2) The aircraft is not operated in visible moisture or in known or forecast icing conditions. OPERATING PROCEDURES Landing capability is CAT II.
MAINTENANCE PROCEDURE Refer to AMM 30-31-00-040-004
30-31-05
TAT Probes Heating
30-31-05A
One inoperative C
2
1
30-31-05B
Both inoperative
2
0
C
One may be inoperative.
(FD)
Both may be inoperative provided that the aircraft is not operated in visible moisture or in known or forecast icing conditions.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.30.21 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-42
Windshield AntiIcing and Defogging
30-42-01 30-42-01A
Window Heat Computer C
2
1
(O)(M) One may be inoperative provided that: (FD) 1) The aircraft is not operated in known or forecast icing conditions, and 2) All heaters and failure alerts on the front and sliding windows associated with the operative computer are checked operative every day.
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I when the PF side is inoperative. Landing capability is CAT II when the PNF side is inoperative.
MAINTENANCE PROCEDURE Refer to AMM 30-42-00-040-001
A320/321
01.30.22 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-42
Windshield Anti-Icing and Defogging
30-42-02
Fixed Lateral Window and Sliding Window Heating
30-42-02A 30-42-03
C
4
0
C
2
1
One or more may be inoperative.
Windshield Heating
30-42-03A
(O)(FD) One may be inoperative provided that the aircraft is not operated in known or forecast icing conditions. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I when the PF side is inoperative. Landing capability is CAT II when the PNF side is inoperative.
30-42-04
PROBES/ WINDOW HEAT pb-sw AUTO Control
30-42-04A 30-42-05
30-42-05A
C
1
0
Automatic control may be inoperative provided that the PROBES/WINDOW HEAT system is manually selected.
C
1
0
May be inoperative provided that PROBES/WINDOW HEATautomatic system is operative.
PROBES/ WINDOW HEAT pb-sw ON light
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.30.23 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-45
Windshield Rain Protection
30-45-01
Windshield Wiper
30-45-01A
One inoperative A on the PNF side
2
1
30-45-01B
One inoperative C on the PNF side
2
0
One may be inoperative on the PNF side for three flights. (O)(FD) One or both may be inoperative provided that: 1) The aircraft is not operated in precipitation within departure and arrival areas, and 2) The approach minima do not require their use. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT 1 when the wiper and the rain repellent are inoperative or deactivated on the PF side.
30-45-01C
30-45-02
Rain repellent system operative
B
2
1
One may be inoperative provided that the associated rain repellent system is installed and operative.
C
2
0
One or both may be inoperative provided that the associated wipers can be positioned in a location that will not obstruct forward vision.
2
0
Windshield Wiper PARK Function
30-45-02A
One or both inoperative
30-45-02B
One or both inoperative and removed
(M)
One or both may be inoperative provided that the associated wipers are removed. Refer to Item 30-45-01 Windshield Wiper MAINTENANCE PROCEDURE Refer to AMM 30-45-00-040-003
A320/321
01.30.24 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-45
Windshield Rain Protection
30-45-03
Rain Repellent System
30-45-03A
C
2
0
One or both may be inoperative. Note: No entry in the logbook is required when it is installed but intentionally deactivated.
30-71
Waste Water Ice Protection
30-71-01
Waste Water Drain Mast Heating System
30-71-01A
C
2
0
(M)(FD) One or both may be inoperative provided that: 1) The associated galleys and lavatories are not used, and 2) The associated lavatory water supplies are closed. MAINTENANCE PROCEDURE Refer to AMM 30-71-00-040-001
30-71-02
30-71-02A
Waste Water Drain Line Ice Protection System C
1
0
May be inoperative.
A320/321 1.
SYSTEM & SEQUENCE OF ITEMS
01.30.25 ICE AND RAIN PROTECTION
MEL/CDL
12 FEB 12 MEL 2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-81
Ice Detection
30-81-01
Ice Detection System
30-81-01A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES IN FLIGHT The presence of ice in the vicinity of the windshield and on the wipers is periodically checked.
30-81-02
External Visual Icing Indicator
30-81-02A 30-81-03
30-81-03A
C
1
0
C
1
0
The presence of ice in the vicinity of the winsheild and on the wipers is periodically checked.
Lighting of External Visual Icing Indicator (O)(FD) May be inoperative. IN FLIGHT -
If icing conditions are expected during night operations: Refer to FCOM limitation for Icing Conditions
*
*
*
A320/321
01.30.26 ICE AND RAIN PROTECTION
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.31.01 INDICATING/RECORDING SYSTEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDIG SYSTEMS 31-00
MAINTENANCE Message on the STATUS SD page
31-00-01
QAR MAINTENANCE Message
31-00-01A 31-00-02
31-00-05A
QAR MAINTENANCE message may be displayed on the STATUS SD page.
C
1
-
ACMS MAINTENANCE message may be displayed on the STATUS SD page.
C
1
-
DAR MAINTENANCE message may be displayed on the STATUS SD page.
C
1
-
CFDIU MAINTENANCE message may be displayed on the STATUS SD page.
C
2
-
DMC 1/3 MAINTENANCE message may be displayed on the STATUS SD page provided that the DMC 2/3 MAINTENANCE message is not displayed on the STATUS SD page.
CFDIU MAINTENANCE Message
31-00-04 31-00-05
-
DAR MAINTENANCE Message
31-00-03A 31-00-04
1
ACMS MAINTENANCE Message
31-00-02A 31-00-03
C
DMC 1/3 MAINTENANCE Message
A320/321
01.31.02 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-00
MAINTENANCE Message on the STATUS SD page
31-00-06
DMC 2/3 MAINTENANCE Message
31-00-06A
31-05
C
2
-
DMC 2/3 MAINTENANCE message may be displayed on the STATUS SD page.
Indications on the Primary Flight Display (PFD)
31-05-01
AP Related Indications on the FMA
31-05-01A 31-05-02
Refer to MEL Item 22-05-01 AP Related Indications on the FMA. A/THR Related Indications on the FMA
31-05-03A 31-05-04 31-05-04A
Refer to MEL Item 22-05-03 Approach and Landing Capabilities on the FMA. Special Messages on the FMA Refer to MEL Item 22-05-04 Special Messages on the FMA.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.31.03 INDICATING/RECORDING SYSTEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-05
Indications on the Primary Flight Display (PFD)
31-05-05
Actual Airspeed Reference Line and Scale Indications on the PFD
31-05-05A 31-05-06
Refer to MEL Item 34-05-01 Actual Airspeed Reference Line and Scale Indication on the PFD Mach Number Indication on the PFD
31-05-06a 31-05-07
Refer to MEL Item 34-05-02 Mach Number Indication on the PFD. VMO/MMO Characteristic Speed Indication on the PFD
31-05-07A 31-05-08
Refer to MEL Item 34-05-03 VMO/MMO Characteristic Speed Indication on the PFD. Altitude Indication on the PFD
31-05-08A 31-05-09
31-05-09A
Refer to MEL Item 34-05-04 Altitude Indication on the PFD. Vertical Speed Indication on the PFD Refer to MEL Item 34-05-06 Vertical Speed in Inertial Mode Indication on the PFD
A320/321
01.31.04 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-05
Indications on the Primary Flight Display (PFD)
31-05-10
Other Air Data Related Indications on the PFD
31-05-10A 31-05-11
Refer to MEL Item 34-05-07 Other Air Data Related Indications on the PFD. Attitude Indication on the PFD
31-05-11A 31-05-12
Refer to MEL Item 34-05-08 Attitude Indication on the PFD. Heading Indication on the PFD
31-05-12A 31-06
Refer to MEL Item 34-05-09 Heading Indication on the PFD.
Indications on the Navigation Display (ND)
31-06-01
Ground Speed Indication on the ND
31-06-01A 31-06-02
31-06-02A
Refer to MEL Item 34-06-01 Ground Speed Indication on the ND. True Air Speed Indication on the ND Refer to MEL Item 34-06-02 True Air Speed Indication on the ND.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.31.05 INDICATING/RECORDING SYSTEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-06
Indications on the Navigation Display (ND)
31-06-04
Heading Indication on the ND
31-06-04A 31-06-05
Refer to MEL Item 34-06-04 Heading Indication on the ND. Position (Aircraft Symbol) Indication on the ND
31-06-05A 31-06-06
Refer to MEL Item 34-06-05 Position (Aircraft Symbol) Indication on the ND. Navigation Station Information on the ND
31-06-06A 31-06-07
Refer to MEL Item 34-06-06 Radio Navaids Indications on the ND. Chrono Indication on the ND
31-06-07A 31-07
Refer to MEL Item 34-06-07 Chrono Indication on the ND.
Indications on the System Display (SD)
31-07-01
31-07-01A
Indications on the System Display pages Refer to corresponding item in the associated ATA chapter.
A320/321
01.31.06 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-07
Indications on the System Display (SD)
31-07-02
Permanent Data (TAT, SAT, ISA, GLOAD - ALT SEL, UTC, GW) Indications on the SD
31-07-02A
C
7
1
(O)
TAT indication must be available. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check that the TAT value is operative on the SD permanent data. -
If the TAT value is not operative: Check that the TAT value is available through the ADR 3. Note: Use the AIR DATA SWITCHING selector to display temporarily the TAT value on the SD.
IN FLIGHT -
31-08
If needed: The TAT value may be displayed through the same action on the AIR DATA SWITCHING selector.
Indications on the Engine Warning Display (EWD)
31-08-01
31-08-01A
Engine Parameter Indications on the EWD Refer to MEL item 77-08
A320/321
01.31.07 INDICATING/RECORDING SYSTEMS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-08
Indications on the Engine Warning Display (EWD)
31-08-02
Fuel On Board (FOB) Indication on the EWD
31-08-02A 31-08-03
Refer to MEL Item 28-07-01-01 Fuel On Board (FOB) Indication on the FUEL SD page. MEMO Messages on the EWD
31-08-03A 31-08-04
C
7
0
One or more may be inoperative.
Slats/Flaps Position Indications on the EWD
31-08-04A
Refer to MEL Item 27-08-01 Flap Position Indication on the EWD. Refer to MEL Item 27-08-02 Slat Position Indication on the EWD. Note: Apply both MEL Items.
31-20
Independent Instruments
31-20-01 31-20-01A
Electrical Clock Indicator C
1
0
(O)
May be inoperative provided that: 1) The UTC indication from the CFDIU is operative on the permanent data of the SD, and 2) A chrono indication is operative on at least one ND. (Cont’d on next page)
A320/321
01.31.08 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-20
Independent Instruments
31-20-01 31-20-01A
Electrical Clock Indicator (Cont’d)
OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
31-30
After any electrical power interruption resulting in the loss of the UTC on the SD: Initialize the UTC and the date using the MCDU: Refer to FCOM /DSC-45-20-GMT/Date Initialization.
Centralized Fault Display System (CFDS) and Data Recording System
31-30-01
Centralized Fault Display System (CFDS)
31-30-01A 31-30-02 31-30-02A
C
1
0
May be inoperative.
Digital AIDS Recorder (DAR) Refer to MEL Item 31-00-03 DAR MAINTENANCE Message Note: Failure of DAR is indicated by a MAINTENANCE message on the STATUS SD page.
A320/321
01.31.09 INDICATING/RECORDING SYSTEMS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-30
Centralized Fault Display System (CFDS) and Data Recording System
31-30-03
Digital Flight Data Recorder (DFDR)
31-30-03A
A
1
0
May be inoperative provided: 1) Cockpit voice Recorder (VCR) is operative, 2) Airplane is not dispatched from JED, RUH, DMM, MED, and 3) Repair are made within 3 flight days.
31-30-04
Data Management Unit (DMU) part of Flight Data Interface and Management Unit(FDIMU)
31-30-04 31-30-05
31-30-05A
C
1
0
A
1
0
May be inoperative.
Flight Data Interface Unit (FDIU) Note: If FDIU is inoperative the DFDR and the QAR are inoperative. Refer to Item 31-30-03 Digital Flight Data Recorder (DFDR), and Refer to Item 31-30-06 Quick Access Recorder (QAR)
A320/321
01.31.10 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-30
Centralized Fault Display System (CFDS) and Data Recording System
31-30-06
Quick Access Recorder (QAR)
31-30-06A
Refer to Item 31-00-01 QAR MAINTENANCE Message Note: Failure of QAR is indicated by a MAINTENANCE message on the STATUS SD page.
31-30-07
Printer
31-30-07A
31-38
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
Up and Down Data Loading System Acquisition/Interface and Equipment
31-38-01
DATA LOADING selector
31-38-01A 31-38-02
31-38-02A
Data Loading Routing Box (DLRB)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.31.11 INDICATING/RECORDING SYSTEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-38
Up and Down Data Loading System Acquisition/Interfa ce and Equipment
31-38-03
Multipurpose Disk Drive Unit (MDDU)
31-38-03A
31-53
C
1
0
C
2
1
May be inoperative.
Flight Warning Computer (FWC)
31-53-01
Flight Warning Computer (FWC)
31-53-01A
(O)
FWC 2 may be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II.
31-53-02
MASTER CAUT Cancel Function
31-53-02A 31-53-03
31-53-04A
2
1
One may be inoperative.
C
2
1
One may be inoperative.
C
2
1
One may be inoperative.
MASTER WARN Cancel Function
31-53-03A 31-53-04
C
MASTER CAUT light
A320/321
01.31.12 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-53-05
MASTER WARN light
31-53-05A 31-53-06 31-53-06A
C
2
1
B
2
1
One may be inoperative.
Altitude Alert (O)
One altitude alert function May be ioperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS -
31-53-06B
A
2
0
When both altitude alert functions are inoperative: RVSM operations are not permitted.
(O)(FD) Both altitude alert functions may be inoperative provided: 1) Autopilot with altitude hold is operative, 2) Flight is not conducted within RVSM airspace, 3) Enroute operations do not require its use, and 4) Repairs are made within one flight days. OPERATING PROCEDURES: 1. Flight crew must be aware that the usual alerts for altitude deviations will not occur. 2. PM should call out approaching and departing assigned altitudes. 3. RVSM operations are not allowed.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.31.13 INDICATING/RECORDING SYSTEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-55
System Data Acquisition Concentrator (SDAC)
31-55-01
System Data Acquisition Concentrator (SDAC)
31-55-01A
31-56
C
2
1
SDAC 2 may be inoperative.
C
11
0
One or more may be inoperative.
1
1
Must be operative.
ECAM Control Panel (ECP)
31-56-01
System Page Manual Call pb on the ECP
31-56-01A
31-56-02 31-56-02A
ALL pb on the ECP
A320/321
01.31.14 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-56
ECAM Control Panel (ECP)
31-56-03
CLR pb on the ECP
31-56-03A 31-56-04
C
2
1
One may be inoperative.
1
1
Must be operative.
1
1
Must be operative.
C
1
0
Must be operative.
C
1
0
EMER CANC pb on the ECP
31-56-04A 31-56-05
RCL pb on the ECP
31-56-05A 31-56-06
STS pb on the ECP
31-56-06A 31-56-07 31-56-07A
T.O CONFIG pb on the ECP (O)
May be inoperative. OPERATING PROCEDURES BEFORE TAKEOFF Check that the configuration: -
aircraft
is
in
the
correct
takeoff
FLAPS/SLATS· · · · · · · · · · · · · · · · · · · · · · · · · CHECK (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.31.15 INDICATING/RECORDING SYSTEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-56
ECAM Control Panel (ECP)
31-56-07 31-56-07A
T.O CONFIG pb on the ECP (Cont’d)
OPERATING PROCEDURES (Cont’d) -
On EWD, check that the FLAPS position corresponds to the position inserted in the MCDU PERF TAKE OFF Page.
-
PITCH TRIM· · · · · · · · · · · · · · · · · · · · · · · · · · · CHECK
-
Check that the selected pitch trim is in the green band of the pitch trim wheel and corresponds to the value inserted in the MCDU PERF TAKE OFF Page.
-
RUDDER TRIM · · · · · · · · · · · · · · · · · · · CHECK ZERO
-
SPEED BRAKE leve · · · · · · · · · · · · · · · · CHECK RET
-
SIDESTICK PRIORITY light · · · · · · · CHECK NO RED
-
On the WHEEL SD page, check that the brakes temperature is below 300 °C.
-
DOORS · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · CHECK
-
On the DOOR/OXY SD page, check that all doors are indicated closed.
-
Deselect the DOOR/OXY SD page after the check.
A320/321
01.31.16 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-62
Display Management Computer (DMC)
31-62-01 31-62-01B
DMC 1 C
1
0
(O)
May be inoperative provided that: 1) The DMC 2 and DMC 3 are operative, and 2) The ISIS airspeed function is operative, and 3) The ISIS altitude indication is operative, and 4) The ISIS attitude function is operative, and 5) The standby compass is operative, and 6) The EIS DMC SWITCHING selector is set to CAPT 3. OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER LIMIT Or ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY Or NAV ATT(ALT1)(HDG) DISCREPANCY Or NAV FM/GPS POS DISAGREE Or FUEL F.USED/FOB DISAGREE Or MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply the below procedure: - Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to confirm that the alerts are undue. - EIS DMC SWITCHING selector . . . . . . . . . . NORM (Cont’d on next page)
A320/321
01.31.17 INDICATING/RECORDING SYSTEMS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-62
Display Management Computer (DMC)
31-62-01 31-62-01B
DMC 1 (Cont’d)
OPERATING PROCEDURES (Cont’d) Note: CAPT PFD and ND ae lost when EIS DMC SWITCHING selector is set to NORM. -
If the undue ECAM alerts stop: - Pull EIS/DMC3/SPLY (121 VU Q09) C/B and EIS/DMC3/STBY/SPLY (49 VU E10) C/B for more than 5 s and push them back. - EIS DMC SWITCHING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . CAPT 3
-
If the undue ECAM alerts continue: - EIS DMC SWITCHING selector. . . . . . . . . . CAPT 3 - Wait for CAPT PFD and ND recovery. - Pull EIS/DMC2/SPLY (121 VU Q08) C/B for more than 5 s and push it back.
A320/321
01.31.18 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-62
Display Management Computer (DMC)
31-62-02 31-62-02A
DMC 2 C
1
0
(O)(M) May be inoperative provided that: 1) The DMC 1 and DMC 3 are operative, and 2) The ISIS airspeed function is operative, and 3) The ISIS altitude indication is operative, and 4) The ISIS attitude function is operative, and 5) The standby compass is operative, and 6) The EIS DMC SWITCHING selector is set to F/O 3, and 7) The AC ESS FEED control is checked operative every day, and 8) The AC ESS FEED pb-sw FAULT light is checked operative every day. OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVER LIMIT Or ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY Or NAV ATT(ALT1)(HDG) DISCREPANCY Or NAV FM/GPS POS DISAGREE Or FUEL F.USED/FOB DISAGREE Or MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply the below procedure: - Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to confirm that the alerts are undue. - EIS DMC SWITCHING selector . . . . . . . . . . NORM (Cont’d on next page)
A320/321
01.31.19 INDICATING/RECORDING SYSTEMS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-62
Display Management Computer (DMC)
31-62-02
DMC 2
31-62-02A
OPERATING PROCEDURES (Cont’d) Note: CAPT PFD and ND ae lost when EIS DMC SWITCHING selector is set to NORM. -
If the undue ECAM alerts stop: - Pull EIS/DMC3/SPLY (121 VU Q09) C/B and EIS/DMC3/STBY/SPLY (49 VU E10) C/B for more than 5 s and push them back. - EIS DMC SWITCHING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . F/O 3
-
If the undue ECAM alerts continue: - EIS DMC SWITCHING selector . . . . . . . . . . . F/O 3 - Wait for CAPT PFD and ND recovery. - Pull EIS/DMC2/SPLY (49 VU E11) C/B for more than 5 s and push it back.
MAINTENANCE PROCEDURE Refer to AMM 31-68-00-040-005 31-62-03 31-62-03B
DMC 3 C
1
0
(O)
May be inoperative provided that: 1) The DMC 1 and DMC 2 are operative, and 2) The ISIS airspeed function is operative, and 3) The ISIS altitude indication is operative, and 4) The ISIS attitude indication is operative, and 5) The standby compass is operative. (Cont’d on next page)
A320/321
01.31.20 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-62
Display Management Computer (DMC)
31-62-03 31-62-03B
DMC 3 (cont’d)
OPERATING PROCEDURES ON GROUND OR IN FLIGHT -
In the case of multiple undue ECAM alerts concerning ENG 1(2) N1(N2) (EGT)(FF) OVERLIMIT Or ENG 1(2) N1(N2)(EGT)(EPR)(FF) DISCREPANCY Or NAV ATT(ALT1)(HDG) DISCREPANCY Or NAV FM/GPS POS DISAGREE Or FUEL F.USED/FOB DISAGREE Or MINIMUM or HUNDRED ABOVE callouts, possibly associated with EFIS red flags, apply the below procedure: - Crosscheck the affected parameters on the EWD, PFD, ND, or on the related SD page to confirm that the alerts are undue.
-EIS DMC SWITCHING selector . . . . . . . . . . . . . . CAPT 3
(Cont’d on next page)
A320/321
01.31.21 INDICATING/RECORDING SYSTEMS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-62
Display Management Computer (DMC)
31-62-03 31-62-03B
DMC 3 (Cont’d)
OPERATING PROCEDURES (Cont’d)
Note: CAPT PFD and ND ae lost when EIS DMC SWITCHING selector is set to CAPT 3. -
If the undue ECAM alerts stop: - Pull EIS/DMC1/SPLY (49 VU E11) C/B a for more than 5 s and push it back. - EIS DMC SWITCHING selector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
-
If the undue ECAM alerts continue: - EIS DMC SWITCHING selector . . . . . . . . . . NORM - Wait for CAPT PFD and ND recovery. - Pull EIS/DMC2/SPLY (121 VU Q08) C/B for more than 5 s and push it back.
A320/321
01.31.22 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-63
Display Unit (DU)
31-63-01
PFDU 1
31-63-01A 31-63-02
1
1
1
0
Must be operative.
PFDU 2
31-63-02A
C
(O)
May be inoperative provided that PFDU 1, NDU 1, NDU 2, EWDU and SDU are operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I. ON GROUND OR IN FLIGHT PFDU 2 knob · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
31-63-03 31-63-03A
NDU 1 C
1
0
(O)
May be inoperative provided that PFDU 1, PFDU 2, NDU 2, EWDU and SDU are operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I. ON GROUND OR IN FLIGHT NDU 1 knob · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF
A320/321
01.31.23 INDICATING/RECORDING SYSTEMS
MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-63
Display Unit (DU)
31-63-04
NDU 2
31-63-04A 31-63-05 31-63-05A
C
1
0
(O)
May be inoperative provided that PFDU 1, PFDU 2, NDU 1, EWDU and SDU are operative.
A
1
0
(O)(M) May be inoperative for three flight days provided that:
SDU
1) The PFDU 1, PFDU 2, NDU 1, NDU 2 and EWDU are operative, and 2) The AC ESS FEED control is checked operative every day, and 3) The AC ESS FEED pb-sw FAULT light is checked operative every day. OPERATING PROCEDURES ON GROUND OR IN FLIGHT SDU knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF -
In the case of alerts being displayed on the EWD: Use the ECAM/ND SWITCHING selector to display the system page on the selected NDU.
-
In the case of failure of the AC BUS 1: All the Display Units are lost. Apply the ELEC AC ESS BUS FAULT alert procedure: Refer to FCOM/PRO-ABN-24-ELEC AC ESS FAULT. Note: The AC ESS BUS is recovered when the AC ESS FEED pb-sw is set to ALTN.
MAINTENANCE PROCEDURE Refer to AMM 31-68-00-040-006
A320/321
01.31.24 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-63
Display Unit (DU)
31-63-06
EWDU
31-63-06A
31-68
1
1
Must be operative.
C
1
0
May be inoperative provided that the AIR DATA SWITCHING selector is set to NORM.
C
1
0
May be inoperative provided that SWITCHING selector is set to NORM.
C
1
0
May be inoperative provided that:
Switching Panel
31-68-01
AIR DATA SWITCHING selector on the Center Pedestal
31-68-01A 31-68-02
ATT HDG SWITCHING selector on the Center Pedestal
31-68-02A 31-68-03
31-68-03A
the
ATT
HDG
ECAM/ND XFR SWITCHING selector on the Center Pedestal
1) Both ECAM DU are operative, and 2) The ECAM/ND XFR SWITCHING selector is set to NORM.
A320/321
01.31.25 INDICATING/RECORDING SYSTEMS
MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-68
Switching Panel
31-68-04
EIS DMC SWITCHING selector on the Center Pedestal
31-68-04A 31-68-05
31-68-05A
C
1
0
C
2
0
May be inoperative provided that SWITCHING selector is set to NORM.
the
EIS
DMC
PFD/ND XFR pb on the Lateral Instrument Panel (O)
One or both may be inoperative provided that: 1) The PFD and ND units are operative, and 2) The PFD to ND automatic switching is checked operative on the PF side before each flight. OPERATING PROCEDURES DURING COCKPIT PREPARATION -
On the side where the PFD/ND XFR pb is inoperative: - PFD brightness control knob . . . . . . . . . . . . . . . OFF - Check that the PFD image is automatically displayed on the NDU. - PFD brightness control knob . . . . . . . . . . . . . . . . On - If the PFD image is not automatically displayed on the NDU: The affected side cannot be used by the Pilot Flying.
(Cont’d on next page)
A320/321
01.31.26 INDICATING/RECORDING SYSTEMS
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
31 INDICATING/RECORDING SYSTEMS 31-68
Switching Panel
31-68-05
31-68-05A
PFD/ND XFR pb on the Lateral Instrument Panel (Cont’d)
OPERATING PROCEDURES (Cont’d)
-
On the side where the PFD to ND automatic switching is inoperative: - PFD brightness control knob . . . . . . . . . . . . . . . OFF - EIS DMC SWITCHING selector (Affected side. . . . . . . . . . . . . . . . . . CAPT 3 (F/O 3) - Check that the PFD image is displayed on the associated NDU. - PFD brightness control knob . . . . . . . . . . . . . . . . On - EIS DMC SWITCHING knob (Affected side) . . . . . . . . . . . . . . . . . . . . . . . NORM
IN FLIGHT -
If a PFDU fails with no automatic transfer to the associated NDU: - PFD brightness control knob . . . . . . . . . . . . . . . OFF - EIS DMC SWITCHING selector (Affected side) . . . . . . . . . . . . . . . . . CAPT 3 (F/O 3) - Check that the PFD image is displayed on the associated NDU. *
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.01 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page C
4
0
(O)
One or more may be inoperative provided that the ground brake cooling time is applied. OPERATING PROCEDURES (A320) FLIGHT PREPARATION/LIMITATIONS The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time. BRAKE ENERGY GRAPH -
If MAX reverser thrust was selected for all reversers during the braking phase: Enter the brake energy graph: WITH THRUST REVERSERS USE.
-
If MAX reverser thrust was NOT selected for all reversers during the braking phase: Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) : -
Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS.
-
Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING : -
Enter with the aircraft landing weight, and
-
Enter with the touch down speed in kt IAS if the auto brake was selected and applied or with the manual braking speed in kt IAS in the other cases. (Cont’d on next page)
A320/321 MEL/CDL
01.32.02 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d) -
Apply airport pressure altitude, temperature, wind and runway slope corrections.
-
Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases. Note: In the case of a dispatch with one brake inoperative (Refer to Item 32-42-01 Main Wheel Brake or Refer to Item 3242-02 Green System Brake), the brake energy accumulated is increased by 34%. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.03 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
01.32.04 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d)
(Cont’d on next page) D
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.05 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320)(Cont’d) BRAKE COOLING TIME TABLE Determination of the brake cooling time: EXAMPLE: 55
152
153
154
155
155
46
46
46
46
47
==> TIME (min) WITHOUT BRAKE COOLING FAN ==> TIME (min) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row. For Example, with Energy = 78 MJ, and OAT = 15°C, entering the next adjacent column/row (Energy = 80 MJ, OAT = 20°C) gives the following results: -
Without brake cooling fan: 189 min
-
With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time. (Cont’d on next page)
A320/321 MEL/CDL
01.32.06 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320) (Cont’d)
(Cont’d on next page)
D
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.07 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320)(Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
01.32.08 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A320)(Cont’d) AFTER ENGINE START -
In the case of a false BRAKES HOT alert displayed on the EWD: EMER CANC pb · · · · · · · · · · · · · · · · · · · · · · · · · Press Note: In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert were displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
OPERATING PROCEDURES (A321) FLIGHT PREPARATION/LIMITATIONS The brake energy graph and the brake cooling time table given hereafter permit to determine the ground brake cooling time. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.09 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d) BRAKE ENERGY GRAPH -
If MAX reverser thrust was selected for all reversers during the braking phase: Enter the brake energy graph: WITH THRUST REVERSERS USE.
-
If MAX reverser thrust was NOT selected for all reversers during the braking phase: Enter the brake energy graph: WITHOUT THRUST REVERSERS USE.
Determination of the brake energy accumulated during a REJECTED TAKEOFF (RTO) : -
Enter with the aircraft takeoff weight (TOW) and with the rejected takeoff speed in kt IAS.
-
Apply airport pressure altitude, temperature, wind and runway slope corrections.
Determination of the brake energy accumulated during a LANDING : -
Enter with the aircraft landing weight, and
-
Enter with touch down speed in kt IAS if the autobrake was selected and applied or with the manual braking speed in kt IAS in the other cases.
-
Apply airport pressure altitude, temperature, wind and runway slope corrections.
-
Correct for brake setting with a preselected autobrake setting (LO, MED) or with MAX PEDAL braking in the other cases. (Cont’d on next page)
A320/321 MEL/CDL
01.32.10 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d)
Note: In the case of a dispatch with one brake inoperative (Refer to Item 32-42-01 Main Wheel Brake or Refer to Item 3242-02 Green System Brake), the brake energy accumulated is increased by 34%.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.11 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
01.32.12 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.13 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d) BRAKE COOLING TIME TABLE Determination of the brake cooling time: EXAMPLE: 55
152
153
154
155
155
46
46
46
46
47
==> TIME (min) WITHOUT BRAKE COOLING FAN ==> TIME (min) WITH BRAKE COOLING FAN
If the Energy and the OAT are not given in the table, use the values given in the next adjacent column/row. For Example, with Energy = 78 MJ, and OAT = 15°C, entering the next adjacent column/row (Energy = 80 MJ, OAT = 20°C) gives the following results: -
Without brake cooling fan: 189 min
-
With brake cooling fan: 57 min
Enter the following table with the energy and the OAT to determine the ground brake cooling time. (Cont’d on next page)
A320/321 MEL/CDL
01.32.14 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.15 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
01.32.16 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-01
32-07-01A
Brakes Temperature Indication on the WHEEL SD page (Cont’d)
OPERATING PROCEDURES (A321)(Cont’d) AFTER ENGINE START -
In the case of a false BRAKES HOT alert displayed on the EWD: EMER CANC pb · · · · · · · · · · · · · · · · · · · · · · · · · Press Note: In the case of a false BRAKES HOT alert due to a faulty BTMU or a faulty BSCU, the "T.O CONFIG NORMAL” line will not replace the "T.O CONFIG . . TEST" line in the T.O MEMO. Consider normal configuration for takeoff provided that no alert were displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG TEST pb must be maintained pressed to check that there is no alert.
32-07-01B
C
4
0
(O)(M) One or more may be inoperative provided that: 1) The associated sensor is deactivated if the BRAKES HOT alert is displayed on the EWD, and 2) The ground brake cooling time is applied. OPERATING PROCEDURES Refer to MEL item 32-07-01A MAINTENANCE PROCEDURE Refer to AMM 32-47-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.17 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-02
L/G Position Indication on the WHEEL SD page
32-07-02A
32-07-03
C
6
0
C
3
0
One or more may be inoperative provided that the L/G gear position indications are operative on the LDG GEAR indicator panel.
L/G Doors Position Indication on the WHEEL SD page
32-07-03A
(O)
One or more may be inoperative. OPERATING PROCEDURES IN FLIGHT MAX SPEED . . . . . . . . . . . . . . . . . . . . . . . 250 kt or M 0.60
32-07-04
L/G CTL Indication on the WHEEL SD page
32-07-04A 32-07-05
32-07-06A
1
0
May be inoperative.
C
3
0
One or more may be inoperative.
C
2
0
One or both may be inoperative.
UP LOCK Indication on the WHEEL SD page
32-07-05A 32-07-06
C
[Y] N/W STEERING Indication on the WHEEL SD page
A320/321 MEL/CDL
01.32.18 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-07
Tire Pressure Indication on the WHEEL SD page
32-07-07A 32-07-08
32-07-11A
One or more may be inoperative.
C
3
0
One or more may be inoperative.
C
1
0
May be inoperative.
C
2
0
One or both may be inoperative.
C
4
0
One or more may be inoperative.
[G] NORM BRK Indication on the WHEEL SD page
32-07-10A 32-07-11
0
AUTO BRK Indication on the WHEEL SD page
32-07-09A 32-07-10
6
ANTI SKID, [1], [2] Indication on the WHEEL SD page
32-07-08A 32-07-09
C
Release Brake Indication on the WHEEL SD page
12 FEB 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.19 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-07
Indications on the WHEEL SD page
32-07-12
ACCU PRESS/ACCU ONLY Indication on the WHEEL SD page
32-07-12A 32-07-13
C
1
0
May be inoperative.
C
2
0
One or both may be inoperative.
Fault on an C alternate braking system pressure transducer
1
0
May be inoperative provided that:
[Y] ALTN BRK Indication on the WHEEL SD page
32-07-13A 32-09
ECAM Alerts
32-09-01
32-09-01A
BRAKES-N/WS MINOR FAULT Alert
1) The alert is confirmed to be caused by a fault on an alternate braking system pressure transducer by troubleshooting, and 2) The associated BRAKES considered inoperative.
pressure
indicator
Refer to Item 32-44-03 BRAKES Pressure Indicator
is
A320/321 MEL/CDL
01.32.20 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-09
ECAM Alerts
32-09-01
32-09-01C
BRAKES-N/WS MINOR FAULT Alert Both BRAKES pressure indicators operative
B
1
0
(O)(M) May be displayed provided that: 1) Both BRAKES pressure indicators are operative, and 2) The alternate braking system is checked operative before the first flight of each day, and 3) It is checked before each flight that the CFDS failure message related to the BRAKES-N/WS MINOR FAULT alert do not report a fault on an alternate pressure transducer. OPERATING PROCEDURES DURING COCKPIT PREPARATION The ACCU PRESS indication must be in the green band. -
If ACCU PRESS indication not in the green band: Y ELEC PUMP pb-sw · · · · · · · · · · · · · · · ON then OFF
-
CHOCKS · · · · · · · · · · · · · · · · · · · · CHECK IN PLACE
-
PARKING BRAKE handle · · · · · · · · · · · · · · · · · · · OFF
-
PARKING PEDALS · · · · · · · · · · · · · · · · · · · · · PRESS Apply maximum pressure on both pedals.
-
BRAKE PRESSURE (on BRAKES pressure indicators) · · · · · · · · · · CHECK Pressure must increase without delay symmetrically on left and right sides for the same application simultaneously applied on left and right pedals. With full pedal deflection, the pressure must be between 900 and 1100 psi.
-
BRAKES PEDALS · · · · · · · · · · · · · · · · · · · · RELEASE Check that no residual pressure in the brakes remains.
-
PARKING BRAKE handle · · · · · · · · · · · · · · · · · · · · ON
MAINTENANCE PROCEDURE Refer to AMM 32-46-00-040-001
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.21 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-09
ECAM Alerts
32-09-02 32-09-02A
WHEEL TYRE LO PR Alert Associated monitoring channel deactivated
C
1
0
(M)
May be displayed on one or more wheels provided that: 1) The alert is confirmed to be false by troubleshooting, and 2) The associated deactivated, and
pressure
monitoring
channel
is
3) The tire pressure on the affected wheel is checked to be within the limits before the first MEL dispatch and then every three days. MAINTENANCE PROCEDURE Refer to AMM 32-49-00-040-001
32-09-02B
TPIC deactivated
C
1
0
(M)
May be displayed on all wheels provided that: 1) The alert is confirmed to be false by troubleshooting, and 2) The Tire Pressure Indicating Computer (TPIC) is deactivated, and 3) The tire pressure on each wheel is checked to be within the limits before the first MEL dispatch and then every three days. MAINTENANCE PROCEDURE Refer to AMM 32-49-00-040-002
A320/321 MEL/CDL
01.32.22 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-11
Main Gear
32-11-01
Main Gear Torque Link Damper
32-11-01A
32-12
A
2
0
(FD)
One or both may be inoperative for 7 flights.
C
2
0
(M)
One or both may be broken or missing.
Main Gear Doors
32-12-01 32-12-01A
Ground Opening Cable
MAINTENANCE PROCEDURE Refer to AMM 32-12-00-040-006
12 FEB 12 MEL
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.23 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-31
Normal Extension and Retraction
32-31-01
32-31-01A
Landing Gear Control and Interface Unit (LGCIU) A
2
1
(O)(FD) The LGCIU 2 may be inoperative for one flight day provided that: 1) All ELACs, SECs, SFCCs, RAs, FACs, and ADIRSs are operative, 2) Both air conditioning packs are operative, 3) The FLEX Takeoff Mode is not used, 4) The operation of avionics equipment is time limited on ground, 5) Reverser number 2 considered inoperative, 6) Both radio altimeter systems are operative, and 7) Both FCU channels are operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION HYDRAULIC/LGCIU/SYS2 (121VU Q35) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL The following table gives the consequences on the systems affected when the LGCIU 2 is inoperative and above mentioned C/B is pulled.
(Cont’d on next page)
A320/321 MEL/CDL
01.32.24 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-31
Normal Extension and Retraction
32-31-01
32-31-01A
Landing Gear Control and Interface Unit (LGCIU) (Cont’d)
OPERATING PROCEDURES (Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.25 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-31
Normal Extension and Retraction
32-31-01
32-31-01A
Landing Gear Control and Interface Unit (LGCIU) (Cont’d)
OPERATING PROCEDURES (Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
01.32.26 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-31
Normal Extension and Retraction
32-31-01
32-31-01A
Landing Gear Control and Interface Unit (LGCIU) (Cont’d)
OPERATING PROCEDURES (Cont’d) IN FLIGHT -
In the case of loss of the LGCIU 1: AP and FD are lost. Maximum landing capability is CAT I.
32-31-02
Landing Gear Retracting System
32-31-02A
C
1
0
(O)
May be inoperative provided that the aircraft is operated in accordance with the Flight Manual supplement for the flight with landing gear down. OPERATING PROCEDURES Refer to FCOM/PRO-SPO-25 Flight With Gear Down.
32-32
Proximity Detector System
32-32-01 32-32-01A
LGCIU 1 Proximity Detector 16 16
All must be operative.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.27 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-02
32-32-02A
LGCIU 2 RH L/G Shock Absorber Proximity Detector A
1
0
(O)(M) May be inoperative for one flight provided that: (FD) 1) Both radio altimeters are operative, and 2) The other proximity detectors are operative, and 3) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
(Cont’d on next page)
A320/321 MEL/CDL
01.32.28 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-02
32-32-02A
LGCIU 2 RH L/G Shock Absorber Proximity Detector (Cont’d)
OPERATING PROCEDURES (Cont’d)
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
12 FEB 12 MEL
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.29 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-02
LGCIU 2 RH L/G Shock Absorber Proximity Detector
32-32-02B
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
32-32-03
32-32-03A
LGCIU 2 LH L/G Shock Absorber Proximity Detector A
1
0
(O)(M) May be inoperative for one flights provided that: (FD) 1) Both radio altimeters are operative, and 2) The other proximity detectors are operative, and 3) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
(Cont’d on next page)
A320/321 MEL/CDL
01.32.30 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32-03A
(Cont’d)
OPERATING PROCEDURES (Cont’d)
(Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.31 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-03
32-32-03A
LGCIU 2 LH L/G Shock Absorber Proximity Detector (Cont’d)
OPERATING PROCEDURES (Cont’d)
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-03B
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to MEL 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
01.32.32 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-04
32-32-04A
LGCIU 2 Nose L/G Shock Absorber Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-04B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.33 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-05
32-32-05A
LGCIU 2 RH L/G Down Lock Proximity Detector Other proximity C detectors operative
1
0
(O)(M) May be inoperative provided that: 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-05B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
01.32.34 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-06
32-32-06A
LGCIU 2 LH L/G Down Lock Proximity Detector Other proximity C detectors operative
1
0
(O)(M) May be inoperative provided that: 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-06B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.35 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-07
32-32-07A
LGCIU 2 Nose L/G Down Lock Proximity Detector Other proximity C detectors operative
1
0
(O)(M) May be inoperative provided that: 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-07B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
01.32.36 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-08
32-32-08A
LGCIU 2 RH L/G Up Lock Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-08B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.37 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-09
32-32-09A
LGCIU 2 LH L/G Up Lock Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-09B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
01.32.38 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-10
32-32-10A
LGCIU 2 Nose L/G Up Lock Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES GENERAL INFORMATION
MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003 32-32-10B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.39 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-11
32-32-11A
LGCIU 2 RH L/G Doors Open Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES Refer to Operating Procedures 32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
32-32-11B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
32-32-12
32-32-12A
LGCIU 2 LH L/G Doors Open Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES Refer to Operating Procedures 32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
A320/321 MEL/CDL
01.32.40 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-12
32-32-12B
LGCIU 2 LH L/G Doors Open Proximity Detector LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
32-32-13
32-32-13A
LGCIU 2 Nose L/G Doors Open Proximity Detector Other proximity A detectors operative
2
0
(O)(M) One or both may be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES Refer to Operating Procedures 32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
32-32-13B
LGCIU 2 considered inoperative
A
2
0
(FD)
One or both may be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.41 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-14
32-32-14A
LGCIU 2 RH L/G Doors Closed Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative. 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES Refer to Operating Procedures 32-32-08A LGCIU 2 RH L/G Up Lock Proximity Detector MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
32-32-14B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
01.32.42 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-15
32-32-15A
LGCIU 2 LH L/G Doors Closed Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES Refer to Operating Procedures 32-32-09A LGCIU 2 LH L/G Up Lock Proximity Detector MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
32-32-15B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.43 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-32
Proximity Detector System
32-32-16
32-32-16A
LGCIU 2 Nose L/G Doors Closed Proximity Detector Other proximity A detectors operative
1
0
(O)(M) May be inoperative for 7 flights provided that: (FD) 1) The other proximity detectors are operative, and 2) The origin of the failure is checked to be electrical. OPERATING PROCEDURES Refer to Operating Procedures 32-32-10A LGCIU 2 Nose L/G Up Lock Proximity Detector MAINTENANCE PROCEDURE Refer to AMM 32-31-00-040-003
32-32-16B
LGCIU 2 considered inoperative
A
1
0
(FD)
May be inoperative for one flight provided that the LGCIU 2 is considered inoperative. Refer to Item 32-31-01 Landing Gear Control and Interface Unit (LGCIU)
32-33
Free Fall Extension
32-33-01
32-33-01A
Landing Gear Gravity Extension System C
1
0
(O)
May be inoperative provided that the aircraft is operated in accordance with the Flight Manual supplement for the flight with landing gear down. OPERATING PROCEDURES Refer to FCOM/SPO-25 Flight With Gear Down.
A320/321 MEL/CDL
01.32.44 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-41
Wheels
32-41-01
Nose Wheel Tie Bolt
32-41-01A
A
12 11 (M)(FD) One tie bolt on one wheel may be broken or missing for 15 flights provided that: 1) The affected wheel tie bolt is removed, and 2) The affected wheel and the associated brake are checked for absence of damage. MAINTENANCE PROCEDURE Refer to AMM 32-41-00-040-002
32-41-02 32-41-02A
Main Wheel Tie Bolt A
18 17 (M)(FD) One tie bolt on one wheel may be broken or missing for 15 flights provided that: 1) The affected wheel tie bolt is removed, and 2) The affected wheel and the associated brake are checked for absence of damage. MAINTENANCE PROCEDURE Refer to AMM 32-41-00-040-003
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.45 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-42-01 32-42-01A
Main Wheel Brake C
4
3
(O)(M) One may be inoperative provided that: (FD) 1) The nose wheel steering is operative, and 2) Both thrust reversers are operative, and 3) The green and yellow systems are operative on operative brakes, and 4) The affected brake is deactivated or removed, and 5) The runway width at departure and arrival airports is at least 45 m, and 5) The Flight applied,and
Manual
performance
penalties
are
6) Anti-skid system is operative and Wheel tachometers are operative.
(Cont’d on next page)
A320/321 MEL/CDL
01.32.46 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-42-01 32-42-01A
Main Wheel Brake (Cont’d)
OPERATING PROCEDURES (A320) FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch. Landing performance computation: Increase the landing distances by 20 %. FOR TAKEOFF The autobrake function, even if available, must not be used. Performed the takeoff using full thrust (TOGA). -
In the case of engine failure at takeoff: Retract the landing gear when positive climb. Vibrations may occur during 1 or 2 min after the retraction of the landing gear.
-
If both engines are operative: Keep the landing gear down for 1 min.
FOR LANDING The autobrake function, even if available, must not be used.
(Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.47 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-42-01 32-42-01A
Main Wheel Brake (Cont’d)
OPERATING PROCEDURES (A321) For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch. Landing performance computation: Increase the landing distances by 20 %. FOR TAKEOFF The autobrake function, even if available, must not be used. Performed the takeoff using full thrust (TOGA).
-
In the case of engine failure at takeoff: Retract the landing gear when positive climb. Vibrations may occur during 1 or 2 min after the retraction of the landing gear.
-
If both engines are operative: Keep the landing gear down for 1 min.
FOR LANDING The autobrake function, even if available, must not be used. MAINTENANCE PROCEDURE Refer to AMM 32-42-00-040-003
A320/321 MEL/CDL
01.32.48 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-42-02
32-42-02A
Green System Brake
C
1
1
(O)(M) Braking on one wheel may be inoperative provided that: (FD) 1) The nose wheel steering is operative, and 2) Both thrust reversers are operative, and 3) The green hydraulic supply of affected brake is deactivated, and 4) The runway width at departure and arrival airports is at least 45 m, and 5) The Flight Manual performance penalties are applied. OPERATING PROCEDURES Refer to Operating Procedures 32-42-01A Main Wheel Brake MAINTENANCE PROCEDURE Refer to AMM 32-42-00-040-002
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
32 LANDING GEAR 32-42
01.32.49 LANDING GEAR
REMARKS OR EXCEPTIONS
Normal Braking
32-42-03
Braking/Steering Control Unit (BSCU) System 1
32-42-03A
C
1
0
(M)
May be inoperative provided that: 1) The BSCU system 2 is operative, and 2) The affected system is deactivated, and 3) It is checked that the CFDS does not report a fault related to the L/G SYS DISAGREE alert before each flight, and 4) The AUTO/BRK (LO, MED, MAX) pb-sw DECEL light and the AUTO/BRK (LO, MED, MAX) pb-sw ON light are considered inoperative, and 5) Brake pressure indicators is operative, and 6) Alternate brake system checked operative before each depature. Refer to Item 32-42-08 AUTO/BRK (LO, MED, MAX) pb-sw DECEL light, and Refer to Item 32-42-09 AUTO/BRK (LO, MED, MAX) pb-sw ON light MAINTENANCE PROCEDURE Refer to AMM 32-42-00-040-007
32-42-04
32-42-04A
Braking/Steering Control Unit (BSCU) System 2 C
1
0
(M)
May be inoperative provided that: 1) The affected system is deactivated, and 2) It is checked that the CFDS does not report a fault related to the L/G SYS DISAGREE alert before each flight, and (Cont’d on next page)
A320/321 MEL/CDL
01.32.50 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-42-04
Braking/Steering Control Unit (BSCU) System 2
32-42-04A (Cont’d)
3) Brake pressure indicators is operative, and 4) Alternate brake system checked operative before each depature. MAINTENANCE PROCEDURE Refer to AMM 32-42-00-040-007
32-42-05
AUTO/BRK Function
32-42-05A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. BEFORE TAKEOFF When T.O MEMO is displayed on the EWD, disregard the line: AUTO BRK . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX (blue)
32-42-06
Tachometer
32-42-06B
32-42-08
32-42-08A
4
4
Must be operative.
3
0
One or more may be inoperative.
AUTO/BRK (LO, MED, MAX) pb-sw DECEL light C
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.51 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-42-09
AUTO/BRK (LO, MED, MAX) pb-sw ON light
32-42-09A
AUTO/BRK C mode arming displayed on the WHEEL SD page
3
0
One or more may be inoperative provided that, when appropriate, the associated AUTO/BRK mode arming is displayed on the WHEEL SD page.
32-42-09B
AUTO/BRK function considered inoperative
C
3
0
One or more may be inoperative provided that the AUTO/BRK function is considered inoperative.
Refer to Item 32-42-05 AUTO/BRK Function
32-44
Alternate Braking
32-44-01 32-44-01A
Yellow System Brake C
1
1
(M)
Braking on one wheel may be inoperative provided that: 1) Both thrust reversers are operative, and 2) The yellow hydraulic supply of the affected brake is deactivated. MAINTENANCE PROCEDURE Refer to AMM 32-43-00-040-001
A320/321 MEL/CDL
01.32.52 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-44
Alternate Braking
32-44-02
32-44-02A
32-44-02B
ACCU PRESS Indicator
Brakes pressure indicator operative
C
Checks on WHEEL SD page
C
1
0
May be inoperative provided that: 1) Both brakes pressure indicators are operative, and 2) The pressure on both brakes pressure indicators is checked with parking brake ON before each flight.
1
0
May be inoperative provided that: 1) The ACCU PRESS/ACCU ONLY indication operative on the WHEEL SD page, and
is
2) The hydraulic pressure of the brake accumulator is checked on the WHEEL SD page before each flight.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.53 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-42
Normal Braking
32-44-03
BRAKES Pressure Indicator
32-44-03A 32-44-04
C
0
One or both may be inoperative provided that the BSCU system 1 and the BSCU system 2 are operative.
1
1
Must be operative.
2
1
Alternate Braking Control Unit (ABCU)
32-44-04A 32-45
2
Parking/Ultimate Emergency Braking
32-45-01
32-45-01A
Parking Brake Control Valve Electrical Motor C
(M)
One may be inoperative provided that: 1) Both thrust reversers are operative, and 2) The aircraft is not towed if the STBY motor is affected and when the batteries supply the aircraft.
MAINTENANCE PROCEDURE Refer to AMM 32-45-00-040-001
A320/321 MEL/CDL
01.32.54 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-47
Brake Temperature System
32-47-01
Brake Temperature Monitoring Unit (BTMU)
32-47-01A
C
2
0
(O)
One or both may be inoperative provided that the ground brake cooling time is applied. OPERATING PROCEDURES DURING PRELIMINARY COCKPIT PREPARATION HYDRAULIC/BRK/TEMP/DET/UNIT (121VU M26 or M37) C/B. . . . . . . . . . . . . . . . . . . . . . PULL Determine brake cooling time (Refer to OpsProc 32-0701A(B) Brakes Temperature Indication on the WHEEL SD page).
32-48
Brake Cooling
32-48-01
Brake Fan System
32-48-01A 32-48-02
32-48-03A
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
BRK FAN pb-sw HOT light
32-48-02A 32-48-03
C
BRK FAN pb-sw ON light
Note: Brake Fan operation may be checked through the brake fan ECAM MEMO.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.32.55 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-51
Steering
32-51-01
Nose Wheel Steering Control System
32-51-01A
32-51-02 32-51-02A
A
1
1
C
2
0
Must be operative.
Rudder PEDALS DISC pb (O)
One or both may be inoperative (no disconnection is possible). OPERATING PROCEDURES The purpose of the procedure is to explain how to perform the flight control check with one or both PEDALS DISC pb failed in the released position. OPERATING PROCEDURES GENERAL INFORMATION -
When the disconnection is not possible on one side: The flight control check can be performed on the operative side.
-
When the disconnection is not possible on both sides: The flight control check must be performed while aircraft is stopped. Note: It is not necessary to set the A/SKID & N/W STRG sw to OFF.
A320/321 MEL/CDL
01.32.56 LANDING GEAR 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-51
Steering
32-51-03 32-51-03A
NWS Electrical Deactivation Box No towing mode when lever in the TOWING position
C
1
0
(O)
May be inoperative.
Note: The towing mode is not available when the lever is in the TOWING position.
OPERATING PROCEDURES
BEFORE CONVENTIONAL OR TOWLESS PUSHBACK A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . OFF AFTER PUSHBACK A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . . ON
32-51-03B
NWS electrical C deactivation box deactivated
1
0
(O)(M) May be inoperative provided that the NWS electrical deactivation box is deactivated.
(Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1.
ITEM
SYSTEM & SEQUENCE OF ITEMS
2.
01.32.57 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-51
Steering
32-51-03 32-51-03B
NWS Electrical Deactivation Box NWS electrical deactivation box deactivated (Cont’d)
OPERATING PROCEDURES
BEFORE CONVENTIONAL OR TOWLESS PUSHBACK A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . OFF As a result of the NWS electrical box deactivation, the parking brake light on that box will not be available. The parking brake setting must be verbally confirmed between the flight crew and the ground personnel before pushback.
AFTER PUSHBACK A/SKID & N/W STRG selector . . . . . . . . . . . . . . . . . . . . ON
MAINTENANCE PROCEDURE Refer to AMM 32-51-00-040-002
A320/321 MEL/CDL
01.32.58 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-51
Steering
32-51-04
PARKING BRAKE light on the NWS Electrical Deactivation Box
32-51-04A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES BEFORE PUSHBACK The parking brake setting must be verbally confirmed between the flight crew and the ground personnel.
32-61
Landing Gear Panel on the Center Instrument Panel
32-61-01
LDG GEAR Indicator Panel
32-61-01A 32-61-02
32-61-02A
C
1
0
C
1
0
May be inoperative.
DOWN Red Arrow light on the Landing Gear lever (M)
May be inoperative provided that the L/G GEAR NOT DOWN alert and the L/G GEAR NOT DOWNLOCKED alert are checked operative.
MAINTENANCE PROCEDURE Refer to AMM 32-61-00-040-001 *
*
*
A320/321 MEL/CDL
MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.32.59 LANDING GEAR
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
01.32.60 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
MEL
A320/321 MEL/CDL
MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
01.32.61 LANDING GEAR
A320/321 MEL/CDL
01.32.62 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
D
01.32.63 LANDING GEAR
A320/321 MEL/CDL
01.32.64 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
MEL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.33.01 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-01
Overhead Panels
33-01-01
ANN LT Overhead Panel
33-01-01-01
TEST Function of ANN LT sw
33-01-01-01A
C
1
0
May be inoperative.
C
1
0
Dim lighting may be inoperative provided that the bright lighting is operative.
C
1
0
Bright lighting may be inoperative for night operation.
C
1
0
33-01-01-02 DIM Function of ANN LT sw 33-01-01-02A 33-01-01-03 BRT Function of ANN LT sw 33-01-01-03A 33-01-02-01 EMER EXIT LT OFF light 33-01-02-01A
(M)
May be inoperative provided that the emergency lighting system is checked operative every day.
MAINTENANCE PROCEDURE Refer to AMM 33-51-00-040-002
A320/321 MEL/CDL
01.33.02 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-01
Overhead Panels
33-01-01
ANN LT Overhead Panel
33-01-02-02 AUTO Function of SEAT BELT SIGNS sw 33-01-02-02A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES DURING COCKPIT PREPARATION SEAT BELTS selector · · · · · · · · · · · · · · · · · · · · · · · ON AFTER TAKEOFF SEAT BELTS selector · · · · · · · · · · · · · · · · As required DURING APPROACH SEAT BELTS selector · · · · · · · · · · · · · · · · · · · · · · · ON
33-01-02-03 AUTO Function of NO SMOKING SIGNS sw 33-01-02-03A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check that the passenger address function is operative in the affected lavatory with the door closed.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.33.03 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-10
Cockpit General Illumination
33-10-01
Cockpit General Illumination (Center & Main Instrument Lighting, Console and Floor Lighting, Dome lights and Lighting Strips, Instrument and Panel Integral Lighting, Map Holder Lighting, Center Pedestal Lighting)
33-10-01A
C
13 10
May be inoperative provided that: 1) The lighting is sufficient for all instruments and controls, and 2) The RH dome light is operative, and 3) The left section of the center main panel flood light is operative. NOTE: RH dome light is considered operative with a minimum of three bulbs illuminated in each assembly. The bulbs can be checked by selecting the DOME toggle switch from DIM to BRT and ensure both functions operate.
33-20
Cabin General Illumination
33-20-01 33-20-01A
Cabin General Illumination C
6
3
The lighting must be sufficient for cabin attendants to perform their duties.
A320/321 MEL/CDL
01.33.04 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-20
Cabin General Illumination
33-20-02
33-20-02A
Cabin Signs (No Smoking/No Electronic Devices/Fasten Seat Belt/Return to Seat) Passenger seat C occupied
30
0
One or more may be inoperative and the affected passenger seat may be occupied provided that: 1) The passenger address system is operative, and can be heard throughout the cabin during the flight, and 2) The passenger address system is used to alert the passengers when return to seat is requested, seat belts should be fastened and smoking is prohibited.
33-20-02B
Passenger seat C not occupied
30
0
(M)(FD) One or more “No Smoking/Fasten Seat Belt” sign may be inoperative provided that: 1) No passenger seat is occupied from which a passenger cannot see a readily legible “No smoking/Fasten Seat Belt” sign, and 2) The affected inoperative.
seat
is
blocked
MAINTENANCE PROCEDURE Refer to AMM 33-20-00-040-001
and
placarded
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.33.05 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-20
Cabin General Illumination
33-20-03 33-20-03A
Lavatory Sign (Return to seat) C
3
0
(O)(FD) One or more may be inoperative and the affected lavatory may be used provided that: 1) The passenger address system is checked operative in the affected lavatory, and 2) The passenger address system is used to alert the occupant to return to his seat.
OPERATING PROCEDURES
DURING COCKPIT PREPARATION Check that the passenger address function is operative in the affected lavatory with the door closed.
A320/321 MEL/CDL
01.33.06 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-30
Cargo and Service Compartment Lighting
33-30-01
Cargo and Service Compartment Lighting System
33-30-01A 33-40
C
1
0
May be inoperative.
Exterior Lighting
33-40-01
Navigation light System 1
33-40-01A
Daylight operations
C
3
0
33-40-01B
Navigation light C system 2 operative
3
0
One or more may be inoperative provided that the Navigation light system 2 is operative.
C
3
0
One or more may be inoperative.
One may be inoperative provided that the nose, taxi and takeoff lights are operative.
33-40-02
One or more may be inoperative for daylight operations.
Navigation light System 2
33-40-02A 33-40-03
(FD)
Landing light
33-40-03A
Nose, taxi and takeoff lights operative
C
2
1
33-40-03B
Daylight operations
C
2
0
(FD)
One or both may be inoperative for daylight operations.
A320/321 MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.33.07 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-40
Exterior Lighting
33-40-04
33-40-04A
Landing light Extension/ Retraction System Inoperative in extended position
C
2
0
(O)(FD) One or both may be inoperative in the extended position.
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS The fuel consumption is increased by 1 % per landing light extended. 33-40-04B
Inoperative in retracted position
C
2
0
One or both may be inoperative in the retracted position provided that the associated light is considered inoperative. Refer to MEL Item 33-40-03 Landing light
33-40-05
Runway Turnoff lights
33-40-05A 33-40-06
33-40-07A
2
0
One or both may be inoperative.
C
2
1
One may be inoperative.
D
2
0
One or both may be inoperative.
Taxi and Takeoff light
33-40-06A 33-40-07
C
Logo lights
A320/321 MEL/CDL
01.33.08 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-40
Exterior Lighting
33-40-08 33-40-08A
Beacon light Daylight operations
C
2
0
(O)(FD) One or both may be inoperative for daylight operations. OPERATING PROCEDURES BEFORE ENGINE START -
33-40-08B
Strobe lights operative
C
2
0
(O)
If the bottom light is inoperative: If this light is used to alert the ground crew of the engine start, the captain must brief the ground mechanic regarding beacon light.
One or both may be inoperative provided that the Strobe lights are operative. OPERATING PROCEDURES Refer to MEL item 33-40-08A
33-40-09
Wing Scan lights
33-40-09A
Daylight operations
C
2
0
33-40-09B
Night operations
C
2
1
One may be inoperative for night operations.
C
3
0
One or more may be inoperative.
33-40-10 33-40-10A
(FD)
One or both may be inoperative for daylight operations.
Strobe light
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.33.09 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-51
Cabin Emergency Lighting
33-51-01
33-51-01B
33-51-01
33-51-01B
33-51-02
Exit Marking Sign (A320) A maximum of C three nonadjacent LEDs inoperative
33-51-03A
6
A maximum of three non-adjacent LEDs may be inoperative in one or more signs.
8
8
A maximum of three non-adjacent LEDs may be inoperative in one or more signs.
C
18 15
A maximum of three non-adjacent LEDs may be inoperative in one or more signs.
C
22 19
A maximum of three non-adjacent overhead emergency lights may be inoperative.
Exit Marking Sign (A321) A maximum of C three nonadjacent LEDs inoperative Exit Location Sign in the Main Aisle
33-51-02A 33-51-03
6
Overhead Emergency Lighting System in the Main Aisle
A320/321 MEL/CDL
01.33.10 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-51
Cabin Emergency Lighting
33-51-04
Overhead Emergency Lighting System in the Door Vicinity (A320)
33-51-04A
Refer to Item 52-10-01 Cabin Passenger Door, and Refer to Item 52-10-02 Overwing Emergency Exit
33-51-04
Overhead Emergency Lighting System in the Door Vicinity (A321)
33-51-04A 33-51-05
33-51-05A ( M : meters )
Refer to MEL Item 52-10-01 Cabin Passenger Door Floor Proximity Emergency Escape Path Marking System in the Main Aisle C
80 79 M M
Each of the photoluminescent strips of an aisle may be inoperative or missing up to a length of 0,25 meter (10 inches) provided the inoperative or missing parts are not directly opposite each other and are not closer than 2,0 meter (78.74 inches). No more than four such inoperative or missing parts are allowed provided: 1- All strips within 1 meter of an exit is operative, and 2- All strips marking right angle intersection including cross aisles and overwing exits are operative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.33.11 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-51
Cabin Emergency Lighting
33-51-07
Floor Proximity Emergency Escape Path Marking System Exit Marker
33-51-07A 33-51-08
Overwing Emergency light
33-51-08A
33-51
Refer to MEL Item 52-10-01 Cabin Passenger Door, and Refer to MEL Item 52-10-02 Overwing Emergency Exit
Daylight operations
C
4
0
(FD)
One or more may be inoperative for daylight operations.
C
4
0
One or more may be inoperative.
C
8
0
May be inoperative for daylight operations.
C
4
0
One or more may be inoperative.
Cabin Emergency Lighting
33-51-09
Overwing Exit Handle light
33-51-09A 33-51-10 33-51-10A
33-51-11 33-51-11A
Escape Slide Lighting Daylight operations
Lavatory Auxiliary light
*
*
*
A320/321 MEL/CDL
01.33.12 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.01 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-00
MAINTENANCE Messages on the STATUS SD page
34-00-01
ADR (1)(2)(3) MAINTENANCE Message
34-00-01A 34-00-02
C
3
-
ADR (1)(2)(3) MAINTENANCE message may be displayed on the STATUS SD page.
C
3
-
IR MAINTENANCE message may be displayed on the STATUS SD page.
C
3
0
One or more may be inoperative.
C
3
0
One or more may be inoperative.
C
3
0
One or more may be inoperative.
C
3
0
One or more may be inoperative.
IR MAINTENANCE Message
34-00-02A 34-01
Overhead Panels
34-01-01
ADIRS Overhead Panel
34-01-01-01
ADR pb-sw FAULT light
34-01-01-01A 34-01-01-02 ADR pb-sw OFF light 34-01-01-02A 34-01-01-03 IR pb-sw FAULT light 34-01-01-03A 34-01-01-04 IR pb-sw OFF light 34-01-01-04A
A320/321 MEL/CDL
01.34.02 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-01
Overhead Panels
34-01-01
ADIRS Overhead Panel
34-01-01-04 IR pb-sw OFF light 34-01-01-04A
C
3
0
One or more may be inoperative.
C
1
0
May be inoperative.
C
3
2
34-01-01-05 ON BAT light 34-01-01-05A 34-01-01-31 ADR pb-sw 34-01-01-31A
(O)
ADR 2 or ADR 3 pb-sw may be inoperative provided that: 1) The associated mode selector is operative, and 2) The two ADRs and the two IRs associated with the two operative ADRs pb-sw are operative. OPERATING PROCEDURES IN FLIGHT If needed, the associated ADR can be set to OFF through the associated mode selector. Note: -
If the ADR is set to OFF: The associated IR is also set to OFF. The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.03 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-01
Overhead Panels
34-01-01
ADIRS Overhead Panel
34-01-01-32 IR pb-sw 34-01-01-32A
C
3
2
(O)
IR 2 or IR 3 pb-sw may be inoperative provided that: 1) The associated mode selector is operative, and 2) The two ADRs and the two IRs associated with the two operative IRs pb-sw are operative. OPERATING PROCEDURES FLIGHT If needed, the associated IR can be set to OFF through the associated mode selector. Note: -
If the IR is set to OFF: The associated ADR is also set to OFF. The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
34-01-01-33 IR Mode selector 34-01-01-33A
C
3
2
One may be inoperative.
A320/321 MEL/CDL
01.34.04 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-01
Overhead Panels
34-01-02
GPWS Overhead Panel
34-01-02-01 GPWS SYS FAULT light 34-01-02-01A 34-05
C
1
0
May be inoperative provided GPWS is verified operative before each departure.
2
2
Both must be operative.
Indications on the Primary Flight Display (PFD)
34-05-01
Actual Airspeed Reference Line and Scale Indication on the PFD
34-05-01A 34-05-02
Mach Number Indication on the PFD
34-05-02A One indication inoperative
C
2
1
One may be inoperative.
34-05-02B Both indications inoperative - FCU operative
C
2
0
Both may be inoperative provided that the SPD/MACH selection window on the FCU is operative.
34-05-02C Both indications inoperative - FL limitation
C
2
0
34-05-02D Both indications inoperative - ISIS Mach Number Function operative
C
2
0
(FD)
Both may be inoperative provided that the flight altitude is limited to 25 000 ft. Both may be inoperative provided that the ISIS Mach Number indication is operative.
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-05
Indications on the Primary Flight Display (PFD)
34-05-03
VMO/MMO Characteristic Speed Indication on the PFD
34-05-03A 34-05-04
34-05-06A
Both must be operative.
2
2
Both must be operative.
2
2
Both must be inoperative.
2
0
One or both may be inoperative.
Baro Reference Indication on the PFD
34-05-05A 34-05-06
2
Altitude Indication on the PFD
34-05-04A 34-05-05
2
Vertical Speed in Inertial Mode Indication on the PFD C
01.34.05 NAVIGATION
A320/321 MEL/CDL
01.34.06 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-05
Indications on the Primary Flight Display (PFD)
34-05-07
Other Air Data Related Indications on the PFD
34-05-07A
C
2
0
(O)
One or more may be inoperative. OPERATING PROCEDURES GENERAL INFORMATION For F, S, Green Dot determination, refer to the QRH/FPESPD speeds. For VAPP determination, refer to QRH/FPE-IFL-VAPP determination. For VFE or VLE determination, refer to the corresponding placard in the cockpit.
34-05-08
Attitude Indication on the PFD
34-05-08A
C
2
1
(O)
One may be inoperative provided that the aircraft is operated in day VMC conditions. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I.
34-05-09 34-05-09A
Heading Indication on the PFD C
2
1
One may be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.07 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-06
Indications on the Navigation Display (ND)
34-06-01
Ground Speed Indication on the ND
34-06-01A 34-06-02
34-06-06A
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
2
1
One may be inoperative provided that the heading indications are operative on both PFDs.
C
2
0
One or both may be inoperative.
C
2
0
One or more may be inoperative.
Position (Aircraft Symbol) Indication on the ND
34-06-05A 34-06-06
One or both may be inoperative.
Heading Indication on the ND
34-06-04A 34-06-05
0
Wind Indication on the ND
34-06-03A 34-06-04
2
True Air Speed Indication on the ND
34-06-02A 34-06-03
C
Radio Navaids Indications on the ND
A320/321 MEL/CDL
01.34.08 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-06
Indications on the Navigation Display (ND)
34-06-07
Chrono Indication on the ND
34-06-07A
34-10
C
2
0
One or both may be inoperative.
1
1
Must be operative.
1
0
Air Data/Inertial Reference System (ADIRS)
34-10-01
ADR 1
34-10-01A 34-10-02 34-10-02B
ADR 2 C
(O)
May be inoperative provided that: 1) The IR 1, IR 3, ADR 1 and ADR 3 are operative, and 2) The takeoff is not performed in CONF 1+F. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION -
ADR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
-
AIR DATA SWITCHING selector · · · · · · · · · · · · · F/O 3
-
ADIRS/ADIRU/2/26VAC AND AOA (location 121VU N08 or N09) C/B · · · · · · · · · · · · · Pull (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
ITEM
SYSTEM & SEQUENCE OF ITEMS
2.
01.34.09 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-10
Air Data/Inertial Reference System (ADIRS)
34-10-02 34-10-02B
ADR 2 (Cont’d)
OPERATING PROCEDURES (Cont’d) AFTER ENGINE START -
Use the RCL pb-sw on the ECAM control panel, in order to recall the NAV ADR 2 FAULT alert.
-
On the EWD, check that the ADR 2...OFF procedure is not displayed.
FOR TAKEOFF Takeoff in CONF 1+F is not permitted. Note: When the ADR 2 pb-sw is set to OFF, and if the aircraft is in CONF 1+F, the SFCS n°2 Flap channel is unable to crosscheck the airspeed coming from the ADR 1 with the ADR 2 airspeed coming from the SFCS n°2 Slat channel. This may lead to an uncommanded flap retraction during the takeoff. As a consequence, takeoff in CONF 1+F is not permitted when the ADR 2 pb-sw is set to OFF.
A320/321 MEL/CDL
01.34.10 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-10
Air Data/Inertial Reference System (ADIRS)
34-10-03 34-10-03A
ADR 3 C
1
0
(O)
May be inoperative provided that the IR 1, IR 2, ADR 1 and ADR 2 are operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION -
ADR 3 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
-
ADIRS/ADIRU/3/26VAC AND AOA (location 121VU N07 or N08) C/B· · · · · · · · · · · · · · Pull
AFTER ENGINE START -
Use the RCL pb-sw on the ECAM control panel, in order to recall the NAV ADR 3 FAULT alert.
-
On the EWD, check that the ADR 3...OFF procedure is not displayed.
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.11 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-10
Air Data/Inertial Reference System (ADIRS)
34-10-04 34-10-04B
IR 1 GPS 1 operative
B
1
1
(O)(FD) The NAV mode may be inoperative provided that: 1) The IR 1 is operated in ATT mode, and 2) The IR 2 and IR 3 are operative, and 3) The GPS 1 is operative, and 4) The terrain function of the TAWS is considered inoperative. Refer to MEL Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS) OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION
34-10-04C
GPS 1 inoperative
B
1
1
-
ATT HDG SWITCHING selector · · · · · · · · · · · CAPT 3
-
IR 1 mode selector · · · · · · · · · · · · · · · · · · · · · · · · · ATT
-
The heading must be entered through the MCDU for the IR 1 and has to be frequently reset (Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN ATT MODE).
(O)(FD) The NAV mode may be inoperative provided that: 1) The IR 1 is operated in ATT mode, and 2) The IR 2 and IR 3 are operative, and 3) The Flight remains within radio navaids coverage, and 4) The terrain function of the TAWS ñ– is considered inoperative. Refer to MEL Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS) (Cont’d on next page)
A320/321 MEL/CDL
01.34.12 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-10
Air Data/Inertial Reference System (ADIRS)
34-10-04
IR 1
34-10-04C GPS 1 inoperative (Cont’d)
34-10-05
OPERATING PROCEDURES Refer to MEL item 34-10-04B Operating Procedures
IR 2
34-10-05B IR 2 totally inoperative
C
1
0
(O)
May be inoperative provided that: 1) The IR 2 pb-sw is set to OFF, and 2) The IR 1, the IR 3, the ADR 1 and the two ADRs are operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION
34-10-05C Only NAV mode of IR 2 inoperative
C
1
0
(O)
-
IR 2 pb-sw · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · · OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
-
ATT HDG SWITCHING selector · · · · · · · · · · · · · F/O 3
-
AIR DATA SWITCHING selector · · · · · · · · · · · · · F/O 3
The NAV mode may be inoperative provided that: 1) The IR 2 is operated in ATT mode, and 2) The IR 1 and the IR 3 are operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. (Cont’d on next page)
A320/321 MEL/CDL
01 MAY 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.13 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-10
Air Data/Inertial Reference System (ADIRS)
34-10-05 34-10-05C
34-10-07 34-10-07A
IR 2 Only NAV mode of IR 2 inoperative (Cont’d)
OPERATING PROCEDURES (Cont’d) DURING COCKPIT PREPARATION -
ATT HDG SWITCHING selector · · · · · · · · · · · · · F/O 3
-
IR 2 mode selector · · · · · · · · · · · · · · · · · · · · · · · · · ATT
-
The heading must be entered through the MCDU keyboard for the IR 2 and has to be frequently reset (Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN ATT MODE).
IR 3 IR 3 mode selector set to OFF
B
1
0
(O)
May be inoperative provided that: 1) The IR 3 pb-sw is set to OFF, and 2) The IR 1, the IR 2, the ADR 1, and the ADR 2 are operative. OPERATING PROCEDURES GENERAL INFORMATION For aircraft fitted with Honeywell 10 MCU ADIRU, disregard the characteristic speeds (Vls, F, S, Green Dot) displayed on the PFD. For characteristic speeds (Vls, F, S, Green Dot) determination, refer to the QRH. The “CHECK GW” (or “CHECK WEIGHT”) message may be displayed on the MCDU. FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION IR 3 pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF The F/CTL MAINTENANCE message is displayed on the STATUS SD page.
A320/321 MEL/CDL
01.34.14 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-10
Air Data/Inertial Reference System (ADIRS)
34-10-07
IR 3
34-10-07B IR 3 operated in ATT mode
C
1
0
(O)
The NAV mode may be inoperative provided that: 1) The IR 3 is operated in ATT mode, and 2) The IR 1 and the IR 2 are operative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Landing capability is CAT II. DURING COCKPIT PREPARATION
34-11
-
IR 3 mode selector · · · · · · · · · · · · · · · · · · · · · · · · · ATT
-
The heading must be entered through the MCDU for the IR 3 and has to be frequently reset. (Refer to FCOM/PRO-ABN-34: IR ALIGNMENT IN ATT MODE).
Sensors
34-11-01 34-11-01A
Angle of Attack (AOA) Sensor C
3
2
The F/O or the STBY Angle Of Attack sensor may be inoperative provided that the associated ADR is considered inoperative. Refer to MEL Item 34-10-02 ADR 2, or Refer to MEL Item 34-10-03 ADR 3
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.15 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-11
Sensors
34-11-02
34-11-02A
CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR1 C
1
0
(O)
May be inoperative provided that: 1) The CAPT sensor element connected to the ADR 3 is operative, and 2) The F/O sensor connected to the ADR 2 is operative, and 3) The ADR 2 and the ADR 3 are operative, and 4) The TAT indication on the SD is checked operative, and 5) The TAS indication on the ND 1 is considered inoperative. Refer to MEL Item 34-06-02 True Air Speed Indication on the ND OPERATING PROCEDURES Refer to Operating Procedures 31-07-02A Permanent Data Indications on the SD
A320/321 MEL/CDL
01.34.16 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-11
Sensors
34-11-03
CAPT Total Air Temperature (TAT) Sensor Element Connected to ADR3
34-11-03A
C
1
0
(O)
May be inoperative provided that: 1) The CAPT sensor element connected to the ADR 1 is operative, and 2) The F/O sensor connected to the ADR 2 is operative, and 3) The ADR 1 and the ADR 2 are operative, and 4) The TAT indication on the SD is checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check that the TAT is displayed on the SD permanent data.
34-11-04
34-11-04A
F/O Total Air Temperature (TAT) Sensor Element Connected to ADR2 C
1
0
(O)
May be inoperative provided that: 1) Both CAPT TAT sensor elements are operative, and 2) The ADR 1 and the ADR 3 are operative, and 3) The TAT indication on the SD is checked operative, and 4) The TAS indications on the ND 2 is considered inoperative. Refer to MEL Item 34-06-02 True Air Speed Indication on the ND (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.17 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-11
Sensors
34-11-04
F/O Total Air Temperature (TAT) Sensor Element Connected to ADR2
34-11-04A
(Cont’d)
OPERATING PROCEDURES Refer to Operating Procedures 31-07-02A Permanent Data Indications on the SD
34-21
Altitude and Airspeed Standby Data
34-21-05 34-21-05A
Standby ALT Metric Indicator C
1
0
May be inoperative.
A320/321 MEL/CDL
01.34.18 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-22
Attitude and Heading Standby Data
34-22-01
Standby Compass Indicator
34-22-01A Applicable to aircraft fitted with NORTHROP GRUMMAN (LITTON) ADIRU except P/N 4650200303-0316 or subsequent, having the shelf modified (MOD 30650/SB 25-1248, or MOD 30872)
1
1
34-22-01B Applicable to C aircraft fitted with NORTHROP GRUMMAN (LITTON) ADIRU P/N 465020-03030316 or subsequent, having the shelf modified (MOD 30650/SB 25-1248, or MOD 30872) or HONEYWELL ADIRU
1
0
Must be operative.
(O)
May be inoperative provided that: 1) The three IRs are operative, and 2) The ATT/HDG SWITCHING selector, the EIS DMC SWITCHING selector and the PFD/ND XFR pb are checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check of the ATT HDG, PFD/ND, and EIS DMC switching: -
ATT HDG SWITCHING selector . . . . . . . . CAPT 3
-
Check that the display is normal on the CAPT PFD, the CAPT ND, and the RMI VOR.
-
ATT HDG SWITCHING selector . . . . . . . . . . F/O 3
-
Check that the display is normal on the F/O PFD and the F/O ND.
-
ATT HDG SWITCHING selector . . . . . . . . . NORM
-
EIS DMC SWITCHING selector. . . . . . . . . CAPT 3
-
Check that the display is normal on the CAPT PFD and the CAPT ND. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.19 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-22
Attitude and Heading Standby Data
34-22-01
Standby Compass Indicator OPERATING PROCEDURES (Cont’d)
34-22-01B Applicable to aircraft fitted with NORTHROP GRUMMAN (LITTON) ADIRU P/N 465020-03030316 or subsequent, having the shelf modified (MOD 30650/SB 25-1248, or MOD 30872) or HONEYWELL ADIRU
34-22-02
34-22-02A
-
EIS DMC SWITCHING selector . . . . . . . . . . F/O 3
-
Check that the display is normal on the F/O PFD and the F/O ND.
-
EIS DMC SWITCHING selector . . . . . . . . . NORM
-
CAPT PFD/ND XFR pb . . . . . . . . . . . . . . . . . Press
-
Check that the CAPT PFD and the CAPT ND images are exchanged.
-
CAPT PFD/ND XFR pb . . . . . . . . . . . . . . . . . Press
-
F/O PFD/ND XFR pb. . . . . . . . . . . . . . . . . . . Press
-
Check that the F/O PFD and the F/O ND images are exchanged.
-
F/O PFD/ND XFR pb. . . . . . . . . . . . . . . . . . . Press
Standby Compass Lighting C
1
0
May be inoperative.
A320/321 MEL/CDL
01.34.20 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-23
Integrated Standby Instrument System (ISIS)
34-23-01
ISIS Baro-Altitude Indication
34-23-01A 34-23-02
B
1
0
May be inoperative provided that the aircraft is operated in day VMC conditions.
C
1
0
May be inoperative provided that:
ISIS Airspeed Indication
34-23-02A
1) The ISIS attitude indication is operative, and 2) The ADRs, DMCs and probe heat computers are operative, and 3) The AIR DATA SWITCHING selector, the EIS DMC SWITCHING selector and the PFD/ND XFR pb are operative. 34-23-03 34-23-03A
ISIS Bugs Indication C
1
0
May be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.21 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-23
Integrated Standby Instrument System (ISIS)
34-23-04 34-23-04B
ISIS Attitude Indication B
1
0
(O)(FD) May be inoperative provided that the aircraft is operated in day VMC conditions.
OPERATING PROCEDURES
FLIGHT PREPARATION/LIMITATIONS Maximum landing capability is CAT I.
A320/321 MEL/CDL
01.34.22 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-23
Integrated Standby Instrument System (ISIS)
34-23-05
ISIS ILS Indication
34-23-05A 34-23-06
1
0
May be inoperative.
C
1
0
May be inoperative.
C
2
1
ISIS Mach Number Indication
34-23-06A 34-30
C
Landing and Taxiing Aid
34-30-04
34-30-04A
Instrument Landing System (ILS) (O)(FD) One ILS may be inoperative for VMC operations or for IMC operations provided approach minimums do not require use. Note: When the ILS 1 is inoperative, the reactive modes of TAWS are inoperative. Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS) (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.23 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-30
Landing and Taxiing Aid
34-30-04
Instrument Landing System (ILS)
34-30-04A
(cont’d)
OPERATING PROCEDURES Note: -
When one ILS is inoperative: Maximum landing capability is ILS CAT I.
-
When both ILS are inoperative: CAT I ILS approaches are not permitted.
34-40
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
34-40-01
34-40-01A
Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS) A
1
0
(O)
May be inoperative provided: a) For the intent of returning International Flights to either JED, RUH or DMM, the aircraft may continue the flight sector(s) scheduled before the failure, b) Flight is conducted under Day VMC conditions,and c) Repairs are made within one flight day. (Cont’d on next page)
A320/321 MEL/CDL
01.34.24 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-40
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
34-40-01
Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)
34-40-01A (Cont’d)
OPERATING PROCEDURES Flight crew should increase their awareness of airplane configuration, altitude and flight path at all times and review and comply with Minimum Enroute Altitudes (MEA) and altitude callouts.
34-40-01B Modes 1- 4
A
4
0
(O)
May be inoperative provided: 1) For the intent of returning International Flights to either JED, RUH or DMM, the aircraft may continue the flight sector(s) scheduled before the failure, 2) Flight is conducted under Day VMC conditions,and 3) Repairs are made within one flight day. OPERATING PROCEDURES Flight crew should increase their awareness of airplane configuration, altitude and flight path at all times and review and comply with Minimum Enroute Altitudes (MEA) and altitude callouts.
34-40-01C Test Mode
A
1
0
(O)
May be inoperative provided: 1) For the intent of returning International Flights to either JED, RUH or DMM, the aircraft may continue the flight sector(s) scheduled before the failure, 2) Flight is conducted under Day VMC conditions,and 3) Repairs are made within one flight day. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.25 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-40
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
34-40-01
34-40-01C
Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS) Test Mode (Cont’d)
OPERATING PROCEDURES Flight crew should increase their awareness of airplane configuration, altitude and flight path at all times and review and comply with Minimum Enroute Altitudes (MEA) and altitude callouts.
34-40-01D
Glideslope B Deviation Mode 5
1
0
34-40-01E
Advisory CallOuts
7
0
C
May be inoperative.
(O)
May be inoperative provided alternate procedures are established and used. OPERATING PROCEDURES The PM must be briefed to handle all the advisory calls per FCOM instructions.
34-40-01F
TAWS
C
1
0
(O)
May be inoperative provided alternate procedures are established and used. OPERATING PROCEDURES Flight crew should increase their awareness of airplane configuration, altitude and flight path at all times and comply with Minimum Enroute Altitude (MEA).
A320/321 MEL/CDL
01.34.26 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-40
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
34-40-02
Radio Altimeter Automatic Callout
34-40-02A
C
1
0
(O)
May be inoperative. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Maximum Landing capability is CAT I.
30-40-03 30-40-03A
Radio Altimeter System C
2
1
(O)
One may be inoperative provided that both FCU channels, all ELACs, SECs, ADIRUs, SFCCs, LGCIUs and FACs are operative. Note: When the radio altimeter 1 inoperative, the reactive modes TAWS are inoperative.
is of
Refer to MEL 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System. OPERATING PROCEDURES FLIGHT PREPERATION LIMITATION Maximum landing Capability is CAT I. The F/CTL MAINTENACE Message is displayed on the STATUS SD page. (Cont’d on next page)
A320/321 MEL/CDL
30 JUN 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.27 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-40
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
30-40-03 30-40-03A
Radio Altimeter System (Cont’d)
OPERATING PROCEDURES (Cont’d) DURING COCKPIT PREPERATION < If RA 1 is inoperative: COM NAV/RAD ALTM/1 (121VU K11) C/B. . . . . . . . . . Pull < If RA 2 is inoperative: COM NAV/RAD ALTM/2 (121VU K12) C/B. . . . . . . . . . Pull
34-40-04
Traffic Collision Avoidance System (TCAS)
34-40-04A
1
1
Must be operative. Note: When the TCAS is deactivated, the TAWS is also inoperative. Refer to Item 34-40-01 Ground Proximity Warning System (GPWS)/Terrain Awareness and Warning System (TAWS)
34-40-05 34-40-05A
Weather Radar System C
2
1
One may be inoperative.
A320/321 MEL/CDL
01.34.28 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-40
GPWS/TAWS, Radio Altimeter, TCAS, Weather Radar
34-40-05 34-40-05B
Weather Radar System B
2
0
(FD)
Both may be inoperative provided: 1) Flight is conducted in Day VMC, and 2) For IMC or Night VMC flights, provided current weather reports do not indicate any thunderstorms or other potentially hazardous weather conditions which can be detected by weather radar.
Note: When the captain and flight dispatcher have determined that weather radar inoperative requirements are met, the associated Dispatch Release must include the following statement: “Airborne weather radar is inoperative and not required.”
Note: When the weather radar system is inoperative, the predictive Windshear Detection System is inoperative . Refer to Item 34-40-06 Weather Radar/Predictive Windshear Detection Function .
A320/321 MEL/CDL
30 JUN 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.29 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-40-06
Predictive Windshear Detection Function
34-40-06A 34-40-07
Refer to MEL item 22-60-03A PULL UP-GPWS pb-sw
34-40-07A
One inoperative
C
2
1
(O)
One may be inoperative provided that the GPWS or the TAWS aural and visual warnings are checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check of the GPWS (or TAWS) aural and visual warnings:
34-50
-
PULL UP . GPWS pb-sw (operative · · · · · · · · · · Press
-
Check that the GPWS (or the TAWS) aural and visual warnings are operative. Refer to FCOM/DSC-34-70 GPWS.
ATC and Radio / GPS Navigation Systems
34-50-01 34-50-01A
ATC B
2
1
(O)(FD) One may be inoperative OPERATING PROCEDURES -
An altitude encoder must be operative for the operative transponder,
-
In the event both ATC transponders become inoperative enroute, the flight may continue to the next point of intended landing where repairs or replacement facilities are available. Appropriate authorization from ATC centers concerned is necessary.
-
An ATC transponder must be operative to enter RVSM airspace (Cont’d on next page)
A320/321 MEL/CDL
01.34.30 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-50
ATC and Radio / GPS Navigation Systems
34-50-01
ATC
34-50-01A (Cont’d)
OPERATING PROCEDURES (Cont’d) FLIGHT PREPARATION/LIMITATIONS When both ATCs are inoperative, RVSM operations are not permitted.
34-50-03
ADF
34-05-03A
34-50-04
C
34-50-06A
May be inoperative unless its use is required.
2
1
One may be inoperative provided both GPS is operative.
2
2
Both must be operative.
1
0
VOR
34-50-05A
34-50-06
0
DME
34-50-04A
34-50-05
1
MARKER C
(FD)
May be inoperative provided approach minimums do not required its use.
A320/321 MEL/CDL
30 JUN 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.34.31 NAVIGATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
34 NAVIGATION 34-50
ATC and Radio / GPS Navigation Systems
34-50-09
Global Positioning System (GPS)
34-50-09A
34-50-09B
B
2
2
(FD)
Both are required to be operative for flights departing the kingdom envolving RNAV routes, and/or RNAV/GPS approaches.
2
1
(O)(FD) One may be inoperative on RNAV routes, and/or RNAV/GPS approaches returning to the kingdom provided both DME systems are operative OPERATING PROCEDURES: Dispatch must confirm whether the route or part of the route is RNAV airspace and destination airport does not have published GPS approaches only.
34-50-09C
B
2
0
(O)(FD) May be inoperative provided the flight is not dispatched through RNAV airspace. OPERATING PROCEDURES: Dispatch must confirm whether the route or part of the route is not RNAV airspace and destination, alternate airport does not have published GPS approaches only.
*
*
*
A320/321 MEL/CDL
01.34.32 NAVIGATION 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.35.01 OXYGEN
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-01 35-01-01
Overhead Panels OXYGEN Overhead Panel
35-01-01-01 CREW SUPPLY pb-sw OFF light 35-01-01-01A
C
1
0
May be inoperative.
C
1
0
May be inoperative.
C
1
0
35-01-01-02 PASSENGER SYS ON light 35-01-01-02A 35-01-01-31 MANUAL Control of the MASK MAN ON pb 35-01-01-31A
AUTO control function checked operative
(M)
May be inoperative provided that the AUTO control function is checked operative. MAINTENANCE PROCEDURE Refer to AMM 35-23-00-040-008
A320/321 MEL/CDL
01.35.02 OXYGEN 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-01
Overhead Panels
35-01-01
OXYGEN Overhead Panel
35-01-01-32 AUTO Control of the MASK MAN ON pb 35-01-01-32A 35-07
C
1
0
(FD)
May be inoperative provided that the operating altitude is limited to FL 300.
C
1
0
(O)(M) May be inoperative provided that the oxygen pressure is checked by direct reading before each flight.
Indications on the DOOR/OXY SD page
35-07-01
35-07-01A
Crew OXY High Pressure Indication on the DOOR/OXY SD page
OPERATING PROCEDURES DURING COCKPIT PREPARATION · After application of the maintenance procedure: Check that the oxygen pressure is sufficient for the intended flight. Refer to FCOM/LIM-35 Cockpit Fixed Oxygen System
MAINTENANCE PROCEDURE Refer to AMM 35-10-00-040-001
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.35.03 OXYGEN
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-07
Indications on the DOOR/OXY SD page
35-07-02
Crew Oxygen REGUL LO PR Indication on the DOOR/OXY SD page
35-07-02A
C
1
0
(O)(M) May be inoperative provided that the oxygen pressure is checked before the first flight of each day. OPERATING PROCEDURES GENERAL INFORMATION On the DOOR/OXY SD page, disregard the REGUL LO PR indication and the associated OXY indication. MAINTENANCE PROCEDURE Refer to AMM 35-10-00-040-002
35-10
Crew Oxygen
35-10-01
Crew Oxygen Mask
35-10-01A 35-10-02
35-10-03A
4
2
(FD)
Each occupant of the cockpit must have his assigned mask operative.
C
4
2
(FD)
One must be operative for each pilot.
C
1
0
(O)
May be missing or damaged.
Crew Oxygen Mask Microphone
35-10-02A 35-10-03
C
Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc)
(Cont’d on next page)
A320/321 MEL/CDL
01.35.04 OXYGEN 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-10
Crew Oxygen
35-10-03
Exterior Crew Oxygen Overpressure Indicator Disc (Green Disc)
35-10-03A (cont’d)
OPERATING PROCEDURES DURING COCKPIT PREPARATION Before the first flight of each day, check that the oxygen pressure does not decrease: On the DOOR/OXY SD page, check the OXY pressure indication twice. A 15 min interval must be applied between both checks.
35-20
Passenger Oxygen
35-20-01 35-20-01A
Passenger Oxygen Unit Associated seats considered inoperative (A320)
C
46
0
(A321)
C
60
0
(FD)
One or more may be inoperative provided that the associated seats are considered inoperative. Refer to Item 25-20-01 Passenger Seat
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.35.05 OXYGEN
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-20
Passenger Oxygen
35-20-02 35-20-02A
35-20-04
35-20-04A
Cabin Attendant Oxygen Unit (A320)
C
5
4
(A321)
C
7
5
(FD)
Galley Oxygen Unit
Adjacent cabin B attendant oxygen unit available
May be inoperative provided that the associated seats are considered inoperative. Refer to Item 25-20-03 Cabin Attendant Seat
Note: For an inoperative cabin attendant oxygen unit located within the galley area: Refer to Item 35-20-02 Cabin Attendant Oxygen Unit 2
0
(O)
One or more may be inoperative and the associated galley area may be occupied provided that an adjacent cabin attendant individual oxygen unit is available for each occupants of the associated galley area. OPERATING PROCEDURES IN FLIGHT The number of galley area occupants must be in accordance with the available adjacent cabin attendant oxygen units.
35-20-04B
Portable B oxygen available in the associated galley area
2
0
(O)
One or more may be inoperative and the associated galley area may be occupied provided that a cabin attendant portable oxygen device is available for each occupants of the associated galley area.
(Cont’d on next page)
A320/321 MEL/CDL
01.35.06 OXYGEN 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-20
Passenger Oxygen
35-20-04
Galley Oxygen Unit
35-20-04B (cont’d)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Before the flight, the flight crew shall brief the cabin crew that the galley oxygen unit is inoperative and that the cabin attendant portable oxygen device should be used instead.
35-20-04C
35-20-05
Associated B galley area not occupied
0
(FD)
One or more may be inoperative provided that the associated galley area is not occupied.
6
1
One must be available.
2
2
Both must be available.
Manual Release Tool
35-20-05A
35-30
2
C
Portable Oxygen
35-30-01 35-30-01A
Flight Crew Portable Device
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.35.07 OXYGEN
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
35 OXYGEN 35-30
Portable Oxygen
35-30-02 35-30-02A
Cabin Attendant Portable Device PBE or Smoke C Hood
3
2
One required in the cockpit, and One required in the cabin. NOTE: Any in excess of that required may be inoperative or missing provided the inoperative PBE is placarded inoperative, removed from the installed location and placed out of sight so it can not be mistaken for a functional unit.
35-30-02B
Portable Oxygen Cylinder
May be inoperative or missing provided the inoperative Portable Oxygen Cylinderis placarded inoperative, removed from the installed location and placed out of sight so it can not be mistaken for a functional unit.
(A320)
C
7
4
(A321)
C
8
5
*
*
*
A320/321 MEL/CDL
01.35.08 OXYGEN 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.36.01 PNEUMATIC
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-00
MAINTENANCE Message on the STATUS SD Page
36-00-01
AIR BLEED MAINTENANCE Message
36-00-01F 36-01
C
1
-
AIR BLEED MAINTENANCE message may be displayed on the STATUS SD page.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
1
0
May be inoperative.
C
1
0
May be inoperative.
AIR COND Overhead Panel
36-01-01
ENG BLEED pbsw FAULT light
36-01-01A
36-01-02
ENG BLEED pbsw OFF light
36-01-02A
36-01-03
APU BLEED pb-sw FAULT light
36-01-03A
36-01-04 36-01-04A
APU BLEED pb-sw ON light
A320/321 MEL/CDL
01.36.02 PNEUMATIC 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-07
Indications on the BLEED SD page
36-07-01
APU Bleed Valve Indication on the BLEED SD page
36-07-01A 36-07-02
36-07-05A
May be inoperative.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
C
2
0
One or both may be inoperative.
Engine Bleed Precooler Inlet Pressure Indication on the BLEED SD page
36-07-04A 36-07-05
0
Engine Bleed HP Valve Indication on the BLEED SD page
36-07-03A 36-07-04
1
Engine Bleed Valve Indication on the BLEED SD page
36-07-02A 36-07-03
C
Engine Bleed Precooler Outlet Temperature Indication on the BLEED SD page
12 FEB 12 MEL
A320/321 MEL/CDL
01 MAY 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.36.03 PNEUMATIC
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-07
Indications on the BLEED SD page
36-07-06
X Bleed Valve Indication on the BLEED SD page
36-07-06A 36-11
C
1
0
May be inoperative.
Engine Bleed Air Supply System
36-11-01
36-11-01A
Engine Bleed Air Supply System
no FL limitation C
Note: The HP ground connection is near the engine 1 hazardous area. If the bleed air supply system 2 is inoperative, it is better to use the APU bleed for engine start. If the APU bleed is not available, a ground cart can be used as long as the pneumatic pipe is kept out of the hazardous area. 2
1
(O)(FD) One may be inoperative provided that: 1) The associated ENG BLEED pb-sw is set to OFF, 2) The X-BLEED selector is set to OPEN, 3) The speedbrakes are operative, and 4) The aircraft is not operated in known or forecast icing condations. OPERATING PROCEDURES AFTER ENGINE START - Refer to FCOM/PRO-ABN-36-C. AIR ENG 1(2) BLEED FAULT and Refer to FCOM/PRO-ABN-36-B. AIR ENG 1(2) BLEED ABNORM PR.
(Cont’d on next page)
A320/321 MEL/CDL
01.36.04 PNEUMATIC 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01 MAY 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-11
Engine Bleed Air Supply System
36-11-01
Engine Bleed Air Supply System
36-11-01A (cont’d)
OPERATING PROCEDURES (Cont’d) FOR TAKEOFF Consider selecting the air conditioning packs OFF or the APU bleed air supply system ON. AFTER TAKEOFF If the APU has been used to supply the air conditioning during the takeoff, set the APU BLEED pb-sw to OFF. IN FLIGHT · If Wing Anti-Ice is required: PACK (affected side) pb-sw . . . . . . . . . . . . . . . . . OFF · In the case of failure of the remaining engine bleed air supply system, or in the case of failure of the associated engine: - Apply the associated ECAM procedure, then - Refer to QRH/ABN-36 AIR DUAL BLEED FAULT
A320/321 MEL/CDL
01 MAY 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.36.05 PNEUMATIC
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC
36-11-02
Engine Bleed Valve (PRV)
36-11-02A
C
2
1
(M)
One may be inoperative provided that: 1) The affected engine bleed valve is secured in the closed position, and 2) The associated bleed air supply system is considered inoperative. Refer to Item 36-11-01 Engine Bleed Air Supply System MAINTENANCE PROCEDURE Refer to AMM 36-11-00-040-001
36-11-03
36-11-03A
Engine Bleed Overpressure Valve Associated bleed considered inoperative
C
2
1
One may be inoperative provided that the associated bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
A320/321 MEL/CDL
01.36.06 PNEUMATIC 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-11
Engine Bleed Air Supply System
36-11-04
Engine Bleed Fan Air Valve
36-11-04A
C
2
1
(FD)
One may be inoperative provided that the associated engine bleed air supply system is considered inoperative. Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-05
Engine Bleed Air Precooler
36-11-05A
C
2
1
One may be inoperative provided that the associated engine bleed air supply system is considered inoperative. Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-06 36-11-06A
Engine Bleed IP Check Valve Associated bleed considered inoperative
C
2
1
(FD)
One may be inoperative provided that the associated engine bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-06B
Associated HP C valve secured in the closed position
2
1
(O)(M) One may be inoperative in the open position provided that the associated HP valve is secured in the closed position.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.36.07 PNEUMATIC
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-11 36-11-06
Engine Bleed Air Supply System Engine Bleed IP Check Valve
36-11-06B (cont’d)
OPERATING PROCEDURES DURING TAXI When the engines operate in idle thrust: - ENG (affected side) BLEED pb-sw . . . . . . . . . . . OFF - X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN · If wing anti-ice is required: One PACK pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF DURING TAKEOFF, CLIMB, AND CRUISE - ENG (affected side) BLEED pb-sw . . . . . . . . . . . On - X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . AUTO DURING DESCENT When the engines operate in idle thrust: - ENG (affected side) BLEED pb-sw . . . . . . . . . . . OFF - X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN · If wing anti-ice is required: One PACK pb-sw . . . . . . . . . . . . . . . . . . . . . . . . . OFF
MAINTENANCE PROCEDURE Refer to AMM 36-11-00-040-002
A320/321 MEL/CDL
01.36.08 PNEUMATIC 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-11
Engine Bleed Air Supply System
36-11-07 36-11-07A
Engine Bleed HP Valve Associated bleed considered inoperative
C
2
1
(FD)
One may be inoperative in the closed position provided that the associated engine bleed air supply system is considered inoperative. Refer to Item 36-11-01 Engine Bleed Air Supply System
36-11-07B
HP valve C secured in the closed position
2
1
(O)(M) One may be inoperative provided that the affected engine bleed HP valve is secured in the closed position. OPERATING PROCEDURES Refer to MEL item 36-11-06B MAINTENANCE PROCEDURE Refer to AMM 36-11-00-040-003
36-11-08 36-11-08A
Bleed Monitoring Computer (BMC) C
2
1
(FD)
One may be inoperative provided that the associated engine bleed air supply system is considered inoperative. Refer to Item 36-11-01 Engine Bleed Air Supply System
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.36.09 PNEUMATIC
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-12
APU Bleed Air Supply and Crossbleed Systems
36-12-01
APU Bleed Air Supply System
36-12-01A 36-12-02 36-12-02A
C
1
0
C
1
0
May be inoperative provided that the APU BLEED pb-sw is set to OFF.
APU Bleed Valve APU bleed considered inoperative
(M)
May be inoperative provided that: 1) The APU bleed valve is secured in the closed position, and 2) The APU bleed air supply system is considered inoperative. Refer to Item 36-12-01 APU Bleed Air Supply System MAINTENANCE PROCEDURE Refer to AMM 36-12-00-710-001
36-12-02B
APU not used
C
1
0
(O)
May be inoperative in the open position provided that the APU is not used in flight. Refer to Item 49-10-01 Power Plant (APU) OPERATING PROCEDURES ON GROUND OR IN FLIGHT · When the APU runs: APU BLEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . ON · After APU shutdown: APU BLEED pb-sw . . . . . . . . . . . . . . . . . . . . . . . . Off
A320/321 MEL/CDL
01.36.10 PNEUMATIC 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-12
APU Bleed Air Supply and Crossbleed Systems
36-12-03
APU Bleed Check Valve
36-12-03A
C
1
0
May be inoperative provided that the APU bleed air supply system is considered inoperative. Refer to Item 36-12-01 APU Bleed Air Supply System
36-12-04
36-12-04A
Automatic Control of the X Bleed Valve C
1
0
(O)
May be inoperative provided that the manual control is checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION Check of the manual control of the X BLEED valve: - X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . OPEN - On the BLEED, check that the cross bleed valve is indicated open. - X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . SHUT - On the BLEED, check that the cross bleed valve is indicated closed. - X BLEED selector . . . . . . . . . . . . . . . . . . . . . . . . AUTO
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.36.11 PNEUMATIC
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
36 PNEUMATIC 36-22
Leak Detection Loop
36-22-01
Pylon Leak Detection System
36-22-01A
C
2
1
(M)
One may be inoperative provided that: 1) The associated deactivated, and
pylon
leak
detection
loop
is
2) The AIR ENG 1(2) BLEED LEAK alert is confirmed to be false by troubleshooting, and 3) The associated bleed air supply system is considered inoperative. Refer to Item 36-11-01 Engine Bleed Air Supply System MAINTENANCE PROCEDURE Refer to AMM 36-22-00-040-001 36-22-02
Wing Leak Detection System
36-22-02A
2
2
Must be operative. Note: Failure of one loop in one or both wing leading edges is indicated by a MAINTENANCE message displayed on the STATUS SD page. Refer to Item 36-00-01 AIR BLEED MAINTENANCE Message
36-22-03 36-22-03A
APU Leak Detection Loop C
1
0
May be inoperative.
*
*
*
A320/321 MEL/CDL
01.36.12 PNEUMATIC 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
NUMBER INSTALLED 3.
ITEM
01.38.01 WATER/WASTE
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
38 WATER/WASTE -10-01 Potable Water Systems C 1
0
(M)
Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks. NOTE: Any portion of system which is operative may be used. MAINTENANCE PROCEDURE Refer to AMM 38-10-00
C 1
0
(M)
May be inoperative provided: a) System is drained, and b) Procedures are established to ensure that system is not serviced. MAINTENANCE PROCEDURE Refer to AMM 38-10-00
-30-01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories)
C 1
0
(M)
Individual components may be inoperative provided: a) Associated components are deactivated or isolated,and b) Associated system components are verified not to have leaks. NOTE: Any portion of system which is operative may be used. MAINTENANCE PROCEDURE Refer to AMM 38-30-00
(Cont’d on next page)
A320/321 MEL/CDL
01.38.02 WATER/WASTE 1. SYSTEM & SEQUENCE OF ITEMS
2.
NUMBER INSTALLED 3.
ITEM
04 APR 12 MEL
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
38 WATER/WASTE -30-01 Lavatory Waste Systems (Including Wheelchair Accessible Lavatories) (Cont’d)
C 1
0
(M)(FD) Associated Lavatory system(s) may be inoperative provided: a) Associated components are deactivated or isolated to pervent leaks, b) Extra safety pilot should be assigned to operate the flight in case the forward lavatory placarded, c) Associated Lavatory door (s) is secured closed and placarded, “INOPERATIVE - DO NOT ENTER”, and d) Two lavatories must be operative. NOTE: These provisions are not intended to prohibit inspections by crew members. MAINTENANCE PROCEDURE Refer to AMM 38-30-00
1) Vacuum Generator Systems (Toilet)
C 2
0
(M)(FD) May be inoperative provided: a) Vacuum generator is deactivated, and b) Procedures are established and used to only allow use of the associated lavatory at or above 16000 FT MSL. MAINTENANCE PROCEDURE Refer to AMM 38-30-00
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.46.01 INFORMATION SYSTEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
46 INFORMATION SYSTEM 46-11
Aircraft Information Network Systems
46-11-01
Electronic Flight Bag (EFB)
46-11-01A
B
2
0
(FD)
One or both may be inoperative provided that the following documents must be provided to the FDC by dispatch: 1. Flight Dispatch Release and attachments.(including ATS FP) 2. Computer Flight Plan or manual flight log. 3. NOTAMS. 4. Latest current available TAFs/ METARs. 5. Temporary/ MTTL takeoff and landing preformance charts (when applicable) and takeoff data cards. 6. NOTOC (if applicable). 7. ASR/ Flight Crew Report forms. 8. Manual Loadsheet Calculation Form.
46-21
Air Traffic and Information Management System
46-21-01 46-21-01A
Air Traffic Service Unit (ATSU) B
1
0
(O)(FD) May be inoperative provided altenate procedures are used.
(Cont’d on next page)
A320/321 MEL/CDL
01.46.02 INFORMATION SYSTEM 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
46 INFORMATION SYSTEM 46-21
Air Traffic and Information Management System
46-21-01
Air Traffic Service Unit (ATSU)
46-21-01A (cont’d)
OPERATING PROCEDURES 1) Flight crew must transmit depature, enroute, and the arrival reports in accordance with the route manual communication requirement. 2) Flight crew must complete the in-flight cruise performance data records if required. Note: Any portion of the system that is operative may be used
46-21-02
Datalink Control and Display Unit (DCDU)
46-21-02A
46-21-03 46-21-03A
B
2
0
(FD)
One or both may be inoperative provided two way communications established with ATC and inroute not require its use.
B
2
0
(FD)
Refer to MEL 46-21-02A
ATC MSG pb
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
47
2.
ITEM
01.47.01 INERT GAS SYSTEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
INERT GAS SYSTEM
47-00
MAINTENANCE Message on the STATUS SD Page
47-00-01
47-00-01A
FUEL INERT MAINTENANCE Message C
1
-
FUEL INERT MAINTENANCE Message may be displayed on the STATUS SD page.
*
*
*
A320/321 MEL/CDL
01.47.02 INERT GAS SYSTEM 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.49.01 AIRBORNE AUXILIARY POWER
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY POWER 49-00
MAINTENANCE Message on the STATUS SD page
49-00-01
APU MAINTENANCE Message
49-00-01A 49-01
C
1
-
APU MAINTENANCE message may be displayed on the STATUS SD page.
C
1
0
May be inoperative provided that the N and the EGT indications are operative on the APU SD page.
C
1
0
May be inoperative.
C
1
0
May be inoperative provided that the N indication is operative on the APU SD page.
C
1
0
May be inoperative.
APU Overhead Panel
49-01-01
APU MASTER SW pb-sw FAULT light
49-01-01A 49-01-02
APU MASTER SW pb-sw ON light
49-01-02 49-01-03
APU START pb-sw AVAIL light
49-01-03A 49-01-04 49-01-04A
APU START pb-sw ON light
A320/321
01.49.02 AIRBORNE AUXILIARY POWER
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
49 AIRBORNE AUXILIARY POWER 49-07
Indications on the APU SD page
49-07-01
Indications on the APU SD page
49-07-01A 49-10
C
9
0
C
1
0
One or more may be inoperative.
Power Plant
49-10-01
Power Plant (APU)
49-10-01A
(O)
May be inoperative. OPERATING PROCEDURES GENERAL INFORMATION No APU bleed air will be available for Main Engine Start (MES) or air conditioning. No electrical power will be available from the APU generator. DURING COCKPIT PREPARATION APU MASTER SW pb-sw . . . . . . . . . . . . . . . . . . . Off
49-10-02
APU Air Intake Flap
49-10-02A
APU not used
C
1
0
49-10-02B
APU used
A
1
0
May be inoperative in the closed position provided that the APU is not used. (M)
May be inoperative in the open position for 10 days. MAINTENANCE PROCEDURE Refer to AMM 49-16-00-040-002 *
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.01 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01 52-01-01
Overhead Panels CKPT DOOR CONT Normal Overhead Panel
52-01-01-01 CHAN (1, 2) LEDs on the CKPT DOOR CONT Overhead Panel 52-01-01-01A
C
2
1
One may be inoperative.
C
3
2
One may be inoperative.
One inoperative A
2
1
52-01-01-02 STRIKE (TOP, MID, BOT) LEDs on the CKPT DOOR CONT Overhead Panel 52-01-01-02A 52-01-01-03 Pressure Rate Sensor on the CKPT DOOR CONT Overhead Panel 52-01-01-03A
(M)
One may be inoperative for 60 consecutive calendar days provided that the remaining pressure rate sensor is checked operative. MAINTENANCE PROCEDURE Refer to AMM 52-51-00-040-011
52-01-01-03B
Both inoperative
C
2
0
Both may be inoperative provided that the CDLS normal system is considered inoperative. Refer to Item 52-51-01 CDLS Normal System (Normal Control Unit, Switch and Lights on the CKPT DOOR Panel, Buzzer, Keypad).
A320/321 MEL/CDL
01.52.02 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01
Overhead Panels
52-01-02
CKPT DOOR CONT BK UP Overhead Panel
52-01-02-01 CHAN (1, 2) LEDs on the CKPT DOOR CONT BK UP Overhead Panel
52-01-02-01A
CTL pb FAULT C light checked operative
2
0
(O)
One or more may be inoperative provided that the CTL pb FAULT light is checked operative.
OPERATING PROCEDURES DURING COCKPIT PREPARATION - ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST - Check that the associated CTL pb FAULT light comes on. 52-01-02-01B
CDLS back-up C system considered inoperative
2
0
One or more may be inoperative provided that the CDLS back-up system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.03 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01 52-01-02
Overhead Panels CKPT DOOR CONT BK UP Overhead Panel
52-01-02-02 STRIKE (TOP, MID, BOT) LEDs on the CKPT DOOR CONT BK UP Overhead Panel 52-01-02-02A
CTL pb FAULT C light checked operative
3
2
(O)
One may be inoperative provided that the CTL pb FAULT light is checked operative. OPERATING PROCEDURES DURING COCKPIT PREPARATION - ANN LT selector . . . . . . . . . . . . . . . . . . . . . . . . . TEST - Check that the associated CTL pb FAULT light comes on.
52-01-02-02B
CDLS back-up C system considered inoperative
3
0
One or more may be inoperative provided that the CDLS back-up system is considered inoperative.
Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
A320/321 MEL/CDL
01.52.04 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01
Overhead Panels
52-01-02
CKPT DOOR CONT BK UP Overhead Panel
52-01-02-03Pressure Rate Sensor on the CKPT DOOR CONT BK UP Overhead Panel
52-01-02-03A
One inoperative
A
2
1
(M)
One may be inoperative for 60 consecutive calendar days provided that the remaining pressure rate sensor is checked operative.
MAINTENANCE PROCEDURE Refer to AMM 52-51-00-040-012 52-01-02-03B
Both inoperative
C
2
0
Both may be inoperative provided that the CDLS back-up system is considered inoperative. Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.05 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01 52-01-03
Overhead Panels CKPT DOOR BK UP Overhead Panel
52-01-03-01 CTL pb FAULT light on the CKPT DOOR BK UP Overhead Panel
52-01-03-01A
C
1
0
(O)
May be inoperative.
OPERATING PROCEDURES DURING COCKPIT PREPARATION · To ensure that the door is closed and locked: On the CKPT DOOR CONT BK UP panel, check that the three STRIKE LEDs are off.
52-01-03-01B
C
1
0
May be inoperative provided that the CDLS back-up system is considered inoperative. Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
A320/321 MEL/CDL
01.52.06 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01
Overhead Panel
52-01-03
CKPT DOOR BK UP Overhead Panel
52-01-03-02 CTL pb OPEN light on the CKPT DOOR BK UP Overhead Panel 52-01-03-02A
C
1
0
(O)
May be inoperative.
OPERATING PROCEDURES DURING COCKPIT PREPARATION · To ensure that the door is closed and locked: On the CKPT DOOR CONT BK UP panel, check that the three STRIKE LEDs are off.
52-01-03-02B
C
1
0
May be inoperative provided that the CDLS back-up system is considered inoperative. Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.07 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01 52-01-03
Overhead Panel CKPT DOOR BK UP Overhead Panel
52-01-03-31 CTL pb on the CKPT DOOR BK UP Overhead Panel 52-01-03-31A
C
1
0
(O)
May be inoperative.
OPERATING PROCEDURES - Manual opening from the cockpit has to be performed by the cockpit crew. One additional crew member must lock or unlock the cockpit door manually whenever access to the flight deck is granted or one of the crew leaves the cockpit.
52-01-03-31B
C
1
0
May be inoperative provided that the CDLS back-up system is considered inoperative. Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
A320/321 MEL/CDL
01.52.08 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01
Overhead Panel
52-01-03
CKPT DOOR BK UP Overhead Panel
52-01-03-32 BK UP Function of the LKG SYS sw on the CKPT DOOR BK UP Overhead Panel 52-01-03-32A
C
1
0
May be inoperative provided that the CDLS back-up system is considered inoperative. Refer to Item 52-51-02 CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
52-01-03-33 NORM Function of the LKG SYS sw on the CKPT DOOR BK UP Overhead Panel 52-01-03-33A
C
1
0
May be inoperative provided that the CDLS normal system is considered inoperative. Refer to Item 52-51-01 CDLS Normal System (Normal Control Unit, Switch and Lights on the CKPT DOOR Panel, Buzzer, Keypad)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.09 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-01 52-01-03
Overhead Panel CKPT DOOR BK UP Overhead Panel (cont’d)
52-01-03-34 OFF Function of the LKG SYS sw on the CKPT DOOR BK UP Overhead Panel
52-01-03-34A
C
1
0
(M)
May be inoperative. Note: For maintenance purpose only, the CDLS normal and the CDLS back-up systems can be deactivated by performing the associated maintenance procedure.
MAINTENANCE PROCEDURE Refer to AMM 52-51-00-040-008
A320/321 MEL/CDL
01.52.10 DOORS 1.
ITEM
SYSTEM & SEQUENCE OF ITEMS
DOORS
52-07
Indications on the DOOR/OXY SD page
52-07-01A
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
52
52-07-01
2.
12 FEB 12 MEL
REMARKS OR EXCEPTIONS
Passenger Door Permanently Indicated Open on the DOOR/OXY SD page (A320) Check of C associated door and 'C' repair interval
4
0
(O)(FD) One or more may be permanently indicated open when actually closed provided that: 1) The associated door is visually checked to be closed and locked before each flight, and 2) The white SLIDE ARMED light on the associated door does not come on when the door is closed and locked and the slide arming lever is in the armed position. OPERATING PROCEDURES GENERAL INFORMATION If passenger doors are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong. AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.52.11 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01A
Passenger Door Permanently Indicated Open on the DOOR/OXY SD page (A320) Check of associated door and 'C' repair interval (cont’d)
OPERATING PROCEDURES (cont’d) BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST.
CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
A320/321 MEL/CDL
01.52.12 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01B
Passenger Door Permanently Indicated Open on the DOOR/OXY SD page (A320) Check of B associated door and 'B' repair interval
4
0
(O)(FD) One or more may be permanently indicated open when actually closed provided that the associated door is visually checked to be closed and locked before each flight. OPERATING PROCEDURES GENERAL INFORMATION If passenger doors are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong. The SLIDE ARMED light on passenger doors may be permanently illuminated. AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.13 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01B
Passenger Door Permanently Indicated Open on the DOOR/OXY SD page (A320) Check of associated door and 'B' repair interval (cont’d)
OPERATING PROCEDURES (cont’d)
BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
52-07-01C
No night operations
C
4
0
(O)(FD) One or more may be permanently indicated open when actually closed provided that: 1) The aircraft is not operated at night, and 2) The associated door is visually checked to be closed and locked before each flight. OPERATING PROCEDURES Refer to MEL item 52-07-01B
A320/321 MEL/CDL
01.52.14 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01A
Passenger Door/Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page (A321) Check of C associated door and 'C' repair interval
8
0
(O)(FD) One or more may be permanently indicated open when actually closed provided that: 1) The associated door is visually checked to be closed and locked before each flight, and 2) The white SLIDE ARMED light on the associated door does not come on when the door is closed and locked and the slide arming lever is in the armed position.
OPERATING PROCEDURES GENERAL INFORMATION If passenger doors/emergency exits are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.52.15 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01A
Passenger Door/Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page (A321) Check of associated door and 'C' repair interval (cont’d)
OPERATING PROCEDURES (cont’d) AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
A320/321 MEL/CDL
01.52.16 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01B
Passenger Door/Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page (A321) Check of B associated door and 'B' repair interval
8
0
(O)(FD) One or more may be permanently indicated open when actually closed provided that the associated door is visually checked to be closed and locked before each flight. OPERATING PROCEDURES GENERAL INFORMATION If passenger doors/emergency exits are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong. The SLIDE ARMED light on passenger doors/emergency exit may be permanently illuminated. AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.17 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-01
52-07-01B
Passenger Door/Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page (A321) Check of associated door and 'B' repair interval (cont’d)
OPERATING PROCEDURES (cont’d) BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
52-07-01C
No night operations
C
8
0
(O)(FD) One or more may be permanently indicated open when actually closed provided that: 1) The aircraft is not operated at night, and 2) The associated door is visually checked to be closed and locked before each flight. OPERATING PROCEDURES Refer to MEL item 52-07-01B
A320/321 MEL/CDL
01.52.18 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-02
52-07-02A
Passenger Door Permanently Indicated Closed on the DOOR/OXY SD page (A320) No night operations
C
4
0
(O)(FD) One or more may be permanently indicated closed when actually open provided that: 1) The aircraft is not operated at night, and 2) The associated door is visually checked to be closed and locked before each flight.
OPERATING PROCEDURES GENERAL INFORMATION If passenger doors are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.19 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-02
52-07-02A
Passenger Door/Emergency Exit Permanently Indicated Closed on the DOOR/OXY SD page (A321) No night operations
C
8
0
(O)(FD) One or more may be permanently indicated closed when actually open provided that: 1) The aircraft is not operated at night, and 2) The associated door is visually checked to be closed and locked before each flight.
OPERATING PROCEDURES GENERAL INFORMATION If passenger doors/emergency exits are affected, indications on the PTP or the FAP may be affected. If passenger doors are affected, the time recorded in the ACARS movement report may be wrong.
A320/321 MEL/CDL
01.52.20 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-03
52-07-03A
Overwing Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page Check of C associated exit and 'C' repair interval
2
0
(O)(M) One or both may be permanently indicated open when (FD) actually closed provided that: 1) The associated exit is visually checked to be closed and locked before each flight, and 2) The relevant SLIDE indication on the DOOR/OXY SD page is normally displayed in white. OPERATING PROCEDURES GENERAL INFORMATION Indications on the PTP or the FAP ñ– may be affected. AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.52.21 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-03
52-07-03A
Overwing Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page Check of associated exit and 'C' repair interval (cont’d)
OPERATING PROCEDURES (Cont’d)
BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert were displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert.
MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-010
A320/321 MEL/CDL
01.52.22 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-03
52-07-03B
Overwing Emergency Exit Permanently Indicated Open on the DOOR/OXY SD page (A320) Check of B associated exit and 'B' repair interval
2
0
(O)(M) One or both may be permanently indicated open when actually closed provided that the associated exit is visually checked to be closed and locked before each flight. OPERATING PROCEDURES Refer to MEL item 52-07-03A
MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-010
52-07-03C
No night operations
C
2
0
(O)(M) One or more may be permanently indicated open when (FD) actually closed provided that: 1) The aircraft is not operated at night, and 2) The associated exit is visually checked to be closed and locked before each flight. OPERATING PROCEDURES Refer to MEL item 52-07-03A
MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-010
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.23 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-04
52-07-04A
Overwing Emergency Exit Permanently Indicated Closed on the DOOR/OXY SD page (A320) No night operations
C
2
0
(O)(M) One or more may be permanently indicated closed when (FD) actually open provided that: 1) The aircraft is not operated at night, and 2) The associated exit is visually checked to be closed and locked before each flight.
OPERATING PROCEDURES GENERAL INFORMATION Indications on the PTP or the FAP may be affected.
MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-011
A320/321 MEL/CDL
01.52.24 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-05
52-07-05A
Cargo Door Indication on the DOOR/OXY SD page C
3
0
(O)(M) One or more may be inoperative provided that the (FD) associated door is visually checked to be closed and locked before each flight. OPERATING PROCEDURES GENERAL INFORMATION · If cargo indication is inoperative due to a proximity switch failure: The relevant cargo heating is inhibited. Live animals must not be carried in the cargo. AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press
Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.25 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-05
Cargo Door Indication on the DOOR/OXY SD page
52-07-05A (cont’d)
OPERATING PROCEDURES (Cont’d) BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert was displayed during the T.O CONFIG TEST. CAUTION The T.O CONFIG pb must be maintained pressed to check that there is no alert. MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-001
52-07-06
52-07-06A
Avionics Compartment Access Door Indication on the DOOR/OXY SD page C
4
0
(O)(M) One or more may be inoperative provided that the (FD) associated door is visually checked to be closed and locked before each flight.
(Cont’d on next page)
A320/321 MEL/CDL
01.52.26 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
Indications on the DOOR/OXY SD page
52-07-06
Avionics Compartment Access Door Indication on the DOOR/OXY SD page
52-07-06A (cont’d)
OPERATING PROCEDURES AFTER ENGINE START · In the case of false door alert: EMER CANC pb . . . . . . . . . . . . . . . . . . . . . . . . . . Press Note: the limitation MAX FL : 100/MEA remains displayed on the STATUS SD page. BEFORE TAKEOFF - T.O CONFIG pb . . . . . . . . . . . . . . . . . . . . . . . . . Press In the T.O MEMO, the "T.O CONFIG NORMAL" line will not replace the "T.O CONFIG . . TEST" line. - Consider normal configuration for takeoff provided that no alert were displayed during the T.O CONFIG TEST.
MAINTENANCE PROCEDURE Refer to AMM 52-70-00-040-004
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.27 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-10
Passenger/Crew Door
52-10-01
Cabin Passenger Door
52-10-01A 52-10-02 (A320)
52-10-03A
4
Must be operative.
2
2
Must be operative.
Overwing Emergency Exit
52-10-02A
52-10-03
4
Passenger Exit Stop Fitting (A320)
C
56 52 (FD)
(A321)
C
96 90
A maximum of one per exit may be inoperative provided that the flight is not pressurized, and
Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Cabin
Flight must be conducted in accordance with FOPM CH 8 Maintenance Ferry Flights. 52-10-04 (A320)
Door Damper Function
52-10-04A 52-10-04 (A321) 52-10-04A
C
4
0
One or more may be inoperative.
C
8
0
One or more may be inoperative.
Door Damper Function
A320/321 MEL/CDL
01.52.28 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-10
Passenger/Crew Door
52-10-05 52-10-05A
52-10-06
52-10-06A
Door Emergency Opening Function (A320)
4
4
(A321)
8
8
CHECK DOOR PRESSURE Message on the Flight Attendant Panel (FAP) (A320)
C
4
0
(A321)
C
8
0
(M)
One or more messages may be displayed provided that the door bottle pressure is checked on the associated bottle pressure gauge before the first dispatch and then every 8 days. MAINTENANCE PROCEDURE Refer to AMM 52-00-00-040-003
52-10-07
52-10-07A
Passenger Door Stay Mechanism (A320)
4
4
(A321)
8
8
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.29 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-10
Passenger/Crew Door
52-10-08
CABIN PRESSURE light (on Doors)
52-10-08A
(A320)
C
4
0
(A321)
C
8
0
52-30-01A
Cargo door C indicated locked on the DOOR/OXY SD page
3
0
52-30-01B
Visual check of C the cargo door
3
0
52-30
One or more may be inoperative.
Cargo Door
52-30-01
Cargo Door (FWD, AFT and BULK) One or more may be inoperative in the closed and locked position provided that they are indicated locked on the DOOR/OXY SD page.
(M)
One or more may be inoperative in the closed and locked position provided that the associated cargo door is visually checked to be closed and locked before each flight. MAINTENANCE PROCEDURE Refer to AMM 52-30-00-040-001
52-30-02 52-30-02A
Cargo Door Actuator A maximum of A one actuator inoperative per cargo door
4
2
(FD)
A maximum of one per cargo door may be inoperative provided that: 1) The integrity of the yellow hydraulic system is not affected, and 2) The wind velocity during loading and unloading operations is below 30 kt, and 3) The operation of the door with a single actuator is limited to 100 open/close cycles.
A320/321 MEL/CDL
01.52.30 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-30
Cargo Door
52-30-02 52-30-02B
Cargo Door Actuator One or more actuator inoperative
C
4
0
(M)
One or more may be inoperative provided that: 1) The integrity of the yellow hydraulic system is not affected, and 2) The associated cargo door is manually closed and locked. MAINTENANCE PROCEDURE Refer to AMM 52-36-00-040-001
52-30-03
Cargo Door Electrical Control
52-30-03A
Cargo door C operated using hand pump
2
0
52-30-03B
Cargo door considered inoperative
2
0
C
One or more may be inoperative provided that the associated cargo doors can be operated using the hand pump. (FD)
One or more may be inoperative provided that the associated cargo doors are considered inoperative. Refer to Item 52-30-01 Cargo Door (FWD, AFT)
52-30-04
52-30-04A
Cargo Door Locking Hooks and Spools (Rollers) (Hooks)
C
14 11 (FD)
(Spools)
C
14 11
A maximum of one locking hook or one spool per cargo door may be inoperative provided that: 1) All the others have no damage, and 2) The flight is not pressurized. Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Cabin
Flight must be conducted in accordance with FOPM CH 8 Maintenance Ferry Flights.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.31 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-30
Cargo Door
52-30-05
Cargo Door Hand Pump
52-30-05A 52-30-06
52-30-07A
1
0
May be inoperative provided that the integrity of the yellow hydraulic system is not affected.
A
4
0
One or both on each cargo door may be inoperative for one flight.
C
2
0
Cargo Door Drift Pin
52-30-06A 52-30-07
C
Cargo Doors Open/Locked Indicator light (O)
One or both may be inoperative provided that the associated cargo door is in the fully open position during loading and unloading operations. OPERATING PROCEDURES ON GROUND · When the Cargo Door Open/Locked Indicator light is inoperative, it is necessary to inform the ground personnel: - To visually check that the affected cargo door is in the fully open position, with no downward movement after releasing the lever of the manual selector valve. - To visually check that the lever of the manual selector valve stays in the neutral position.
A320/321 MEL/CDL
01.52.32 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-33
Bulk Cargo Compartment Door
52-33-01
Cargo Door Balance Mechanism
52-33-01A
C
1
0
(M)
May be inoperative or damaged provided that: 1) A safety hold device is used to maintain the cargo door in the open position during loading and unloading operations, and 2) The associated cargo door is visually checked to be closed and locked. MAINTENANCE PROCEDURE Refer to AMM 52-33-00-040-001
52-51
Reinforced Cockpit Door (CDLS)
52-51-01
52-51-01A
CDLS Normal System (Normal Control Unit, Switch and Lights on the CKPT DOOR Panel, Buzzer, Keypad) CDLS back-up C control unit operative
Note:
1
0
(O)
Any part of the CDLS may be inoperative provided the complete system is deactivated in the unlocked position and is not required by operational regulations for the intended flight. May be inoperative provided that: 1) The interphone system between the cabin and the cockpit is operative, and 2) The LKG SYS selector on the CKPT DOOR BK UP panel is set to the BK UP position , and 3) The CDLS back-up control unit is operative.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.52.33 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-51
Reinforced Cockpit Door (CDLS)
52-51-01
52-51-01A
CDLS Normal System (Normal Control Unit, Switch and Lights on the CKPT DOOR Panel, Buzzer, Keypad) CDLS back-up control unit operative (cont’d)
OPERATING PROCEDURES PIC brief cabin crew before departure to use the cabin interphone to communicate with the cockpit crew to request access to the cockpit, and A third crew member must be available in the cockpit when a flight crew member leaves the cockpit during flight
DURING COCKPIT PREPARATION LKG SYS sw . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BK UP The CDLS keypad operation is not available in back-up mode. The cockpit crew must brief the cabin crew that the CDLS keypad is inoperative.
IN FLIGHT At least two people must always be present in the cockpit throughout the entire flight.
A320/321 MEL/CDL
01.52.34 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-51
Reinforced Cockpit Door (CDLS)
52-51-02
CDLS BK UP System (Back-up Control Unit, CTL pb and Lights on the CKPT DOOR BK UP Panel)
52-51-02A 52-51-03
C
1
0
C
1
0
May be inoperative.
CDLS Buzzer
52-51-03A
(O)
May be inoperative provided: 1) Keypad is deactivated, and 2) Alternate procedures are established and used. OPERATING PROCEDURES Flight attendants shall be briefed not to use the keypad and instead use interphone and pre-arranged knocks on the door when entry is required.
52-51-04 52-51-04A
CDLS Keypad C
1
0
(O)(M) May be inoperative provided : (FD) 1) The interphone system between the cabin and the cockpit is operative, and 2) The keypad is deactived.
(Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.35 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-51
Reinforced Cockpit Door (CDLS)
52-51-04
CDLS Keypad
52-51-04A (Cont’d)
OPERATING PROCEDURES 1. Flight attendants shall be briefed on an alternate flight deck entry procedure which requires the use of cabin interphone and a specified sequence of knocks on the door. 2. A third crew member must be available in the cockpit when a flight crew member leaves the cockpit during flight. MAINTENANCE PROCEDURE Refer to AMM 52-51-00-040-007
52-51-05
52-51-05A
CDLS Keypad Green and Red LEDs C
2
0
(O)(FD) May be inoperative provided alternate procedures are established and used.
OPERATING PROCEDURES 1. Flight attendants shall be briefed on an alternate flight deck entry procedure which requires the use of cabin interphone and a specified sequence of knocks on the door. 2. A third crew member must be available in the cockpit when a flight crew member leave the cockpit during flight.
A320/321 MEL/CDL
01.52.36 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-51
Reinforced Cockpit Door (CDLS)
52-51-06
CDLS Door Release Strike (Catch, Spring, Solenoid, Bolt)
52-51-06A
C
3
2
(M)
One may be inoperative provided associated door release strike is deactivated or removed. NOTE: Application of the maintenance procedure is only necessary when the inoperative door release strike is failed in locked position. MAINTENANCE PROCEDURE Refer to AMM 52-51-00-040-010
52-53
COCKPIT DOOR Panel on the Center Pedestal
52-53-01 52-53-01
COCKPIT DOOR FAULT light B
1
0
(M)
May be inoperative provided: 1) Automatic lock controls are verified operative, and 2) Door chime is operative. MAINTENANCE PROCEDURE Refer to AMM 52-51-00-810-801
A320/321 MEL/CDL
01 MAY 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.52.37 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-53
COCKPIT DOOR Panel on the Center Pedestal
52-53-02
COCKPIT DOOR OPEN light
52-53-02A
52-53-03
B
1
0
B
1
0
May be inoperative provided automatic lock controls are verified operative.
LOCK Function of the COCKPIT DOOR sw
52-53-03A
(O)
May be inoperative provided: 1) The cockpit deactivated.
door
locking
system
keypad
is
2) Alternate procedures are established and used. OPERATING PROCEDURES Refer to MEL item 52-51-01A 52-53-04
52-53-04A
UNLOCK Function of the COCKPIT DOOR sw B
1
0
(O)
May be inoperative provided alternate procedures are established and used. OPERATING PROCEDURES: One additional crew member must lock or unlock the cockpit door manually whenever access to the flight deck is granted or one of the crew leaves the cockpit. *
*
*
A320/321 MEL/CDL
01.52.38 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.56.01 WINDOWS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
56 WINDOWS 56-10
Cockpit
56-10-01
Front Windshield
Note: A cockpit window with minor damages (as described in the associated maintenance procedure) is considered operative, but the vision through this cockpit window must be acceptable to the flight crew.
56-10-01C
For SPS A Windshields (P/N STA320-13-1 and STA320-2-3-1)
2
2
(O)(M) One front windshield external ply may be cracked for one (FD) flight provided that: 1) The other front windshield is not damaged, and 2) The associated windshield heating is deactivated, and 3) The visibility through the associated front windshield is acceptable to the flight crew, and 4) The aircraft is not operated in known or forecast icing conditions.
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS < When PF side is affected: Maximum landing capability is CAT I < When PNF side is affected: Maximum landing capability is not affected and is still CAT II. MAINTENANCE PROCEDURE Refer to AMM 56-10-00-040-001
A320/321 MEL/CDL
01.56.02 WINDOWS 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
56 WINDOWS 56-10
Cockpit
56-10-01 56-10-01D
Front Windshield For SPS C Windshields (only P/N STA320-1-3-1 and STA320-23-1)
2
2
(O)(M) One front windshield may have burn spots in the bus bar (FD) area beyond the limits provided that: 1) The other front windshield is not damaged, and 2) The associated windshield heating is deactivated, and 3) The visibility through the associated front windshield is acceptable to the flight crew, and 4) The aircraft is not operated in known or forecast icing conditions. OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS < When PF side is affected: Maximum landing capability is CAT I < When PNF side is affected: Maximum landing capability is not affected and is still CAT II. MAINTENANCE PROCEDURE Refer to AMM 56-10-00-040-001
56-10-02
Lateral Fixed/Sliding Window
Note: A cockpit window with minor damages (as described in the associated maintenance procedure) is considered operative, but the vision through this cockpit window must be acceptable to the flight crew.
A320/321 MEL/CDL
12 FEB 12 MEL 1.
2.
ITEM
SYSTEM & SEQUENCE OF ITEMS
01.56.03 WINDOWS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
56 WINDOWS 56-10
Cockpit
56-10-03
Sliding Window Opening/Closing Mechanism
56-10-03A 56-20
2
2
Both must be operative.
Cabin
56-20-01 56-20-01A
Cabin Window (A320)
A
36 30 (FD)
(A321)
A
44 40
One or more may be cracked for one flight day provided that the flight is not pressurized. Refer to FCOM/PRO-SPO-20 Pressurized.
Fligt
Without
Cabin
Flight must be conducted in accordance with FOPM CH 8 Maintenance Ferry Flight
*
*
*
A320/321 MEL/CDL
01.56.04 WINDOWS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.70.01 ENGINE
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
70 ENGINE 70-00
MAINTENANCE Messages on the STATUS SD page
70-00-01
ENG FADEC MAINTENANCE Message
70-00-01B
For Engines Affected by CFM VSB 730241
A
1
-
70-00-01C
For Engines Affected by CFM VSB 730241
C
1
-
ENG FADEC MAINTENANCE message may be displayed on the STATUS SD page for 25 flight hours or 3 days, whichever occurs first. (M)
ENG FADEC MAINTENANCE message may be displayed on the STATUS SD page provided it is checked before the first flight of each day that the CFDS does not report any fault on a T12 sensor. MAINTENANCE PROCEDURE Refer to AMM 73-29-00-040-001
70-00-02
ENG EIU MAINTENANCE Message
70-00-02A 70-00-03
70-00-03A
C
1
-
ENG EIU MAINTENANCE message may be displayed on the STATUS SD page.
C
1
-
ENG EVMU MAINTENANCE message may be displayed on the STATUS SD page.
ENG EVMU MAINTENANCE Message
*
*
*
A320/321 MEL/CDL
01.70.02 ENGINE 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.73.01 ENGINE FUEL AND CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
73 ENGINE FUEL AND CONTROL 73-07
Indications on the ENGINE SD page
73-07-01
F. USED Indication on the ENGINE SD page
73-07-01A
73-07-02
One indication inoperative
2
1
One may be inoperative provided that the fuel quantity indications of the associated tanks are operative on the FUEL SD page.
C
2
0
One or both may be inoperative.
C
2
1
One may be inoperative.
Fuel Filter Clog Indication on the ENGINE SD page
73-07-02A
73-08
C
Indications on the EWD
73-08-01
73-08-01A
Fuel Flow Indication on the EWD
A320/321
01.73.02 ENGINE FUEL AND CONTROL
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
73 ENGINE FUEL AND CONTROL 73-09
ECAM Alert
73-09-01
ENG 1(2) FUEL FILTER CLOG Alert
73-09-01A
C
2
1
(M)
One may be displayed provided that: 1) The alert is confirmed to be false by troubleshooting, and 2) The associated filter is replaced every day. MAINTENANCE PROCEDURE Refer to AMM 73-30-00-040-043
73-10
Distribution
73-10-01
Fuel Return Valve
73-10-01A
Inoperative in C closed position
2
1
One may be inoperative in the closed position on one engine provided that the APU and the AC auxiliary generation are operative.
73-10-01B
Inoperative in open position
2
0
One or both may be inoperative in the open position provided that the four wing tank pumps are operative.
2
2
Both must be operative.
2
0
May be inoperative on one or both engines provided that the maximum thrust is used for takeoff.
73-10-03
C
Fuel Metering Valve
73-10-03A 73-20
Controlling
73-20-01 73-20-01A
Flex Takeoff Mode C
A320/321
01.73.03 ENGINE FUEL AND CONTROL
MEL/CDL
30 JUN 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
73 ENGINE FUEL AND CONTROL 73-20
Controlling
73-20-05 73-20-05A
Minimum Idle on Ground C
2
0
(O)
One or both may be inoperative provided that the Flight Manual performance penalties are applied. OPERATING PROCEDURES (A321) FLIGHT PREPARATION/LIMITATIONS Takeoff performance: For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch or use the following penalties for takeoff and landing performance determination if MTTL charts are not available. Takeoff must be performed with full thrust. VMCG/VMCA limitation
No VMCG/VMCA limitation
Weight decrement (kg)
1300
400
V1, VR, V2 decrement (kt IAS)
0
2
Landing performance: No penalty.
(Cont’d on next page)
A320/321
01.73.04 ENGINE FUEL AND CONTROL
MEL/CDL
1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
30 JUN 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
73 ENGINE FUEL AND CONTROL 73-20
Controlling
73-20-05
Minimum Idle on Ground
73-20-05A (cont’d)
OPERATING PROCEDURES (A320) FLIGHT PREPARATION/LIMITATIONS Takeoff performance: For performance calculations request Modified Tailored Takeoff and Landing charts (MTTL) from FPE through Flight Dispatch or use the following penalties for takeoff and landing performance determination if MTTL charts are not available.. Takeoff must be performed with full thrust. VMCG/VMCA limitation
No VMCG/VMCA limitation
Weight decrement (kg)
1500
200
V1, VR, V2 decrement (kt IAS)
0
1
Landing performance: No penalty.
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.74.01 IGNITION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
74 IGNITION 74-07
Indications on the ENGINE SD page
74-07-01
74-07-01A
Selected Igniter Indication on the ENGINE SD page C
4
0
(O)
One or more may be inoperative provided that the associated ENG 1(2) IGN A(B)(A+B) FAULT alert is checked operative.
OPERATING PROCEDURES AFTER ENGINE START · If engine 1 is affected: - ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL - ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL - ENGINE/IGN/ENG 1/ SYS B (121VU P41) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL · If engine 2 is affected: - ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL - ENGINE/IGN/ENG 2/ SYS A BAT (121VU P40) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL - ENGINE/IGN/ENG 2/ SYS B (121VU P42) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
(Cont’d on next page)
A320/321 MEL/CDL
01.74.02 IGNITION 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
74 IGNITION 74-07
Indications on the ENGINE SD page
74-07-01
Selected Igniter Indication on the ENGINE SD page
74-07-01A (cont’d)
OPERATING PROCEDURES (Cont’d) On the EWD, check that the ENG 1(2) A+B IGN FAULT alert is displayed. · If engine 1 is affected: - ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH - ENGINE/IGN/ENG 1/ SYS A BAT (121VU P39) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH - ENGINE/IGN/ENG 1/ SYS B (121VU P41) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH · If engine 2 is affected: - ENGINE/1 AND 2/IGN/SYS A (49VU A03) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH - ENGINE/IGN/ENG 2/ SYS A BAT (121VU P40) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH - ENGINE/IGN/ENG 2/ SYS B (121VU P42) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.74.03 IGNITION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
74 IGNITION 74-09
ECAM Alert
74-09-01
ENG 1(2) IGN A(B)(A+B) FAULT Alert
74-09-01B
One displayed
C
4
3
(M)
One may be displayed provided that the associated engine ignition system is checked operative every day. MAINTENANCE PROCEDURE Refer to AMM 74-31-040-001
74-09-01C
Two displayed
C
4
2
(M)
Two may be displayed provided that the associated engine ignition systems are checked operative before each flight. MAINTENANCE PROCEDURE Refer to AMM 74-31-040-001
74-31
Ignition Starting and Continuous Relight
74-31-01 74-31-01A
Ignition System A C
2
1
(O)
One may be inoperative provided that the associated engine ignition system B is operative. OPERATING PROCEDURES BEFORE ENGINE START ENGINE/1 AND 2/IGN/SYS A (49 VU A03) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL AFTER ENGINE START ENGINE/1 AND 2/IGN/SYS A (49 VU A03) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH
A320/321 MEL/CDL
01.74.04 IGNITION 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
74 IGNITION 74-31
Ignition Starting and Continuous Relight
74-31-02 74-31-02A
Ignition System B C
2
0
(O)
One or both may be inoperative. OPERATING PROCEDURES BEFORE ENGINE START ENGINE/IGN/ENG (1 and/or 2)/SYS B (121 VU P41/P42) C/B . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PULL
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.76.01 ENGINE CONTROLS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
76 ENGINE CONTROLS 76-11
Throttle Control
76-11-01 76-11-01A
Thrust lever Position Sensor A
4
3
One may be inoperative on one engine for three days provided that: 1) The A/THR is operative, and 2) Both LGCIUs are operative, and 3) The L/G shock absorbers proximity detectors are operative.
*
*
*
A320/321 MEL/CDL
01.76.02 ENGINE CONTROLS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.77.01 ENGINE INDICATING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
77 ENGINE INDICATING 77-07 77-07-01
Indications on SD pages Indications on the CRUISE SD page
77-07-01-01 N1 Vibration Indication on the CRUISE SD page 77-07-01-01A
Refer to Item 77-07-02-05 N1 Vibration Indication on the ENGINE SD page
77-07-01-02 N2 Vibration Indication on the CRUISE SD page 77-07-01-02A
Refer to Item 77-07-02-06 N2 Vibration Indication on the ENGINE SD page
77-07-01-03 F. USED (Fuel Used) Indication on the CRUISE SD page 77-07-01-03A
Refer to Item 73-07-01 Fuel Used Indication on the ENGINE SD page
77-07-01-04 OIL QT (Oil Quantity) Indication on the CRUISE SD page 77-07-01-04A
Refer to Item 79-07-03 Oil Quantity Indication on the ENGINE SD page
A320/321 MEL/CDL
01.77.02 ENGINE INDICATING 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
77 ENGINE INDICATING 77-07
Indications on SD pages
77-07-02
Indications on the ENGINE SD page
77-07-02-01 Engine Bleed Pressure Indication on the ENGINE SD page 77-07-02-01A
Refer to Item 36-07-04 Engine Bleed Precooler Inlet Pressure Indication on the BLEED SD page
77-07-02-02 Fuel Filter Clog Indication on the ENGINE SD page 77-07-02-02A
Refer to Item 73-07-02 Fuel Filter CLOG Indication on the ENGINE SD page
77-07-02-03 Fuel Used Indication on the ENGINE SD page 77-07-02-03A
Refer to Item 73-07-01 Fuel Used Indication on the ENGINE SD page
77-07-02-04 Nacelle Temperature Indication on the ENGINE SD page 77-07-02-04A
C
2
0
One or both may be inoperative.
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.77.03 ENGINE INDICATING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
77 ENGINE INDICATING 77-07 77-07-02
Indications on SD pages Indications on the ENGINE SD page
77-07-02-05 N1 Vibration Indication on the ENGINE SD page 77-07-02-05A
One indication inoperative
C
2
1
One may be inoperative.
77-07-02-05B
Both indications A inoperative
2
0
Both may be inoperative for three flights provided that no vibration advisory was displayed during the previous flight.
77-07-02-06 N2 Vibration Indication on the ENGINE SD page 77-07-02-06A
One indication inoperative
C
2
1
One may be inoperative.
77-07-02-06B
Both indications A inoperative
2
0
Both may be inoperative for three flights provided that no vibration advisory was displayed during the previous flight.
77-07-02-07 Oil Filter Clog Indication on the ENGINE SD page 77-07-02-07A
Refer to Item 79-07-01 CLOG Indication on the ENGINE SD page
A320/321 MEL/CDL
01.77.04 ENGINE INDICATING 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
77 ENGINE INDICATING 77-07
Indications on SD pages
77-07-02
Indications on the ENGINE SD page (cont’d)
77-07-02-08 Oil Pressure Indication on the ENGINE SD page 77-07-02-08A
Refer to Item 79-07-02 Oil Pressure Indication and Advisory on the ENGINE SD page
77-07-02-09 Oil Quantity Indication on the ENGINE SD page 77-07-02-09A
Refer to Item 79-07-03 Oil Quantity Indication on the ENGINE SD page
77-07-02-10 Oil Temperature Indication on the ENGINE SD page 77-07-02-10A
Refer to Item 79-07-04 Oil Temperature Indication on the ENGINE SD page
77-07-02-11 Selected Igniter Indication on the ENGINE SD page 77-07-02-11A
Refer to Item 74-07-01 Selected Igniter Indication on the ENGINE SD page
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.77.05 ENGINE INDICATING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
77 ENGINE INDICATING 77-07
Indications on SD pages (cont’d)
77-07-02
Indications on the ENGINE SD page
77-07-02-12 Start Valve Position Indication on the ENGINE SD page 77-07-02-12A 77-08
Refer to Item 80-07-01 Start Valve Position Indication on the ENGINE SD page
Indications on the EWD
77-08-01
EGT Indication on the EWD
77-08-01A 77-08-03
2
2
Fuel Flow Indication on the EWD
77-08-03A 77-08-04
Refer to Item 73-08-01 Fuel Flow Indication on the EWD N1 Indication on the EWD
77-08-04A 77-08-05 77-08-05A
Must be operative.
2
2
Must be operative.
2
2
Must be operative.
N2 Indication on the EWD
*
*
*
A320/321 MEL/CDL
01.77.06 ENGINE INDICATING 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.78.01 EXHAUST
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
78 EXHAUST 78-08
Indications on the EWD
78-08-01
REV Indication on the EWD
78-08-01A
78-30
-
2
2
C
2
1
Both must be operative.
Thrust Reversers
78-30-01
78-30-01A
Thrust Reverser
(O)(M) One may be inoperative provided that: (FD) 1) The inoperative thrust reverser is deactivated and secured in the stowed position, and 2) All stow and deploy switches circuits on the inoperative thrust reverser are checked operative, and 3) The ENG 1(2) REV PRESSURIZED alert is not displayed on the EWD after deactivation, and 4) The appropriate performance adjustments are applied.
(Cont’d on next page)
A320/321 MEL/CDL
01.78.02 EXHAUST 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
78 EXHAUST 78-30
Thrust Reversers
78-30-01
Thrust Reverser
78-30-01A (cont’d)
OPERATING PROCEDURES FLIGHT PREPARATION/LIMITATIONS Performance Adjustments: Runway State Takeoff Dry, or
One Thrust Reverser Inoperative
Landing Dry, or Landing Wet
Performance Adjustments No performance adjustments are necessary (Basic performance data is computed without thrust reversers) Use performance data computed with :
Takeoff Wet
- One thrust reverser inoperative. (Refer to SV A320/321 Performance Manual CH 12)
FOR TAKEOFF During the takeoff briefing, the flight crew must review: - The status of the thrust reversers, and - The use of the thrust reversers (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
01.78.03 EXHAUST
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
78 EXHAUST 78-30 78-30-01
Thrust Reversers Thrust Reverser
78-30-01A (cont’d)
OPERATING PROCEDURES (cont’d) REJECTED TAKEOFF Ensure that both engine thrust levers are set to IDLE detent, then: · If one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust.
Note: ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after selection of the reverse thrust.
IN FLIGHT · Should a failure occur with "LDG DIST PROC.......APPLY" message displayed on the STATUS SD page, and Whatever the actual thrust reversers selection at landing: To calculate the LDG DIST with the in-flight failure, use, as a conservative approach, the LDG DIST factors “WITHOUT REV” (LDG CONF/APP SPD/LDG DIST FOLLOWING FAILURES tables in the QRH part 2).
(Cont’d on next page)
A320/321 MEL/CDL
01.78.04 EXHAUST 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
78 EXHAUST 78-30
Thrust Reversers
78-30-01
Thrust Reverser
78-30-01A (cont’d)
OPERATING PROCEDURES (cont’d) DURING APPROACH During the approach briefing, the flight crew must review: - The status of the thrust reversers, and - The use of the thrust reversers FOR LANDING Before the touchdown, ensure that both engine thrust levers are set to IDLE detent for the flare. · After touchdown, if one thrust reverser is inoperative: Use both thrust levers when applying reverse thrust. Note: ENG (AFFECTED SIDE) REVERSER FAULT alert is displayed on the EWD after selection of the reverse thrust.
MAINTENANCE PROCEDURE Refer to AMM 78-30-00-040-040
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.78.05 EXHAUST
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
78 EXHAUST 78-30
Thrust Reversers
78-30-02
Thrust Reverser Inhibition Relay sw
78-30-02A
C
4
2
Two may be inoperative provided that the associated thrust reverser is considered inoperative. Refer to Item 78-30-01 Thrust Reverser
78-30-03 78-30-03A
Thrust Reverser Shutoff Valve C
2
0
One or both may be inoperative in the open position.
*
*
*
A320/321 MEL/CDL
01.78.06 EXHAUST 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.79.01 OIL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
79 OIL 79-07
Indications on the ENGINE SD page
79-07-01
CLOG Indication on the ENGINE SD page
79-07-01A 79-07-02
C
2
1
One may be inoperative.
Oil Pressure Indication and Advisory on the ENGINE SD page
Note: Simultaneous illumination of the BLUE ELEC PUMP pb-sw FAULT light and the ENG 1(2)PUMP pb-sw FAULT light with engines off may be due to a failed engine oil low pressure switch. In this case, the ENG 1(2) OIL LO PR alert is inoperative. Refer to Item 79-09-01 ENG 1(2) OIL LO PR Alert
79-07-02A
Associated thrust reverser checked operative
C
2
1
(M)
One may be inoperative provided that: 1) The associated ENG 1(2) OIL LO PR alert is operative, and 2) The associated oil quantity indication is operative on the ENGINE SD page, and 3) The associated thrust reverser is checked operative. MAINTENANCE PROCEDURE Refer to AMM task
79-07-02B
Associated thrust reverser considered inoperative
C
2
1
One may be inoperative provided that: 1) The associated ENG 1(2) OIL LO PR alert is operative, and 2) The associated oil quantity indication is operative on the ENGINE SD page, and 3) The associated inoperative.
thrust
reverser
Refer to Item 78-30-01 Thrust Reverser
is
considered
A320/321 MEL/CDL
01.79.02 OIL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
79 OIL 79-07
Indications on the ENGINE SD page (cont’d)
79-07-03
Oil Quantity Indication on the ENGINE SD page
79-07-03A
C
2
1
(M)
One may be inoperative provided that the associated oil quantity is checked before each flight. MAINTENANCE PROCEDURE Refer to AMM 79-31-00-040-042
79-07-04
Oil Temperature Indication on the ENGINE SD page
79-07-04A
79-09
2
2
2
0
Must be operative.
ECAM Alerts
79-09-01 79-09-01A
ENG 1(2) OIL LO PR Alert C
(O)
One or both may be displayed. OPERATING PROCEDURES AFTER ENGINE START · If both engines are affected: RCDR GND CTL pb-sw . . . . . . . . . . . . . . . . . .CHECK ON
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.79.03 OIL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
79 OIL 79-09
ECAM Alerts
79-09-02
79-09-02B
ENG 1(2) OIL FILTER CLOG Alert Inspection of the visual indicator (popout) of the electrical master chip detector
C
2
1
(M)
One may be displayed provided that: 1) The associated filter is replaced every day, and 2) The visual indicator (pop-out) of the electrical master chip detector is checked operative before the first MMEL dispatch, and 3) The visual indicator (pop-out) of the electrical master chip detector is inspected when the filter is replaced and does not reveal the presence of chips. MAINTENANCE PROCEDURE Refer to AMM 79-35-00-040-042
79-09-02C
Inspection of the electrical master chip detector
C
2
1
(M)
One may be displayed provided that: 1) The associated filter is replaced every day, and 2) The electrical master chip detector is inspected when the filter is replaced and does not reveal the presence of chips. MAINTENANCE PROCEDURE Refer to AMM 79-35-00-040-044
A320/321 MEL/CDL
01.79.04 OIL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
79 OIL 79-20
Distribution
79-20-02
EMCD Visual PopOut Indicator
79-20-02A 79-40
C
2
0
One or both may be inoperative.
IDG Oil Cooling System
79-40-01 79-40-01A
Fuel Return Valve Refer to Item 73-10-01 Fuel Return Valve
*
*
*
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
01.80.01 STARTING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
80 STARTING 80-01
ENG MAN START Overhead Panel
80-01-31
ENG MAN START pb-sw
80-01-31A 80-07
Indication on the ENGINE SD page
80-07-01
Start Valve Position Indication on the ENGINE SD page
80-07-01A
C
2
0
C
2
1
One or both may be inoperative.
(M)
One may be inoperative provided that the start valve is checked closed after the engine start. MAINTENANCE PROCEDURE Refer to AMM 80-11-00-040-044
80-11
Pneumatic Starter and Valve System
80-11-01
Start Valve
80-11-01A
C
2
1
(O)(M) One may be inoperative provided that the start valve is manually closed after the start of the affected engine. OPERATING PROCEDURES BEFORE ENGINE START Refer to FCOM/PRO-SUP-70 START VALVE MANUAL OPERATION. MAINTENANCE PROCEDURE Refer to AMM 80-11-00-040-045
A320/321 MEL/CDL
01.80.02 STARTING 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
80 STARTING 80-12
ENG MASTER Panel on the Center Pedestal
80-12-01
80-12-01A
FAULT light on the ENG MASTER Panel C
2
0
One or both may be inoperative.
*
*
*
A320/321 MEL/CDL
12 FEB 12 CDL
02.00.01 TABLE OF CONTENTS
ITEM
PAGE CDL INTRODUCTION
-----
CDL INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.01.01 LIMITATIONS DISPATCH FUEL PENALTY WEIGHT REDUCTIONS SPEED CALCULATION AND RESTRICTIONS ENROUTE DIVERSION SPEED EFFECTS GENERAL LOCATION PICTURES & PERFORMANCE
ATA 21 - AIR CONDITIONING 21-01 21-03
Ram air inlet flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.21.01 Ram air inle leading Edge . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 01.21.02 ATA 23 - COMMUNICATIONS
23-01
Static Discharger . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.23.01 ATA 27 - FLIGHT CONTROL
27-01 27-02 27-03 27-05 27-06 27-07 27-08 27-09 27-10 27-11 27-12 27-13 27-14 27-15 27-16 27-17
Flap Track Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.01 Flap Track Fairing 1A Extension . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.03 Slat Track Closing Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.04 Access Panel For Bearings At Elevator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.05 Flat Track Fairing Rear Top Cover And Tail Cone . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.06 Rubber Seal Under Slat . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.07 Seal Between Inboard And Outboard Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.08 Inboard Aileron Edge To Wing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.10 Slat End Seal And Weather Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.11 Slat Track Filler Block . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.12 Slat Track Sealing Packer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.13 Inter-flap Cushion Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.14 Flap Track Movable Fairing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.15 Flap Track Fixed Fairing Seal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.16 Flap Track Movable Fairing Pivot Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.17 Flap Tab Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.27.18 ATA 28- FUEL
28-01 28-02
Refuel /defuel coupling CAP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.01 Refuel Panel Door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.28.02
02.00.02 TABLE OF CONTENTS
A320/321 MEL/CDL
ITEM
12 FEB 12 CDL PAGE
ATA 30 - ICE AND RAIN PROTECTION
30-01
Icing indicator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.30.01 ATA 32 - LANDING GEAR
32-03 32-04
Nose wheel hubcap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.01 Nose fitting towing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.32.02 ATA 33 - LIGHTS
33-01 33-02 33-03 33-04 33-05 33-07 33-08 33-09
Wing / Engine / Scan Light Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.01 Taxi Light lamp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.02 Rear navigation light lens . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.03 Upper and lower anti-collision (Beacon) light Cover . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.04 Logo light lens (Cover) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.06 Landing light lens . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.07 Turn OFF light lamp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.08 Takeoff light lamp . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.33.09 ATA 49 - APU
49-01
APU overpressure release door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.49.01 ATA 51- STRUCTURE
51-01 51-02 51-03 51-04
Random conductive Strip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.01 Passenger door Scuff Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.02 Bulk cargo door Scuff Plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.03 Fairing AFT Safety Stay Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.51.04
A320/321 12 FEB 12 CDL
MEL/CDL
ITEM
02.00.03 TABLE OF CONTENTS PAGE
ATA 52 - DOORS 52-01 52-02 52-03 52-04 52-05 52-06 52-07 52-08 52-09 52-10 52-11 52-12 52-13 52-14 52-15 52-16 52-18 52-19 52-20 52-21 52-22 52-23
Toilet sem rvicing door and drainage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.01 Access door to hydraulic ground connectors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.03 access door to potable water filling and drainage . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.05 access door to opening control of landing gear doors on ground . . . . . . . . . . . . . . . 02.52.07 access door to air conditioning ground supply . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.09 Forward jacking point access door. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.11 External power ground connection access door ASSY . . . . . . . . . . . . . . . . . . . . . . . 02.52.13 Access door of cargo opening system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.14 Nose landing gear main . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.15 Nose landing gear aft doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.17 Nose landing gear leg doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.19 Main landing gear door (732, 742) (Flight with gear up) . . . . . . . . . . . . . . . . . . . . . . 02.52.21 Main landing gear door (733, 743) (Flight with gear up) . . . . . . . . . . . . . . . . . . . . . . 02.52.23 Main landing gear door (732, 742) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.25 Main landing gear door (733, 743) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.27 Main landing gear door (734, 744) (Flight with gear down) . . . . . . . . . . . . . . . . . . . . 02.52.29 Main landing gear door: Seal on secondary hinged fairing . . . . . . . . . . . . . . . . . . . . 02.52.31 Pax door upper cover plate . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.32 Access door to HP air ground connector . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.33 Blue hydraulic access door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.35 Forward cargo door access cover panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.36 Aft cargo door access cover panel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.52.37 ATA 53 - FUSELAGE
53-01 53-03
Belly Fairing Vent Louver Vanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.01 Root Fillet Fairing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.53.03 ATA 54 - NACELLES / PYLON
54-01 54-03 54-04 54-05 54-06
Nacelle Strakes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.01 Pylon Pressure relief door . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.03 Pylon Access Doors . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.05 Pylon Fairing Seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.06 Aerodynamic Seals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.54.07
A320/321 MEL/CDL
02.00.04 TABLE OF CONTENTS
12 FEB 12 CDL
ATA 57 - WINGS 57-01 57-02 57-03
Wing tip fences. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.01 Belly Fairing Sliding Panels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.03 Outboard Flaps Rubbing Strip . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.57.04 ATA 71 - POWER PLANT
71-01 71-09
Frangible Drain Mast . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.01 Fan Cowl Hold Open Rod . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.71.02 ATA 78 - EXHAUST
78-09
Thrust reverser 11 and 1 O,clock Struts. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02.78.01
*
*
*
A320/321 12 FEB 12 CDL
MEL/CDL
02.01.01 CDL INTRODUCTION
CDL Introduction
Weight Reductions
The Configuration Deviation List presented in this manual is a reproduction of the FAA-approved CDL in the Aircraft Flight Manual (AFM). The numbering and designation of system in this CDL is based on ATA specification 100. The parts within each systems are identified by functional description, and when necessary by part number(s).
The MEL weight reductions must be applied to the maximum performance limited weights, as follows: 1. Takeoff Weight penalty is applied to the most restrictive of the Zero Wind weight or Climb Limit weight.
CDL General Limitations
2. Enroute -
The associated limitations for each applied CDL item must be listed on placard(s) affixed in the cockpit in clear view to both pilots. The pilot in command shall be notified whenever a CDL restriction(s) exists by listing the CDL number in the flight dispatch release.
Weight penalty is applied to cruise and one engine inoperative Altitude Capability limited weights.
3. Landing -
The maintenance log book briefing card must include a data reflecting all imposed CDL(s). An appropriate inspection notation covering the missing part(s) must be noted on aircraft maintenance logbook before each flight.
Weight penalty is applied to the most restrictive of tailored landing charts, field length or landing climb limited weight.
Speed Calculation, and Restrictions
If an additional part is lost in flight, the aircraft may not depart the airport at which it landed following this event until it again complies with the appropriate CDL limitation. This, of course, does not preclude the issuance of a maintenance ferry authorization to allow the aircraft to be flown to a point where the necessary repairs or replacements can be made. No more than one part for any one system in this CDL may be missing, unless specifically designated combinations are indicated. The performance penalties are cumulative. Where performance penalties are listed as “NEGLIGIBLE”, no more than three negligible items may be missing without applying weight penalty. For each missing item in excess of three, the maximum performance limited weight for takeoff, enroute, and landing must be reduced by 50 kg. Where performance penalties are not listed, any accumulative number of sub-systems may be missing without further penalty.
When takeoff weight penalty is imposed, determine takeoff speed with reference to the sum of actual aircraft gross weight plus the imposed takeoff weight penalty. When landing weight penalty is imposed, the Vref, and the minimum maneuvering speeds must be determined with reference to the actual aircraft gross weight, plus the imposed landing weight penalty. Operation with those missing item(s) requiring a reduction of VMO/MMO is only permitted when the appropriate alternate VMO set prior to flight.
Performance Performance determination method. There are two approved ways of determining the performance impact on CDL items missing: - Using CDL chapter of the Airplane Flight Manual, or - Using AFM_OCTO software.
All CDL items must be relayed to the controlling dispatch center prior to departure.
If no performance data are available in OCTO_AFM for a given item listed in this CDL chapter, the penalties published in this CDL chapter must be used.
Dispatch Fuel Penalty
These takeoff, en-route and landing penalties apply to most limiting corresponding weight.
The performance increase in the fuel must be applied to the minimum dispatch fuel requirement. Minimum dispatch fuel required is the sum of trip fuel, alternate fuel and reserve fuel.
Takeoff and approach climb performance limiting weights are reduced by 50 kg ( Cont'd on next page )
A320/321 MEL/CDL
02.01.02 CDL INTRODUCTION (Cont'd)
One engine inoperative net ceiling is reduced by 60 ft (i.e. Corresponding to 60 kg decrease of en-route performance limiting weight.
CAUTION The most limiting performance between the one computed with items missing and the one computed without item missing must be used.
*
*
*
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.21.01 AIR CONDITIONING
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-01
RAM AIR INLET FLAP
2
0
All may be missing. Note: System performance in heating mode will be decreased. Performance: The following performance penalties are applicable per missing flap: -
Takeoff and approach climb performance limiting weights are reduced by 190 kg
-
En route performance limiting weight is reduced by 216 kg
-
Fuel consumption is increased by 0.53 %.
A320/321 MEL/CDL
02.21.02 AIR CONDITIONING 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
21 AIR CONDITIONING 21-03
RAM AIR INLET LEADING EDGE
2
1
One may be missing provided the associated pack is turned off (Refer to MEL/MI-21-52 Air Conditioning Pack).
*
*
*
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
02.23.01 COMMUNICATION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATION 23-01
STATIC DISCHARGER
39 32
20 % of static dischargers may be missing or inoperative on each the following areas: -
RH wing
-
LH wing
-
Vertical stabilizer (including rudder)
-
RH horizontal stabilizer (including elevator)
-
LH horizontal stabilizer (including elevator). Note: i.
If a static discharger is missing or inoperative on a flap track fairing, it is recommended to replace it before flight.
ii. When combined with the case of dispatch with a wing tip fence missing, 20 % of the remaining static dischargers of the affected wing are allowed to be inoperative or missing (Refer to 57-01 Wing Tip Fence). (Cont’d on next page)
A320/321 MEL/CDL
02.23.02 COMMUNICATION 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
23 COMMUNICATION 23-01
STATIC DISCHARGER
*
*
*
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.27.01 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-01
FLAP TRACK FAIRING
6
7
(M)
One fairing may be partly or completely missing.
Note: i.
When the forward part of the fairing is missing, the aft part must be removed.
ii. When the aft part of the fairing is missing, the forward part may remain installed. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 1 430 kg
-
En route performance limiting weight is reduced by 1 575 kg
-
Fuel consumption is increased by 2.81 %.
MAINTENANCE PROCEDURES Refer to AMM 57-55-00-040-001 (Cont’d on next page)
A320/321 MEL/CDL
02.27.02 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
27 FLIGHT CONTROL 27-01
FLAP TRACK FAIRING (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1.
2.
SYSTEM & SEQUENCE OF ITEMS
02.27.03 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-02
FLAP TRACK FAIRING 1A EXTENSION
2
0
All may be missing. Performance: The following performance penalties are applicable per missing extension: -
Takeoff and approach climb performance limiting weights are reduced by 120 kg
-
En route performance limiting weight is reduced by 131 kg
-
Fuel consumption is increased by 0.26 %.
A320/321 MEL/CDL
02.27.04 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-03
SLAT TRACK CLOSING PLATE
24
22
Two may be missing.
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-05
ACCESS PANEL FOR BEARINGS AT ELEVATOR
8
6
Two may be missing.
02.27.05 FLIGHT CONTROL
A320/321 MEL/CDL
02.27.06 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-06
FLAP TRACK FAIRING REAR TOP COVER AND TAIL CONE
6
4
(M)
Both may be missing on two flap track fairings. Note: i.
When the tail cone is missing, the rear top cover may remain installed.
ii. When the rear top cover is missing, the associated tail cone must be removed. MAINTENANCE PROCEDURES Refer to AMM 57-55-00-040-002
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-07
RUBBER SEAL UNDER SLAT
10
0
(M)
1 m per slat may be missing.
MAINTENANCE PROCEDURES Refer to AMM 57-40-00-040-001
02.27.07 FLIGHT CONTROL
A320/321 MEL/CDL
02.27.08 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-08
SEAL BETWEEN INBOARD AND OUTBOARD FLAP
6
3
Three may be missing. Note: For dispatch with inter-flap cushion seal missing, Refer to 27-13 Inter-flap Cushion Seal. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 63 kg per missing seal
-
En route performance limiting weight is reduced by 72 kg (159 lb) per missing seal
-
If two or more seals are missing, fuel consumption is increased by 0.16 % per missing seal. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
27 FLIGHT CONTROL 27-08
SEAL BETWEEN INBOARD AND OUTBOARD FLAP (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
02.27.09 FLIGHT CONTROL
A320/321 MEL/CDL
02.27.10 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-09
INBOARD AILERON EDGE TO WING SEAL
4
2
One seal per aileron may be partially or completely missing provided that any loose or flapping seal material is cut off.
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
02.27.11 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-10
SLAT END SEAL AND WEATHER SEAL
12 10
One seal per wing may be partially or completely missing provided any loose or flapping seal material is cut off.
A320/321 MEL/CDL
02.27.12 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-11
SLAT TRACK FILLER BLOCK
6
0
All may be missing.
Note: May be combined with MCDL item 2712 (Refer to 27-12 Slat Track Sealing Packer).
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.27.13 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-12
SLAT TRACK SEALING PACKER
4
0
All may be missing.
Note: May be combined with MCDL item 2711 (Refer to 27-11 Slat Track Filler Block).
A320/321 MEL/CDL
02.27.14 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-13
INTER-FLAP CUSHION SEAL
4
2
One cushion seal may be missing per wing.
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.27.15 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-14
FLAP TRACK MOVEABLE FAIRING SEAL
12
6
(M)
50 % of the seal length may be missing on each side of the flap track fairing for 100 flight hours provided that a visual inspection is performed before each flight to ensure there is no flapping seal on the aircraft. Note: May be combined with MCDL item 2715 (Refer to 27-15 Flap Track Fixed Fairing Seal). MAINTENANCE PROCEDURES Refer to AMM 57-55-00-040-004
A320/321 MEL/CDL
02.27.16 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-15
FLAP TRACK FIXED FAIRING SEAL
18
0
(M)
All may be missing provided the hole is covered with high speed tape. Note: May be combined with MCDL item 2714 (Refer to 27-14 Flap Track Moveable Fairing Seal). MAINTENANCE PROCEDURES Refer to AMM 57-55-00-040-004
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.27.17 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-16
FLAP TRACK MOVEABLE FAIRING PIVOT COVER
12
0
(M)
All may be missing provided the hole is covered with high speed tape.
Note: A visual inspection must be performed daily to ensure that tape is still in position and in good condition.
A320/321 MEL/CDL
02.27.18 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-17
FLAP TAB FAIRING
10
9
One fairing may be partly or completely missing. Note: i.
When the forward part of the fairing is missing, the aft part must be removed.
ii. When the aft part of the fairing is missing, the forward part may remain installed. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 143 kg
-
En route performance limiting weight is reduced by 158 kg
-
Fuel consumption is increased by 0.32 %. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
02.27.19 FLIGHT CONTROL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
27 FLIGHT CONTROL 27-17
FLAP TAB FAIRING (Cont’d)
*
*
*
A320/321 MEL/CDL
02.27.20 FLIGHT CONTROL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.28.01 FUEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-01
REFUEL/DEFUEL COUPLING CAP 101 QM OR 41 QM
2
0
(M)
All may be missing provided seal integrity of coupling is positively confirmed (i.e. no fuel leak reported). Note: i.
If the coupling or O-ring is damaged and the cap cannot be fitted, dispatch is permitted in accordance with this CDL item provided the cap is removed and coupling integrity is verified.
ii. If only the lanyard is missing, the removal of the cap is not necessary. MAINTENANCE PROCEDURES Refer to AMM 28-25-00-040-003
*
*
*
A320/321 MEL/CDL
02.28.02 FUEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
28 FUEL 28-02
REFUEL PANEL DOOR
1
0
(M)
Belly fairing mounted refuel panel door 192 MB may be missing. Note: If belly fairing mounted refuel panel door 192 MB is not installed, underwing mounted refuel panel doors (622KB, 522KB) must not be missing MAINTENANCE PROCEDURES Refer to AMM 52-42-00-040-001
*
*
*
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.30.01 ICE AND RAIN PROTECTION
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
30 ICE AND RAIN PROTECTION 30-01
ICING INDICATOR
1
0
May be missing. Procedures: -
*
*
If icing conditions expected: For icing conditions definition, Refer to LIM-GEN Icing Conditions Definition. Turn on engine and wing anti-ice.
*
A320/321 MEL/CDL
02.30.02 ICE AND RAIN PROTECTION 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
32 LANDING GEAR 32-03 Nose wheel hubcap
2
1
(M)
One may be missing. MAINTENANCE PROCEDURES Refer to AMM 32-41-00-040-001
02.32.01 LANDING GEAR
A320/321 MEL/CDL
02.32.02 LANDING GEAR 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
(M)
May be missing
32 LANDING GEAR 32-04
Nose Fitting Towing
1
0
MAINTENANCE PROCEDURES Refer to AMM 32-21-00-040-001
*
*
*
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.33.01 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-01
WING/ENGINE SCAN LIGHT COVER 3LX, 4LX
2
1
(M)
One may be missing provided the hole is covered with high speed tape.
Note: If non transparent high speed tape is used, the affected light must be deactivated (Refer to MEL/MI-33-40 Wing Scan light).
A320/321 MEL/CDL
02.33.02 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-02
TAXI LIGHT LAMP 8LR
1
0
(M)
May be missing provided the hole is covered with high speed tape and the affected light is deactivated (Refer to MEL/MI-33-40 Taxi and Takeoff light). MAINTENANCE PROCEDURES Refer to AMM 33-46-00-040-001
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.33.03 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-03
REAR NAVIGATION LIGHT LENS 15LA
1
0
(M)
May be missing for 5 flight cycles provided visual inspection is performed before each flight to check that there is no structural buckling. MAINTENANCE PROCEDURES Refer to AMM 33-41-00-040-002
A320/321 MEL/CDL
02.33.04 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-04
UPPER 7LV AND LOWER 6LV ANTICOLLISION (BEACON) LIGHT COVER
2
0
(M)
All may be missing provided the lamp is covered with high speed tape and affected light is deactivated (Refer to MMEL/MI-33-40 Beacon light). Performance: If upper and lower light covers are missing, the following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 80 kg
-
En route performance limiting weight is reduced by 90 kg
-
Fuel consumption is increased by 0.22 %.
MAINTENANCE PROCEDURES Refer to AMM 33-48-00-040-001 (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
33 LIGHTS 33-04
UPPER 7LV AND LOWER 6LV ANTICOLLISION (BEACON) LIGHT COVER (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
02.33.05 LIGHTS
A320/321 MEL/CDL
02.33.06 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-05
LOGO LIGHT LENS (COVER) 3LY, 4LY
2
0
(M)
All may be missing provided the hole is covered with high speed tape. Note: If non transparent high speed tape is used, the affected light must be deactivated. (Refer to MEL/MI-33-40 Logo light). MAINTENANCE PROCEDURES Refer to AMM 33-47-00-040-001
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.33.07 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-07
LANDING LIGHT LENS 7LB, 8LB
2
1
(M)
One may be missing provided the associated light is retracted and deactivated and the hole is covered with high speed tape (Refer to MEL/MI-33-40 Landing light). MAINTENANCE PROCEDURES Refer to AMM 33-42-00-040-001
A320/321 MEL/CDL
02.33.08 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-08
TURN OFF LIGHT LAMP 3LC1, 3LC2
2
0
(M)
All may be missing provided the hole is covered with high speed tape and the affected light is deactivated (Refer to MEL/MI-33-40 Runway Turnoff light). MAINTENANCE PROCEDURES Refer to AMM 33-43-00-040-002
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.33.09 LIGHTS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
33 LIGHTS 33-09
TAKEOFF LIGHT LAMP 7LR
1
0
(M)
May be missing provided the hole is covered with high speed tape and the affected light is deactivated (Refer to MEL/MI-33-40 Taxi and Takeoff light). MAINTENANCE PROCEDURES Refer to AMM 33-46-00-040-002
*
*
*
A320/321 MEL/CDL
02.33.10 LIGHTS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.49.01 APU
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
49 APU 49-01
APU OVERPRESSURE RELEASE DOOR
1
0
May be missing provided APU is not used in flight and on ground.
Limitations: Flights for which APU is mandatory are not allowed.
*
*
*
A320/321 MEL/CDL
02.49.02 APU 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
51 STRUCTURE 51-01
RADOME CONDUCTIVE STRIP
8
7
One may be missing.
02.51.01 STRUCTURE
A320/321 MEL/CDL
02.51.02 STRUCTURE 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
51 STRUCTURE 51-02
PASSENGER DOOR SCUFF PLATE
4 8
0 0
All may be missing.
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
51 STRUCTURE 51-03
BULK CARGO DOOR SCUFF PLATE
1
0
May be missing.
02.51.03 STRUCTURE
A320/321 MEL/CDL
02.51.04 STRUCTURE 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
51 STRUCTURE 51-04
FAIRING AFT SAFETY STAY POINT 311 AL
1
0
May be missing.
*
*
*
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.01 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
(M)
May be missing.
52 DOORS 52-01
TOILET SERVICING AND DRAINAGE DOOR 172 AR
1
0
Note: i.
Toilet system ground.
is
inoperative
on
ii. May be combined with MCDL items: 52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB 198 CB) 52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage) 52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB) 52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB) 52-06 (Refer to 52-06 Forward Jacking Point Access Door) 52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB). Performance: The following performance penalties are applicable: -
Takeoff and approach performance limiting weights are reduced by 63 kg En-route performance limiting weight is reduced by 72 kg. (Cont’d on next page)
A320/321 MEL/CDL
02.52.02 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-01
TOILET SERVICING AND DRAINAGE DOOR 172 AR (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.03 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-02
ACCESS DOOR TO HYDRAULIC GROUND CONNECTORS 197 CB - 197 EB - 198 CB
3
2
One may be missing. Note: May be combined with MCDL items: -
52-01 (Refer to 52-01 Toilet Servicing and Drainage Door )
-
52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
-
52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB)
-
52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
-
52-06 (Refer to 52-06 Forward Jacking Point Access Door)
-
52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
Performance: The following performance penalties are applicable: -
Takeoff and approach performance limiting weights are reduced by 63 kg
-
En-route performance limiting weight is reduced by 72 kg. (Cont’d on next page)
A320/321 MEL/CDL
02.52.04 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-02
ACCESS DOOR TO HYDRAULIC GROUND CONNECTORS 197 CB - 197 EB - 198 CB (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.05 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-3
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE 133 AL 171 AL - 192 NB
3
2
One may be missing.
Note: May be combined with MCDL items: -
52-01 (Refer to 52-01 Toilet Servicing and Drainage Door )
-
52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB)
-
52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB)
-
52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
-
52-06 (Refer to 52-06 Forward Jacking Point Access Door)
-
52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB). (Cont’d on next page)
A320/321 MEL/CDL
02.52.06 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-03
ACCESS DOOR TO POTABLE WATER FILLING AND DRAINAGE 133 AL 171 AL - 192 NB (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.07 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-04
ACCESS DOOR TO OPENING CONTROL OF LANDING GEAR DOORS ON GROUND 195 BB 196 BB
2
1
One may be missing for five flight cycles. Note: May be combined with MCDL items: -
52-01 (Refer to 52-01 Toilet Servicing and Drainage Door )
-
52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB)
-
52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
-
52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
-
52-06 (Refer to 52-06 Forward Jacking Point Access Door)
-
52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB).
Limitations: Flight in forecasted thunderstorm condition is not allowed. Performance: The following performance penalties are applicable: -
Takeoff and approach performance limiting weights are reduced by 63 kg
-
En-route performance limiting weight is reduced by 72 kg . (Cont’d on next page)
A320/321 MEL/CDL
02.52.08 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-04
ACCESS DOOR TO OPENING CONTROL OF LANDING GEAR DOORS ON GROUND 195 BB 196 BB (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.09 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-05
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY 191 CB
1
0
May be missing. Note: May be combined with MCDL items: -
52-01 (Refer to 52-01 Toilet Servicing and Drainage Door )
-
52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB)
-
52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
-
52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB)
-
52-06 (Refer to 52-06 Forward Jacking Point Access Door)
-
52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB). (Cont’d on next page)
A320/321 MEL/CDL
02.52.10 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-05
ACCESS DOOR TO AIR CONDITIONING GROUND SUPPLY 191 CB (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.11 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-06
FORWARD JACKING POINT ACCESS DOOR
1
0
May be missing. Note: May be combined with MCDL items: -
52-01 (Refer to 52-01 Toilet Servicing and Drainage Door )
-
52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB)
-
52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
-
52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB)
-
52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
-
52-20 (Refer to 52-20 Access Door to HP Air Ground Connector 191 DB). (Cont’d on next page)
A320/321 MEL/CDL
02.52.12 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-06
FORWARD JACKING POINT ACCESS DOOR (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
NUMBER INSTALLED 3.
ITEM
02.52.13 DOORS
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-07
EXTERNAL POWER GROUND CONNECTION ACCESS DOOR ASSY 121 AL
1
0
(M)
May be missing for five flight cycles provided the hole is covered with high speed tape and that a visual inspection is performed before each flight. Limitations: Flight in forecasted thunderstorm condition is not allowed. MAINTENANCE PROCEDURES Refer to AMM 52-42-00-040-003
A320/321 MEL/CDL
02.52.14 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-08
ACCESS DOOR OF CARGO OPENING SYSTEM 134 AR 154 AR
2
0
All may be missing. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 95 kg per missing access door
-
En-route performance limiting weight is reduced by 105 kg (232 lb) per missing access door
-
Fuel consumption is increased by 0.21 % per missing access door.
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.15 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-09
NOSE LANDING GEAR MAIN DOOR (713, 714)
2
0
(M)
May be missing provided both main doors (713, 714) are removed and both aft doors (715, 716) (Refer to 52-10 Nose Landing Gear Aft Door (715, 716)) are removed. Note: May be combined with MCDL item 5211 (Refer to 52-11 Nose Landing Gear Leg Door (712)) Limitations: Passengers transportation is not allowed. Flight with landing gear down is required. Refer to APP-LGDN-GEN General Maximum speed: 220 kt IAS/ M 0.5 Performance: Note: Reference performance for penalties computations are performance with landing gear down. The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 1 109 kg
-
En-route performance limiting weight is reduced by 1 000 kg
-
Fuel consumption is increased by 2 %.
MAINTENANCE PROCEDURES Refer to AMM 32-22-00-040-001 (Cont’d on next page)
A320/321 MEL/CDL
02.52.16 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-09
NOSE LANDING GEAR MAIN DOOR (713, 714) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.17 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-10
NOSE LANDING GEAR AFT DOOR (715, 716)
2
0
(M)
All may be missing. Note: May be combined with MCDL item 5211 (Refer to 52-11 Nose Landing Gear Leg Door (712)) Limitations: Flight with landing gear down is required. Refer to APP-LGDN-GEN General Performance: Note: Reference performance for penalties computations are performance with landing gear down. The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 79 kg
-
En-route performance limiting weight is reduced by 100 kg
-
Fuel consumption is increased by 0.25 %.
When combined with MCDL item 52-09 (Refer to 52-09 Nose Landing Gear Main Door (713, 714)), the performance penalties published in 52-09 are applicable. MAINTENANCE PROCEDURES Refer to AMM 32-22-00-040-002 (Cont’d on next page)
A320/321 MEL/CDL
02.52.18 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-10
NOSE LANDING GEAR AFT DOOR (715, 716) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.19 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
(M)
May be missing.
52 DOORS 52-11
NOSE LANDING GEAR LEG DOOR (712)
1
0
Note: May be combined with MCDL items 5209 (Refer to 52-09 Nose Landing Gear Main Door (713, 714)) and 52-10 (Refer to 52-10 Nose Landing Gear Aft Door (715, 716)). Limitations: Flight with landing gear down is required. Refer to APP-LGDN-GEN General MAINTENANCE PROCEDURES Refer to AMM 32-22-00-040-003 (Cont’d on next page)
A320/321 MEL/CDL
02.52.20 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-11
NOSE LANDING GEAR LEG DOOR (712)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.21 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-12
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR UP)
2
1
(M)
One may be missing. Limitations: Passengers transportation is not allowed. Flight in forecasted icing conditions is not allowed. Performance: The following performance penalties are applicable: -
] Takeoff and approach climb performance limiting weights are reduced by 475 kg
-
] En-route performance limiting weight is reduced by 525 kg (1 158 lb)
-
] Fuel consumption is increased by 0.96 %.
MAINTENANCE PROCEDURES Refer to AMM 32-12-00-040-005 (Cont’d on next page)
A320/321 MEL/CDL
02.52.22 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-12
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR UP) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.23 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-13
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR UP)
2
1
(M)
One may be missing. Limitations: Passengers transportation is not allowed. Flight in forecasted icing conditions is not allowed. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 111 kg
-
En-route performance limiting weight is reduced by 126 kg
-
Fuel consumption is increased by 0.28 %.
MAINTENANCE PROCEDURES Refer to AMM 32-12-00-040-005 (Cont’d on next page)
A320/321 MEL/CDL
02.52.24 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-13
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR UP) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.25 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-14
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR DOWN)
2
1
(M)
One may be missing. Limitations: Flight with landing gear down is required. Refer to APP-LGDN-GEN General Performance: Note: Reference performance for penalties computations are performance with landing gear down. The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 475 kg
-
En-route performance limiting weight is reduced by 450 kg
-
Fuel consumption is increased by 1.00 %. (Cont’d on next page)
A320/321 MEL/CDL
02.52.26 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-14
MAIN LANDING GEAR DOOR (732, 742) (FLIGHT WITH GEAR DOWN) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.27 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-15
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR DOWN)
2
1
(M)
One may be missing. Limitations: Flight with landing gear down is required. Refer to APP-LGDN-GEN General Performance: Note: Reference performance for penalties computations are performance with landing gear down. The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 111 kg
-
En-route performance limiting weight is reduced by 200 kg
-
Fuel consumption is increased by 0.30 %. (Cont’d on next page)
A320/321 MEL/CDL
02.52.28 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-15
MAIN LANDING GEAR DOOR (733, 743) (FLIGHT WITH GEAR DOWN) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.29 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-16
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH GEAR DOWN)
2
1
(M)
One may be missing. Limitations: Flight with landing gear down is required. Refer to APP-LGDN-GEN General Performance: Note: Reference performance for penalties computations are performance with landing gear down. The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 752 kg
-
En-route performance limiting weight is reduced by 700 kg
-
Fuel consumption is increased by 1.50 %. (Cont’d on next page)
A320/321 MEL/CDL
02.52.30 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-16
MAIN LANDING GEAR DOOR (734, 744) (FLIGHT WITH GEAR DOWN) (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.31 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-18
MAIN LANDING GEAR DOOR : SEAL ON SECONDARY HINGED FAIRING
6
0
All may be missing. Performance: If three or more seals are missing, the following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 24 kg per missing seal
-
En-route performance limiting weight is reduced by 27 kg per missing seal
-
Fuel consumption is increased by 0.07 % per missing seal.
A320/321 MEL/CDL
02.52.32 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-19
PAX DOOR UPPER COVER PLATE
8
0
All may be missing. Note: The affected door must be considered as inoperative (Refer to MEL/MI-52-10 Cabin Passenger Door). Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 79 kg per missing plate
-
En-route performance limiting weight is reduced by 88 kg (195 lb) per missing plate
-
If 2 or more plates are missing, fuel consumption is increased by 0.18 % per missing plate.
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.33 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-20
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB
1
0
(M)
May be missing for ten flight cycles. Note: May be combined with MCDL items: -
52-01 (Refer to 52-01 Toilet Servicing and Drainage Door )
-
52-02 (Refer to 52-02 Access Door to Hydraulic Ground Connectors 197 CB - 197 EB - 198 CB)
-
52-03 (Refer to 52-03 Access Door to Potable Water Filling and Drainage)
-
52-04 (Refer to 52-04 Access Door to Opening Control of Landing Gear Doors on Ground 195 BB - 196 BB)
-
52-05 (Refer to 52-05 Access Door to Air Conditioning Ground Supply 191 CB)
-
52-06 (Refer to 52-06 Forward Jacking Point Access Door).
MAINTENANCE PROCEDURES Refer to AMM 47-20-00-040-002 (Cont’d on next page)
A320/321 MEL/CDL
02.52.34 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
52 DOORS 52-20
ACCESS DOOR TO HP AIR GROUND CONNECTOR 191 DB (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
(M)
May be missing.
52 DOORS 52-21
BLUE HYDRAULIC ACCESS DOOR 197 FB
1
0
MAINTENANCE PROCEDURES Refer to AMM 52-41-00-040-001
02.52.35 DOORS
A320/321 MEL/CDL
02.52.36 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-22
FORWARD CARGO DOOR ACCESS COVER PANEL 825 AR
1
0
(M)
May be missing provided all latching hooks are checked latched and locked before each flight. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 234 kg
-
En-route performance limiting weight is reduced by 266 kg
-
Fuel consumption is increased by 0.64 %.
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.52.37 DOORS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
52 DOORS 52-23
AFT CARGO DOOR ACCESS COVER PANEL 826 AR
1
0
(M)
May be missing provided all latching hooks are checked latched and locked before each flight. Performance: The following performance penalties are applicable:
*
-
Takeoff and approach climb performance limiting weights are reduced by 190 kg
-
En-route performance limiting weight is reduced by 216 kg
-
Fuel consumption is increased by 0.53 %.
*
*
A320/321 MEL/CDL
02.52.38 DOORS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
02.53.01 FUSELAGE
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
53 FUSELAGE 53-01
BELLY FAIRING VENT LOUVER VANE
24 18 (M)
Three may be missing per vent louver. Note: Vane with a crack length higher than 50% must be removed before next flight.
A320/321 MEL/CDL
02.53.02 FUSELAGE 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
53 FUSELAGE 53-03
ROOT FILLET FAIRING
2
0
(M)
All may be missing. Note: Must not be combined with MCDL item 54-01 (Refer to 54-01 Nacelle Strake) or MCDL item 54-03 (Refer to 54-03 Pylon Pressure Relief Door 413(423) BL 414(424) BR). Performance: The following performance penalty is applicable: -
Takeoff performance limiting weight is reduced by 900 kg. Note: The above performance penalty is not applicable if the flight crew can check V2 greater than 1.15 VS1G. (Cont’d on next page)
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
02.53.03 FUSELAGE
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
53 FUSELAGE 53-03
ROOT FILLET FAIRING (Cont’d)
*
*
*
A320/321 MEL/CDL
02.53.04 FUSELAGE 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.54.01 NACELLES / PYLON
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
54 NACELLES / PYLON 54-01
NACELLE STRAKE
4
0
All may be missing. Note: Must not be combined with MCDL item 53-03 (Refer to 53-03 Root Fillet Fairing). Procedures: Approach speed: VLS + 4 kt. Landing distance: multiply by 1.09. Performance: The following performance penalties are applicable: -
If no internal strakes and one or both external strakes are missing, takeoff performance limiting weight is reduced by 2 380 kg
-
If one or both internal strakes are missing (with or without external strakes missing), takeoff performance limiting weight is reduced by 3 270 kg
-
Increase V2 and VR by 1 kt. Note: The performance penalties are not applicable if the flight crew can check V2 greater than 1.17 VS1G. (Cont’d on next page)
A320/321 MEL/CDL
02.54.02 NACELLES / PYLON 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
54 NACELLE / PYLON 54-01
NACELLE STRAKE (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.54.03 NACELLES / PYLON
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
54 NACELLES / PYLON 54-03
PYLON PRESSURE RELIEF DOOR 413(423) BL 414(424) BR
4
0
(M)
All may be missing for 5 flight cycles only. Note: i.
If one door is missing on a pylon, the other door on the same pylon must be removed.
ii. Must not be combined with MCDL item 53-03 (Refer to 53-03 Root Fillet Fairing). Limitations: Maximum cruise speed: M 0.78. Procedures: Approach speed: VLS + 4 kt. Landing distance: multiply by 1.09. Performance: The following performance penalties are applicable: -
Takeoff performance limiting weight is reduced by 2 380 kg
-
Increase V2 and VR by 1 kt Note: The above performance penalties are not applicable if the flight crew can check V2 greater than 1.16 VS1G.
-
If two or more doors are missing, en route performance limiting weight is reduced by 40 kg per missing door
-
If three or more doors are missing, fuel consumption is increased by 0.09 % per missing door.
MAINTENANCE PROCEDURES Refer to AMM 54-52-00-040-001 (Cont’d on next page)
A320/321 MEL/CDL
02.54.04 NACELLES / PYLON 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
54 NACELLES / PYLON 54-03
PYLON PRESSURE RELIEF DOOR 413(423) BL 414(424) BR (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.54.05 NACELLES / PYLON
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
54 NACELLES / PYLON 54-04
PYLON ACCESS DOOR 415(425) AL - 415(425) AR
4
0
All may be missing for 5 flight cycles provided the hole is covered with high speed tape. Limitations: Flight in forecasted thunderstorm conditions is not allowed.
A320/321 MEL/CDL
02.54.06 NACELLES / PYLON 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
54 NACELLES / PYLON 54-05
PYLON FAIRING SEAL
4
3
One may be missing per pylon.
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 MEL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
54 NACELLE/PYLON 54-06
AERODYNAMIC SEAL
2
0
(M)
All may be missing. MAINTENANCE PROCEDURES Refer to AMM 54-53-00-040-001
02.54.07 NACELLES / PYLON
A320/321 MEL/CDL
02.54.08 NACELLES / PYLON 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 MEL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.57.01 WINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
57 WINGS 57-01 57-01a
Wing Tip Fence Lower Part Of A Wing Tip Fence
2
1
(M)
One lower part of a wing tip fence may be missing provided the broken part is removed and holes are covered. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 3 960 kg
-
En-route performance limiting weight is reduced by 378 kg
-
Fuel consumption is increased by 0.88 %.
MAINTENANCE PROCEDURES Refer to AMM 57-31-00-040-001 57-01b
Complete Wing Tip Fence
2
1
(M)
One complete wing tip fence may be missing provided exposed interior structure is covered, protective material is inspected before each flight and replaced if necessary. Performance: The following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 8 910 kg
-
En-route performance limiting weight is reduced by 735 kg
-
Fuel consumption is increased by 1.34 %.
MAINTENANCE PROCEDURES Refer to AMM 57-31-00-040-001 (Cont’d on next page)
A320/321 MEL/CDL
02.57.02 WINGS 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
57 WINGS 57-01
Wing Tip Fence (Cont’d)
2.
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.57.03 WINGS
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
57 WINGS 57-02
BELLY FAIRING SLIDING PANEL
2
0
All may be missing. Performance: If two panels are missing, the following performance penalties are applicable: -
Takeoff and approach climb performance limiting weights are reduced by 96 kg
-
En route performance limiting weight is reduced by 108 kg
-
Fuel consumption is increased by 0.28 %.
A320/321 MEL/CDL
02.57.04 WINGS 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
57 WINGS 57-03
OUTBOARD FLAP RUBBING STRIP ITEMS 40, 70, 80, 85, 100, 120
12
0
All may be missing.
*
*
*
12 FEB 12 CDL
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
71 POWER PLANT 71-01
FRANGIBLE DRAIN MAST
2
0
((M)
All may be missing. MAINTENANCE PROCEDURES Refer to AMM 71-71-42-040-044
02.71.01 POWER PLANT
A320/321 MEL/CDL
02.71.02 POWER PLANT 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
71 POWER PLANT 71-09
FAN COWL HOLD OPEN ROD
8
0
(M)
All may be missing. MAINTENANCE PROCEDURES Refer to AMM 71-13-12-000-040
*
*
*
A320/321 MEL/CDL
12 FEB 12 CDL 1. SYSTEM & SEQUENCE OF ITEMS
2.
ITEM
02.78.01 EXHAUST
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
78 EXHAUST 78-09
THRUST REVERSER 11 AND 1 O'CLOCK STRUTS
4
0
(M)
All may be missing. Note: The affected thrust reverser must be considered inoperative (Refer to MEL/MI-78-30 Thrust Reverser). MAINTENANCE PROCEDURES Refer to AMM 78-32-11-040-001
*
*
*
A320/321 MEL/CDL
02.78.02 EXHAUST 1. SYSTEM & SEQUENCE OF ITEMS
ITEM
2.
12 FEB 12 CDL
NUMBER INSTALLED 3.
NUMBER REQUIRED FOR DISPATCH 4.
REMARKS OR EXCEPTIONS
THIS PAGE INTENTIONALLY LEFT BLANK