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A319/A320/A321 TECHNICAL TRAINING MANUAL MECHANICS / ELECTRICS & AVIONICS COURSE 25 EQUIPMENT/FURNISHINGS

This document must be used for training purpose only

Under no circumstances should this document be used as a reference.

It will not be updated.

All rights reserved. No part of this manual may be reproduced in any form, by photostat, microfilm, retrieval system, or any other means, without the prior written permission of Airbus Industrie.

A319/A320/A321 TECHNICAL TRAINING MANUAL _ MECHANICS / ELECTRICS & AVIONICS COURSE

25 EQUIPMENT/FURNISHINGS

25 EQUIPMENT/FURNISHINGS UFD4200

TABLE OF CONTENTS

Page

GENERAL ** System Presentation (1) ....................... 1 COCKPIT ** Cockpit Seats Presentation (1) ................ 9 ** Cockpit Emergency Equipment (1) ............. 17 ** Cockpit Seats Description/Operation (3) ..... 21 Sliding Windows Desc/Operation (3) ............. 27 Cockpit Escape Rope D/O (3) ..................... 31 ** Components (3) ................................ 35

UFD4200

PASSENGER COMPARTMENT ** Cabin Presentation (1) (A320) ................ 41 ** Cabin Presentation (1) (A319) ................ 45 ** Cabin Presentation (1) (A321) ................ 49 ** Cabin EQPT & Furnishings Presentation (1) ... 53 Typical Galley Presentation (1) ................. 57 Typical Lavatory Presentation (1)............... 63 Typical Galley Installation D/O (3) ............ 69 Typical Lavatory Installation D/O (3) .......... 77 Passenger and Attendant Seats (3)............... 85 ** Cabin Panel Removal/Installation (3) ....... 101 ** Cabin Equipment & Furnishings CMPNTS (3) ... 113

** ** ** ** ** ** ** **

Offwing ESC SLD CYL R/I (3) ................. 175 Offwing ESC SLD INSTL (3) ................... 179 EMER Exit ESC SLD/Desc/Deploy (3) (A321) ... 183 EMER Exit ESC SLD/Disconnection (3)(A321) .. 187 Pax Door ESC SLD/Raft Inflat. CYL CHK(3) ... 191 Offwing ESC SLD Inflation CYL CHK(3) ....... 195 Offwing ESC SLD Release Mechanism Desc.(3). 203 Components (3) ............................... 213

CARGO COMPARTMENTS ** Cargo Compartment Presentation (1) ......... 221 ** Cargo Compartment Interior (1) ............. 225 ** Cargo Compartment Capabilities (1) (A320) .. 235 ** Cargo Compartment Capabilities (1) (A319) .. 243 ** Cargo Compartment Capabilities (1) (A321) .. 251 ** Cargo Loading System Presentation (1) ...... 259 ** Cargo Loading Operation (3) ................. 271 ** Cargo Bulk Loading (3) ...................... 275 ** Draining System D/O (3) ..................... 283 ** Cargo Loading Components (3) ................ 287

EMERGENCY EQUIPMENT ** Escape Facility Presentation(1)(A320/319) .. 125 ** Escape Facility Presentation (1) (A321) .... 131 ** Miscellaneous Emergency EQPT Present. (1) .. 137 ** Pax Door ESC SLD/Desc/Depl (3) ............. 143 ** Pax Door ESC SLD/Disctn (3) ................. 147 ** Pax Door ESC SLD/INSTL (3) .................. 151 ** Pax Door ESC SLD/Raft Desc/Depl (3) ........ 155 ** Pax Door ESC SLD/Raft Disctn (3) ........... 159 ** Pax Door ESC SLD/Raft INSTL (3) ............ 163 ** Offwing ESC SLD Deploy. (3) ................. 167 ** Offwing ESC SLD Removal (3) ................. 171

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SYSTEM PRESENTATION

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CONTENTS: General Cockpit Passenger Compartment Cargo Compartment Emergency Equipment Avionics Compartment

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SYSTEM PRESENTATION GENERAL The equipment and furnishings which are installed in the aircraft provide comfort and safety to passengers and crew. The equipment and furnishings are located in different compartments : - The cockpit, - The passenger compartment, - The cargo compartments. COCKPIT

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Various furnishings and equipment are fitted in the cockpit for the comfort, convenience and safety of the occupants. The cockpit is also equipped with adjustable seats for two crew members and folding seats for the third occupant and, if it the option is installed, for the fourth occupant.

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SYSTEM PRESENTATION - GENERAL & COCKPIT EFFECTIVITY EFFECTIVITY ALL

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SYSTEM PRESENTATION PASSENGER COMPARTMENT The and The The

passenger compartment is divided into utility areas seating areas. equipment and furnishings which are installed in: seating areas : - First-class and/or economy-class passenger seats and cabin attendant seats, - Linings and furnishings that cover the compartment structure, - Overhead stowage compartment, - Passenger service/information units, The utility areas : - Cabin attendant seats, - Passenger Service Units (PSUs), - Ancillary equipment, - Galleys, - Lavatories. CARGO COMPARTMENT

TMUESGS01-T02 LEVEL 1

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In the lower deck of the aircraft, there are two lower holds: the FWD cargo compartment and, the AFT/Bulk cargo compartments.

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SYSTEM PRESENTATION - PASSENGER AND CARGO COMPARTMENTS EFFECTIVITY EFFECTIVITY ALL

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SYSTEM PRESENTATION EMERGENCY EQUIPMENT Emergency equipment is kept in different locations in the cockpit and in the cabin. Emergency equipment is composed of : - Fire protection and emergency oxygen equipment, - Cockpit and cabin escape facilities, - Floatation and survival equipment, - Evacuation signalling equipment, - Rapid decompression system. AVIONICS COMPARTMENT

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The avionics compartment is located in the underfloor below the cockpit. For maintenance it can be accessed through four outside access doors and an access panel in the passenger compartment.

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SYSTEM PRESENTATION - EMERGENCY EQUIPMENT & AVIONICS COMPARTMENT EFFECTIVITY EFFECTIVITY ALL

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CONTENTS: General Captain And First Officer Seats Third Occupant Seat Fourth Occupant Seat

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COCKPIT SEAT PRESENTATION GENERAL

TMUESFV09-T01 LEVEL 1

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The cockpit is basically equipped with three seats : - a Captain seat, - a First Officer seat, - a Third Occupant seat located against the right AFT panel. If the option is installed, a folding seat for the Fourth Occupant is located in the cockpit left AFT section.

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COCKPIT SEAT PRESENTATION CAPTAIN AND FIRST OFFICER SEATS

TMUESFV09-T02 LEVEL 1

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The Captain and First Officer seats are symmetrical and their operation is identical. They are not interchangeable. The Captain and First Officer seats are secured to the cockpit floor.

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COCKPIT SEAT PRESENTATION THIRD OCCUPANT SEAT The Third Occupant seat is a folding seat attached to the right rear panel in the cockpit. No longitudinal adjustment is provided. It can slide along the lateral axis. FOURTH OCCUPANT SEAT

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The Fourth Occupant seat is a folding seat located against the left rear partition in the cockpit. The fourth occupant seat is optionally installed. This seat is not adjustable.

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25 - EQUIPMENT/FURNISHINGS 25-60-00 COCKPIT EMERGENCY EQUIPMENT

TMUESFQ06 LEVEL 1

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CONTENTS: Escape Rope Fire Extinguisher Smoke Hood Fire Protective Gloves Crash Axe Life Vest Medical Kit Oxygen Masks Flash Light

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COCKPIT EMERGENCY EQUIPMENT ESCAPE ROPE

FLASH LIGHT

Two items.

Two items.

FIRE EXTINGUISHER One item. SMOKE HOOD One item. FIRE PROTECTIVE GLOVES One item. CRASH AXE One item. LIFE VEST Four items.

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MEDICAL KIT One item OXYGEN MASKS Four items.

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25 - EQUIMENT/FURNISHINGS 25-11-00 COCKPIT SEATS DESCRIPTION/OPERATION

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CONTENT: Pilot Seats Third Occupant Seat Fourth Occupant Seat

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COCKPIT SEATS DESCRIPTION/OPERATION PILOT SEATS Seat movements adjusted.

can

be

electrically

or

manually

TMUESCO0B-T01 LEVEL 3

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VERTICAL TRAVEL To adjust the seat upwards or downwards, pull the control handle marked "V"to unlock the seat. Manual control : - Take your weight off the seat and adjust the seat to the required position. - Release the handle to lock the seat. - To adjust the seat downwards the procedure is similar, your weight is sufficient to move the seat downwards. - The down movement of the seat is slowed down by means of a gas cylinder. Electrical control : - For vertical electrical control, place the control switch in the UP or DOWN position until the seat reaches the required position.

BACKREST Pull the control handle marked "R" to adjust the backrest position. The system is controlled via two cables. A gas cylinder acts as a return spring for the backwards movement of the backrest. LUMBAR REST Two coaxial knobs enable vertical and horizontal lumbar rest adjustment. Rotation of the triangular knob ensures depth adjustment of the lumbar rest. Rotation of the second serrated knob ensures vertical movement of the lumbar rest. INBOARD ARMREST The inboard armrest can be raised vertically and stowed behind the backrest. The inboard armrest is located on the pedestal side Height adjustment is made using a knob located on the front.

HORIZONTAL TRAVEL To move the seat forwards or backwards pull the control handle marked "H"to unlock the seat. Manual control : - When the desired position is reached, release the handle to lock the seat. Electrical control : - For horizontal electrical control, place the control switch in the FORWARD or REAR position until the seat reaches the required position. NOTE: Horizontal travel indicators give the longitudinal position of the seat.

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COCKPIT SEATS DESCRIPTION/OPERATION (PILOT SEATS) EFFECTIVITY EFFECTIVITY ALL

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COCKPIT SEATS DESCRIPTION/OPERATION PILOT SEATS

THIRD OCCUPANT SEAT

SIDESTICK ARMREST The sidestick armrest comprises the fixed arm, the carrier arm and the sidestick table. The fixed arm is attached to the seat pan. It supports the carrier arm and sidestick table assembly. Sidestick table height adjustment is controlled by a knob located on the armrest. Armrest table tilt angle is controlled by a knob located on the front of the armrest. A position indicator fitted on top of the table shows the table tilt. A wheel avoids interference between the armrest and the lateral console when the seat is moved forwards with the table fully inclined.

Seat movements are manually adjusted. A manual control enables the seat to be moved from its stowage. A second control serves to unlock the headrest. The headrest can be folded down so that the circuit breaker panel can be opened while the seat is in its stowed position. A compartment closed by VELCRO tapes and containing a life vest is provided in the lower part of the seat. The safety harness includes straps and an inertia reel controlled by a handle located on the left of the seat, which serves to lock or unlock the inertia reel.

TMUESCO0B-T02 LEVEL 3

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SAFETY HARNESS The shoulder harness is fitted on an inertia reel which can be locked by a control lever, located behind the backrest.

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FOURTH OCCUPANT SEAT The fourth occupant seat is a non- adjustable folding seat. The seat cushion is folded down into place and returns to its stowed position by pressing it upwards and against the partition. The lower section of the seat is provided with a compartment containing a life vest and closed by VELCRO tapes. The safety harness includes straps and an inertia reel, locking control located in the coat storage compartment. The fourth occupant seat is optionally installed.

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25 - EQUIPMENT/FURNISHINGS 25-61-00 COCKPIT SLIDING WINDOWS DESCRIPTION/OPERATION

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CONTENTS: Windows

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COCKPIT SLIDING WINDOWS DESCRIPTION/OPERATION WINDOWS

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One side window is provided on each side of the cockpit beside the seats. The cockpit sliding windows can only be operated from the inside. To open a window, push down the red indicator on top of the opening handle. Prior to closing, unlock the window by pulling the locking pin.

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COCKPIT SLIDING WINDOWS DESCRIPTION/OPERATION - WINDOWS EFFECTIVITY EFFECTIVITY ALL

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CONTENTS: Ropes

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COCKPIT ESCAPE ROPE DESCRIPTION/OPERATION ROPES

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Two ropes enable cockpit crew evacuation through the sliding windows. Two escape ropes are provided in stowage boxes located over the sliding windows. Pull the cover off the stowage box, grasp the handle and throw it out. Each rope can be used through either sliding window in any normal or abnormal aircraft configuration.

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COCKPIT ESCAPE ROPE DESCRIPTION/OPERATION - ROPES EFFECTIVITY EFFECTIVITY ALL

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CONTENTS: Captain and First Officer Seats Pilot Seat Harness Sidestick Armrest Third Occupant Seat Fourth Occupant Seat

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COCKPIT COMPONENTS CAPTAIN AND FIRST OFFICER SEATS

SIDESTICK ARMREST

IDENTIFICATION FIN: 3MS(CAPTAIN), 4MS(F/O)

IDENTIFICATION FIN: 3MS(CAPTAIN), 4MS(F/O)

LOCATION ZONE: 211, 212

LOCATION ZONE: 211, 212

COMPONENT DESCRITION All the manual controls must be operative for each pilot. Electrical controls are optionally installed and may be inoperative.

COMPONENT DESCRITION The manual controls may be inoperative provided setting is suitable for proper operation.

PILOT SEAT HARNESS IDENTIFICATION FIN: 3MS(CAPTAIN), 4MS(F/O) LOCATION ZONE: 211, 212

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COMPONENT DESCRITION The aircraft may not leave an airport where repair or replacements can be made.

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COCKPIT COMPONENTS-CAPTAIN AND FIRST OFFICER SEATS-PILOT SEAT HARNESS-SIDESTICK ARMREST EFFECTIVITY EFFECTIVITY ALL

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THIRD OCCUPANT SEAT IDENTIFICATION FIN: 14MM LOCATION ZONE: 212 FOURTH OCCUPANT SEAT IDENTIFICATION FIN: 13MM

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LOCATION ZONE: 211 The fourth occupant seat is optionally installed.

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COCKPIT COMPONENTS - SIDESTICK ARMREST - THIRD OCCUPANT SEAT - FOURTH OCCUPANT SEAT EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-20-00 CABIN PRESENTATION

TMUESCC01 LEVEL 1

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CONTENTS: General Class Layout Passenger Seats Cabin Attendant Seats Galleys Lavatories Curtains And Partitions

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CABIN PRESENTATION GENERAL

GALLEYS

The passenger compartment can be equipped in different configurations.

The number and location of the galleys vary with the cabin configuration and the aircrft utilization.

CLASS LAYOUT

LAVATORIES

Three typical cabin configurations are : - Basic all economy, - Typical mixed class, - High density. Basic all economy cabin configuration accomodates only tourist class with six seats abreast. Typical mixed class cabin configuration accomodates first class with four seats abreast, tourist class with six seats abreast. High density cabin configuration accomodates only tourist class with six seats abreast.

The number and location of the lavatories change with the cabin configuration. CURTAINS AND PARTITIONS Classes and zones are divided by floor partitions and ceiling mounted curtains.

mounted

PASSENGER SEATS The passenger seats are mounted on standard tracks which allow quick removal for cabin configuration change.

TMUESCC01-T01 LEVEL 1

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CABIN ATTENDANT SEATS Cabin attendant seats are attached to partitions or lavatory walls. Depending on the cabin configuration, the number and location of cabin attendant seats can vary. The three main types of cabin attendant seats are wall mounted single, wall mounted double bench and wall mounted swivel; all are folding seats.

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CONTENTS: General Class Layout Passenger Seats Cabin Attendant Seats Galleys Lavatories Curtains And Partitions

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CABIN PRESENTATION GENERAL

GALLEYS

The passenger compartment can be equipped in different configurations.

The number and location of the galleys vary with the cabin configuration and the aircrft utilization.

CLASS LAYOUT

LAVATORIES

Three typical cabin configurations are : - Basic all economy, - Typical mixed class, - High density. Basic all economy cabin configuration accomodates only tourist class with six seats abreast. Typical mixed class cabin configuration accomodates first class with four seats abreast, tourist class with six seats abreast. High density cabin configuration accomodates only tourist class with six seats abreast.

The number and location of the lavatories change with the cabin configuration. CURTAINS AND PARTITIONS Classes and zones are divided by floor partitions and ceiling mounted curtains.

mounted

PASSENGER SEATS The passenger seats are mounted on standard tracks which allow quick removal for cabin configuration change.

TMUESCC03-T01 LEVEL 1

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CABIN ATTENDANT SEATS Cabin attendant seats are attached to partitions or lavatory walls. Depending on the cabin configuration, the number and location of cabin attendant seats can vary. The three main types of cabin attendant seats are wall mounted single, wall mounted double bench and wall mounted swivel; all are folding seats.

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CABIN PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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TMUESCC02 LEVEL 1

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CONTENTS: General Class Layout Passenger Seats Cabin Attendant Seats Galleys Lavatories Curtains And Partitions

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CABIN PRESENTATION GENERAL The passenger compartment can be equipped in different configurations.

Swivel seats are attached to the cabin floor structure. Wall mounted single seats are attached to the partition or to the lavatory wall. GALLEYS

CLASS LAYOUT Three typical cabin configurations are : - Standard specification, - Optional mixed class, - High density. Standard specification cabin configuration accomodates only tourist class with six seats abreast. Optional mixed class cabin configuration accomodates first class with four seats abreast, tourist class with six seats abreast. High density cabin configuration accomodates only tourist class with six seats abreast.

The number and location of the galleys vary with the cabin configuration and the aircrft utilization. LAVATORIES The number and location of the lavatories change with the cabin configuration. CURTAINS AND PARTITIONS Classes and zones are divided by floor partitions and ceiling mounted curtains.

mounted

PASSENGER SEATS The passenger seats are mounted on standard tracks which allow quick removal for cabin configuration change.

TMUESCC02-T01 LEVEL 1

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CABIN ATTENDANT SEATS Depending on the cabin configuration, the number and location of cabin attendant seats can vary. There are three main types of cabin attendant seats and all are folding seats. Free standing seats are attached to the cabin floor structure.

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TMUESCA01 LEVEL 1

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CONTENTS: General Lower Sidewall Panels Upper Sidewall Panels Cove Light Panels Overhead Stowage Compartment Ceiling Panels PSU/PIU Self Examination

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CABIN EQUIPMENT AND FURNISHINGS PRESENTATION GENERAL The cabin interior is equipped with removable panels. The modular lining design allows cabin customization within flexibility areas.

They extend from the first seat row to the last seat row on the left and right side of the cabin. The overhead stowage compartments are of different sizes and are arranged to suit the cabin layout. CEILING PANELS

LOWER SIDEWALL PANELS The lower sidewall panels are mounted between the cabin floor and the sidewall panels. They are equipped with rapid decompression doors.

Removable ceiling panels are mounted in the cabin. They are installed over the full lenght of the cabin and the utility areas. PSU/PIU

UPPER SIDEWALL PANELS The upper sidewall panels are mounted on the side of the cabin. They include the window contour Inner window panels and sunvisors are fitted to the window frames.

TMUESCA01-T01 LEVEL 1

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COVE LIGHT PANELS The cove light panels covers the space between the upper sidewall panels and the overhead stowage compartments. The cove light panels are removable to allow cabin light replacement. OVERHEAD STOWAGE COMPARTMENT The overhead stowage compartments are intalled above the cabin seat rows.

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The Passenger Service Information Units comprise the Passenger Service Units and Passenger Information Units. They are installed in the service channel, above the set rows. The PSU’s and PIU’s have different lenghts to agree to aircraft furnishing configuration. These units are: - information panel, - attendant call panel, - emergency oxygen mask and generator container, - reading light panel, - individual air outlet-panel. NOTE: On the attendant call panel and the reading light panel the bulb cover is removable. This enables the bulbs to be replaced without removing the PSIU’s.

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CABIN ATTENDANT AND FURNISHING PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

Where are A B C -

passenger oxygen masks stored ? In the Passenger Service Unit. In the seat arm rest. In the overheat stowage compartment.

Where are A B C -

the cabin depressurization doors mounted? On the upper sidewall panels. On the ceiling panels. On the lower sidewall panels.

TMUESCA01 LEVEL 1

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Which cabin panels are removable ? A - Lower sidewall panels only. B - All the panels. C - Upper sidewall panels only.

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25 - EQUIPMENT/FURNISHINGS 25-30-00 TYPICAL GALLEY PRESENTATION

TMUESGP01 LEVEL 1

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CONTENTS: General Dry Galleys Wet Galleys Galleys Cooling

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TYPICAL GALLEY PRESENTATION GENERAL

TMUESGP01-T01 LEVEL 1

UFD4200

The galleys are buyer furnished equipment. They are normally installed in the Forward and Aft sections of the cabin. They are attached at the top to the aircraft structure and at the bottom to the strengthened points in the cabin floor structure. The position and the number of galleys change with the cabin configuration.

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DRY GALLEYS The dry galleys are not connected to the aircraft systems such as ventilation or potable water. Dry galleys are mainly used to store the trolleys and to keep foods and drinks. WET GALLEYS The wet galleys are connected to : - the water and waste system, - the air extraction system, - the main air cabin ventilation system, - the electrical power system. GALLEYS COOLING

TMUESGP01-T02 LEVEL 1

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At most galley locations, chilled air systems are used to cool the meal trolleys. The freon cooling system requires special servicing.

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DRY / WET GALLEYS EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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25 - EQUIPMENT/FURNISHINGS 25-40-00 TYPICAL LAVATORY PRESENTATION

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CONTENTS: General Lavatory

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TYPICAL LAVATORY PRESENTATION GENERAL

TMUESLP01-T01 LEVEL 1

UFD4200

Lavatories are normally installed at the forward and aft sections of the cabin. They are assembled as modular units and they are attached at the top of the aircraft structure and at the bottom to hard points in the cabin floor structure. The position and the number of lavatories change with the cabin configuration.

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TYPICAL LAVATORY PRESENTATION LAVATORY

TMUESLP01-T02 LEVEL 1

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All lavatories have the same equipment. They are connected to the electrical power system, air conditioning system and water/waste system. In case of emergency all lavatories can be unlocked from the outside.

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25 - EQUIPMENT/FURNISHINGS 25-30-00 TYPICAL GALLEY INSTALLATION D/O CONTENTS:

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General Lower Attachment Upper Attachment Interfaces Safety Precautions

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TYPICAL GALLEY INSTALLATION D/O GENERAL

TMUESGD02-T01 LEVEL 3

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Installation of any galley includes the adaptations of the surrounding furnishings and the installation of dummy metal windows behind lateral galleys where necessary. Galley equipment may contain: - ovens, - water heaters, - hot jugs, - hot cups, - coffee makers, - waste trolleys, - containers.

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TYPICAL GALLEY INSTALLATION D/O - GENERAL EFFECTIVITY EFFECTIVITY ALL

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TYPICAL GALLEY INSTALLATION D/O LOWER ATTACHMENT

TMUESGD02-T02 LEVEL 3

UFD4200

Galleys are mounted to the floor on existing seat rails wherever possible. Remaining attachment points consist of hard points which are fixed on additional longitudinal beams. These additional longitudinal beams are only mounted at selected galley locations on structural provisions existing in the uncustomized aircraft. Seat rail attachments provide inch by inch flexibility and hard points provide 2 inches by 2 inches flexibility.

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TYPICAL GALLEY INSTALLATION D/O - LOWER ATTACHMENT EFFECTIVITY EFFECTIVITY ALL

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TYPICAL GALLEY INSTALLATION D/O UPPER ATTACHMENT

TMUESGD02-T03 LEVEL 3

UFD4200

Upper attachments consist of a bracket and two adjustable tie rods. The final attachment is then achieved from the galley by means of tie rods which are part of the galley. The upper attachment points, the fittings for the tie rods, are mounted on the frames on the selected galley locations on the aircraft structure. The final attachment of the galley to the fitting is achieved with a tie rod.

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TYPICAL GALLEY INSTALLATION D/O - UPPER ATTACHEMENT EFFECTIVITY EFFECTIVITY ALL

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INTERFACES

SAFETY PRECAUTIONS

A wet galley unit has several interfaces: - The typical water and waste connections which go through the aircraft floor panel. - The hoses for the typical individual and exhaust air interface which are located on top of the galley. An exhaust air system must be installed on galleys with ovens. - Galleys with electrical equipment which are connected to the nearest terminal board for the power supply. The connectors are found in the ceiling. The wiring should contain sufficient free length to allow removal and installation of the galley unit or galley equipment.

These are the safety precautions for the installation of a galley unit. REMOVAL: - Open, safety and tag corresponding circuit breakers. - Empty galley compartments. - Remove galley catering equipment. - Remove linings in galley area where necessary. - Drain the aircraft water system. INSTALLATION: - Open, safety and tag corresponding circuit breakers. - Installation of removed linings in galley area. - Operational test of coffee maker, water heater and oven. WARNINGS: - USE SOLVENTS AND SEALANTS ONLY WITH GOOD SUPPLY OF AIR. - OBEY THE MANUFACTURER’S INSTRUCTIONS. - PUT ON PROTECTIVE CLOTHING. - GET NOTHING IN YOUR MOUTH AND DON’T SMOKE. - DON’T BREATHE THE VAPORS. - GET MEDICAL HELP IF THE SKIN OR EYES BECOME IRRITATED.

TMUESGD02 LEVEL 3

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TYPICAL GALLEY INSTALLATION D/O

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TMUESLD02 LEVEL 3

UFD4200

CONTENTS: Attachment Interfaces Safety Precautions Door Operation

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TYPICAL LAVATORY INSTALLATION D/O ATTACHMENT Each lavatory, made of composite material, is a completely assembled housing with an integrated floor. Each lavatory is equipped with several accessories. LOWER Lower attachments are obtained by means of four hard points or four seat rail attachments.

TMUESLD02-T01 LEVEL 3

UFD4200

UPPER (LATERAL) Lateral lavatories have one attachment at the top and one attachment at the rear side. Depending on the location of the lavatory, one or two upper attachments are used.

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TYPICAL LAVATORY INSTALLATION D/O - ATTACHMENT EFFECTIVITY EFFECTIVITY ALL

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TYPICAL LAVATORY INSTALLATION D/O INTERFACES

SAFETY PRECAUTIONS

A lavatory unit has several interfaces: - Typical individual and exhaust air interface. - Typical water and waste interface. - Plug which supplies power for the different electrical systems which are installed in the lavatory.

These are the safety precautions for the installation of a lavatory unit. R/I SAFETY PRECAUTIONS : * Make sure that corresponding circuit breakers are open, safetied and tagged. * Drain the potable water system and the toilet system. * Do not service the potable water system. * Do not service the toilet system.

TMUESLD02-T02 LEVEL 3

UFD4200

WARNINGS : * AS SOLVENTS, SEALANTS AND OTHER SPECIAL MATERIAL ARE USED, BE SURE THAT SUFFICIENT AIR IS SUPPLIED. * PUT NOTHING IN YOUR MOUTH. * DON’T SMOKE. * IF NECESSARY, PUT ON PROTECTIVE CLOTHING. * GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED. * OBEY THE MANUFACTURER’S INSTRUCTIONS.

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TYPICAL LAVATORY INSTALLATION D/O - INTERFACES EFFECTIVITY EFFECTIVITY ALL

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TYPICAL LAVATORY INSTALLATION D/O DOOR OPERATION

TMUESLD02-T03 LEVEL 3

UFD4200

During normal door operation, when the indicator reads VACANT, the door can be opened from the outside by rotating the latch. To open the door from the inside, the locking device has to be pushed to unlock the door and then the knob has to be rotated. In case of emergency, the door can be unlocked from outside without using a special tool. Lift the lavatory cover-plate and push the unlocking pin. Then rotate the latch to open the door.

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TYPICAL LAVATORY INSTALLATION D/O - DOOR OPERATION EFFECTIVITY EFFECTIVITY ALL

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TMUESLD02 LEVEL 3

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25 - EQUIPMENT/FURNISHINGS 25-21-00 PASSENGER AND ATTENDANT SEATS

TMUESPS02 LEVEL 3

UFD4200

CONTENTS: Pax Seat Pax Seat Description Pax Seat Attachement Cabin Attendant Seat Cabin Attendant Seat Description Cabin Attendant Seat Attachment Self Examination

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PASSENGER AND ATTENDANT SEATS PAX SEAT Passenger seats are designed for the comfort and safety of the passengers. They are located in the cabin, from the cockpit partition to the aft pressure bulkhead. PAX SEAT DESCRIPTION The passenger seat consists of a framework assembly with: - an upholstered seatpan, - an upholstered backrest assembly, - a folding table, - seat belts, - an upholstered armrest and, - a pocket.

TMUESPS02-T01 LEVEL 3

UFD4200

FRAMEWORK The seat framework holds the seatpan, backrest, armrest and table. A luggage bar is fitted to the front framework legs. Holders for life vests are found below each seatpan. The seat electronic box which serves the passenger service units is installed between the front and rear legs. SEATPAN The upholstered seatpan is installed on the seat framework. It is not foldable or adjustable.

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BACKREST The upholstered backrest assembly of each seat can be hydraulically reclined backwards until it hits an adjustable mechanical stop. The backrest can be mechanically folded forward. TABLE A folding table is installed in the rear of each backrest. When not in use, it is kept in a recess in the backrest by means of a latch. Two hinged arms hold the table when it is folded down. In-armrest tables are installed in the seats, located just behind partitions, galleys or lavatories. SEAT BELT Each seat is equipped with a seat belt. It is attached to the seat framework and has a buckle to lock and to adjust the seat belt length. ARMREST Each seat has armrests. The outer armrests of a seat unit are not foldable. The armrests between the seats can be folded up. The reclining control button for the backrest and an ashtray are installed in the armrest. POCKET A pocket is installed on the back of each seat backrest. A safety instruction card and an air-sickness bag are kept in this pocket.

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PASSENGER AND ATTENDANT SEATS - PAX SEAT EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS PAX SEAT ATTACHMENT

TMUESPS02-T02 LEVEL 3

UFD4200

A quick release fitting in each rear leg and a retainer in each front leg attach the seat unit to the seat tracks. By placing the quick release device in the up position, the seat can be moved on the tracks or removed completely.

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PASSENGER AND ATTENDANT SEATS CABIN ATTENDANT SEAT

TMUESPS02-T03 LEVEL 3

UFD4200

Cabin attendant seats are installed in the forward and aft utility areas or in the passenger seating area. The different types of cabin attendant seats are free standing, swivel and wall mounted attendant seats.

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS CABIN ATTENDANT SEAT DESCRIPTION Cabin Attendant seats consist of: - an aluminium framework, - a backrest with cushion, - a seatpan with cushion, - a headrest with cushion, - a stowage container and, - seat belts.

SAFETY HARNESS Each cabin attendant seat has a seat belt and a shoulder harness with a center buckle. The shoulder harness is pulled-in automatically on inertia reels when not in use. STOWAGE CONTAINER A stowage container with a latch door is located below the seatpan.

FRAMEWORK The seat frame of the cabin attendant seat is assembled out of two aluminium side frames and a backrest framework. HEADREST The headrest cushion is upholstered with foam and seat fabric. The headrest is attached to the seat frame.

TMUESPS02-T04 LEVEL 3

UFD4200

BACKREST The backrest cushion is upholstered with foam and seat fabric. SEATPAN The seatpan is made of an aluminium pan. The seatpan cushion is upholstered with foam and seat fabric. Hinges attach the seatpan to the seat frame. The seatpan is spring loaded to retrct when not in use.

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT DESCRIPTION EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS CABIN ATTENDANT SEAT ATTACHMENT Cabin attendant seats are attached to walls or to the cabin floor.

TMUESPS02-T05 LEVEL 3

UFD4200

WALL MOUNTED The three sections of the cabin attendant seat are attached with six bolts to: - partitions, - lavatories walls.

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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT ATTACHMENT - WALL MOUNTED EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS CABIN ATTENDANT SEAT ATTACHMENT

TMUESPS02-T06 LEVEL 3

UFD4200

FREE STANDING Free standing cabin attendant seats can be mounted on seat rails with inch by inch flexibility. Free standing cabin attendant seats can also be attached to the cabin floor structure by hardpoints.

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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT ATTACHMENT - FREE STANDING EFFECTIVITY EFFECTIVITY ALL

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PASSENGER AND ATTENDANT SEATS CABIN ATTENDANT SEAT ATTACHMENT

TMUESPS02-T07 LEVEL 3

UFD4200

SWIVEL Swivel attendant seats are attached to the cabin floor structure by hardpoints.

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PASSENGER AND ATTENDANT SEATS - CABIN ATTENDANT SEAT ATTACHMENT - SWIVEL EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

legs and in the rear legs as well in the front legs.

TMUESPS02 LEVEL 3

UFD4200

How are passenger seats attached ? A - With retainers in the front with quick release fittings legs. B - With retainers in the front as in the rear legs. C - With quick release fittings legs as well as in the rear

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-20-00 CABIN PANEL REMOVAL/INSTALLATION

TMUESCB01 LEVEL 3

UFD4200

CONTENT: Ceiling Panels Overhead Stowage Compartments Passenger Service Information Unit (PSIUs) Cove Light Panels Upper Sidewall Panels Lower Sidewall Panels

EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION CEILING PANELS

TMUESCB01-T01 LEVEL 3

UFD4200

To remove the ceiling panel, apply the following procedure : - Disconnect the two electrical connectors through access doors located in the corresponding overhead stowage compartment. - Unlock the two quick release fasteners at the left side of the ceiling panel. - Push the left side of the ceiling panel upward. - Move the ceiling panel to the left and out of the spring fasteners. - Lower the right side and slide the ceiling panel out, making sure the right side is clear from the overhead stowage compartments. - Remove the ceiling panel.

EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION - CEILING PANELS EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION OVERHEAD STOWAGE COMPARTMENTS Before removing the overhead stowage compartment : - the ceiling panels and the cove light panels adjacent to the stowage compartment, - the emergency oxygen container, - the Passenger Service Information Unit, must be removed.

TMUESCB01-T02 LEVEL 3

UFD4200

On the stowage compartment lower side, remove the bolts and washers on support plates "F" and junction plates "D". Disconnect the turnbuckles at support plates "F" and attachment point "G". Support the stowage compartment. Inside the compartment, remove the pin at upper attachment points "A" and "H", Remove the overhead stowage compartment.

EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION - OVERHEAD STOWAGE COMPARTMENTS EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION PSIUs

TMUESCB01-T03 LEVEL 3

UFD4200

To remove the Passenger Service Information Unit, apply the following the procedure: Open and safety the corresponding circuit breakers, Remove the mounting seal each side of the PSIU, Push the PSIU up to release the hinges from the mounting rail, Disconnect the electrical connectors, Remove the PSIU. NOTE : For installation use the tool pulley assembly to insert the rubber seal properly.

EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION - PSIUs EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION COVE LIGHT PANELS

TMUESCB01-T04 LEVEL 3

UFD4200

To remove the cove light panel, apply the following procedure : - Remove the seal from the rail at the junction with the overhead stowage compartment, - Move the panel to disconnect it from the rail, - Remove the bonding strap, - Lift the panel, and pull it out.

EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION - COVE LIGHT PANELS EFFECTIVITY EFFECTIVITY ALL

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UPPER SIDEWALL PANELS

LOWER SIDEWALL PANELS

To remove the upper sidewall panel apply the following procedure : - First, remove the passenger seats in the area of the upper sidewall panel which is to be removed, - Remove the decor cover and the inner pane from the window, - Remove the 2 screws fitted on each window, - Pull out the lining strips, - Lift the panel to release it from the mounting brackets and remove it.

To remove the lower sidewall panel, apply the following procedure : - Use a punch to release the center pins of the quick release pins, - Pull the lower edge of the panel away from the compartment wall, - Pull the panel down and remove the fasteners from the attachment fittings, - Remove the panel.

TMUESCB01-T05 LEVEL 3

UFD4200

CABIN PANEL REMOVAL/INSTALLATION

EFFECTIVITY EFFECTIVITY ALL

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CABIN PANEL REMOVAL/INSTALLATION - UPPER AND LOWER SIDEWALL PANELS EFFECTIVITY EFFECTIVITY ALL

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TMUESCB01 LEVEL 3

UFD4200

THIS PAGE INTENTIONALLY LEFT BLANK

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-20-00 CABIN EQUIPMENT AND FURNISHING COMPONENTS

TMUESCE01 LEVEL 3

UFD4200

CONTENTS: Ceiling Panels Overhead Stowage Compartments Passenger Service Information Units (PSIUs) Cove Light Panels Upper Sidewall Panels Lower Sidewall Panels Cabin Attendant Seats Passenger seats

EFFECTIVITY EFFECTIVITY ALL

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CEILING PANELS

OVERHEAD STOWAGE COMPARTMENTS

IDENTIFICATION FIN: TBD

IDENTIFICATION FIN: TBD

LOCATION ZONE: 230, 250, 220, 260

LOCATION ZONE: 200

TMUESCE01-T01 LEVEL 3

UFD4200

CABIN EQUIPMENT AND FURNISHING COMPONENTS

EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS - CEILING PANELS - OVERHEAD STOWAGE COMPARTMENTS EFFECTIVITY EFFECTIVITY ALL

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PASSENGER SERVICE INFORMATION UNITS (PSIUs)

COVE LIGHT PANELS

IDENTIFICATION FIN: TBD

IDENTIFICATION FIN: TBD

LOCATION ZONE: 200

LOCATION ZONE: 200

TMUESCE01-T02 LEVEL 3

UFD4200

CABIN EQUIPMENT AND FURNISHING COMPONENTS

EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS - PASSENGER SERVICE INFORMATION UNITS (PSIUs) COVE LIGHT PANELS EFFECTIVITY EFFECTIVITY ALL

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UPPER SIDEWALL PANELS

LOWER SIDEWALL PANELS

IDENTIFICATION FIN: TBD

IDENTIFICATION FIN: TBD

LOCATION ZONE: 200

LOCATION ZONE: 200

TMUESCE01-T03 LEVEL 3

UFD4200

CABIN EQUIPMENT AND FURNISHING COMPONENTS

EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS - UPPER SIDEWALL PANELS - LOWER SIDEWALL PANELS EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS CABIN ATTENDANT SEATS IDENTIFICATION FIN: TBD

TMUESCE01-T04 LEVEL 3

UFD4200

LOCATION ZONE: 220, 240, 260

EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS - CABIN ATTENDANT SEATS EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS PASSENGER SEATS IDENTIFICATION FIN: TBD

TMUESCE01-T05 LEVEL 3

UFD4200

LOCATION ZONE: 200

EFFECTIVITY EFFECTIVITY ALL

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CABIN EQUIPMENT AND FURNISHING COMPONENTS - PASSENGER SEATS EFFECTIVITY EFFECTIVITY ALL

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TMUESCE01 LEVEL 3

UFD4200

THIS PAGE LEFT INTENTIONALLY BLANK.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-60-00 ESCAPE FACILITY PRESENTATION

TMUESEP05 LEVEL 1

UFD4200

CONTENTS: General Cockpit Passenger Door Slide Emergency Exit Slide Slide Installation Self Examination

EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION GENERAL

EMERGENCY EXIT SLIDE

Escape facilities are provided for passenger and crew evacuation. They are located in the cockpit and in the cabin.

The two emergency exits of each side are equipped with a dual lane offwing escape slide. The four emergency exits provide quick evacuation for the passengers. The dual lane escape slide operates automatically if one door of each side is opened in ARMED mode.

COCKPIT In case of emergency evacuation, there are two possibilities for the flight crew to evacuate the cockpit. The simplest emergency evacuation procedure for the flight crew is to go through the cockpit door and use the passenger door slide. If necessary a secondary means enables the flight crew to evacuate the cockpit by opening the sliding windows and using the escape ropes stowed in the ceiling. PASSENGER DOOR SLIDE

TMUESEP05-T01 LEVEL 1

UFD4200

Single lane escape slides are installed on each passenger door. They provide quick evacuation for the passengers and the crew in an emergency evacuation and operate automatically if the door is opened in ARMED mode.

EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION SLIDE INSTALLATION

TMUESEP05-T02 LEVEL 1

UFD4200

Escape slides are installed at all the aircraft exits. The passenger door escape slide and its inflation reservoir are located in a container at the bottom of the door. The emergency exit escape slide is located in a container above the wing in each wing-to-fuselage fairing, and the inflation reservoirs are installed in the AFT cargo compartment, behind the sidewall panels.

EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUESEP05 LEVEL 1

UFD4200

Where is the inflation reservoir of the escape slide of emergency exit located ? A - In a container at the bottom of the door. B - In the overhead stowage compartment over the door. C - In the cargo compartment.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-60-00 ESCAPE FACILITY PRESENTATION

TMUESEP04 LEVEL 1

UFD4200

CONTENTS: General Cockpit Passenger Door Slide Emergency Exit Slide Slide Installation Self Examination

EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION GENERAL

EMERGENCY EXIT SLIDE

Escape facilities are provided for passenger and crew evacuation. They are located in the cockpit and in the cabin.

The four emergency exits are equipped with a single lane escape slide. The four emergency exits provide quick evacuation for the passengers. The single lane escape slides operates automatically if the door is opened in ARMED mode.

COCKPIT In case of emergency evacuation, there are two possibilities for the flight crew to evacuate the cockpit. The simplest emergency evacuation procedure for the flight crew is to go through the cockpit door and use the passenger door slide. If necessary a secondary means enables the flight crew to evacuate the cockpit by opening the sliding windows and using the escape ropes stowed in the ceiling. PASSENGER DOOR SLIDE

TMUESEP04-T01 LEVEL 1

UFD4200

Single lane escape slides are installed on each passenger door. They provide quick evacuation for the passengers and the crew in an emergency evacuation and operate automatically if the door is opened in ARMED mode.

EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION SLIDE INSTALLATION

TMUESEP04-T02 LEVEL 1

UFD4200

Escape slides are installed at all the aircraft exits. The passenger door escape slide and its inflation reservoir are located in a container at the botton of the door. The emergency exit escape slide is located in a container under the door and the inflation reservoir is over the door in the overhead stowage compartment.

EFFECTIVITY EFFECTIVITY ALL

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ESCAPE FACILITY PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUESEP04 LEVEL 1

UFD4200

Where is the inflation reservoir of the escape slide of emergency exit located ? A - In a container at the botton of the door. B - In the overhead stowage compartment over the door. C - In the cargo compartment.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-60-00 MISCELLANEOUS EMERGENCY EQUIPMENT PRESENTATION

TMUESEE03 LEVEL 1

UFD4200

CONTENTS: General Fire Extinguisher Oxygen Kit Smoke Hood Crash Axe First Aid Kit Megaphone Emergency Radio Beacon Flash Light Life Vest Manual Release Tool Self Examination

EFFECTIVITY EFFECTIVITY ALL

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MISCELLANEOUS EMERGENCY EQUIPMENT PRESENTATION GENERAL

OXYGEN KIT

The emergency equipment is kept in different locations in the cockpit and the cabin. Emergency equipment is composed of : - Fire extinguisher, - Oxygen kit, - Smoke hood, - Crash axe, - First aid kit, - Megaphone, - Emergency radio beacon, - Flash light, - Life vest, - Manual release tool. NOTE: The exact quantity and location of these items depend on individual airline configuration and cabin layout.

The portable oxygen equipment is installed in the passenger cabin to supply oxygen to the passengers in an emergency.

TMUESEE03-T01 LEVEL 1

UFD4200

FIRE EXTINGUISHER The portable fire extinguishers are used to extinguish any fire in the cockpit and cabin. They are fitted under the attendant seats in the passenger compartment and in the cockpit next to the third occupant seat

SMOKE HOOD The flight crew emergency breathing hood system provides protection to the eyes and respiratory system for crew members. Smoke masks are also supplied for the cabin attendants to fight a fire or, against the emission of smoke and noxious gases. CRASH AXE The crash axe is used to cut through light structures, panels and windows to get access or exit in an emergency. The insulated handle is resistant to high voltages. FIRST AID KIT First aid kits are kept near forward and aft attendant stations, in overhead stowage compartments. MEGAPHONE A megaphone is stowed in the left forward and aft attendant stations.

EFFECTIVITY EFFECTIVITY ALL

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MISCELLANEOUS EMERGENCY EQUIPMENT PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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MISCELLANEOUS EMERGENCY EQUIPMENT PRESENTATION EMERGENCY RADIO BEACON An emergency radio beacon is stowed in the left aft attendant station. FLASH LIGHT Hand held flash lights are installed as movable light sources. They are used if bad light conditions occur during an on-board emergency. LIFE VEST One passenger life vest is stowed under each passenger seat. Life vest components include : - a CO2 gas inflation system, - an oral inflation tube, - a lamp for survivor location in poor visibility or night conditions, - a water activited cell (battery) to supply the lamp, - a whistle to attract attention

TMUESEE03-T02 LEVEL 1

UFD4200

MANUAL RELEASE TOOL Manual release tools, used to open the passenger oxygen mask doors, are available at each cabin attendant station.

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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SELF EXAMINATION

TMUESEE03 LEVEL 1

UFD4200

Smoke hoods are supplied for the cabin attendants to: A - supply oxygen for passengers. B - fight a fire or against emission of smoke or noxious gases. C - breathe oxygen.

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25 - EQUIPMENT/FURNISHINGS 25-62-00 PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENT

TMUESFB03 LEVEL 3

UFD4200

CONTENTS: Passenger Door Escape Slide Description/Deployment

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENT

TMUESFB03-T01 LEVEL 3

UFD4200

Passenger Door Escape Slide Description/Deployment A slide deployment can be initiated when ever the door is opened in the emergency configuration When the slide is armed it can be checked on a red indicator, located on the button of the slide decorative cover. As soon as the door handle is lifted the door opens and the escape slide is ejected from its container and the inflation system is activated. The deployment and inflation sequence is automatically initiated when the cabin door is opened. The slide deploys into its final usable position within 3 seconds. The escape slide is connected to the cabin floor by a girt extension which is attached to the girt bar at the door sill. Should the escape slide not inflate automatically a red manual inflation handle must be pulled. This handle is located on the girt extension. Let’s have a look at the inflation system. The system is automatically activated as soon as the slide is ejected from its container. The valve regulator assembly incorporates a direct reading, temperature compensated pressure gage, which indicates the gas charge in the inflation reservoir, relative to ambient temperature. The gas stored within the inflation reservoir is discharged into the inflatable through flexible hoses and an aspirator. Ambient air is drawn in, through the flaps of the aspirator by the partial vacuum, created by the high velocity in the venturi.

EFFECTIVITY EFFECTIVITY ALL

Then the flaps close and the remaining gas charge tops the inflatable up to its operating pressure. Inflation is therefore rapid and reservoir size is maintained at minimum. Restraint devices are used to control the deployment sequence. The primary restraint mechanism is a precision fuse frangible link, which separates at a predetermined force value. In case of pressure loss, no fail handles, located on both side of the runway end, allow the inflation to be used as a hand-held evacuation chute. In the event of a ditching, grasp lines are fitted around the outside of the inflatable to facilitate the use of slide as a flotation device. The slide is equipped with a lighting system. The lights located along the side tubes and across the runway, are supplied from the aircraft emergency power supply units. The lights are automatically supplied with power when the slide is deployed. The escape slide can be disconnected from the aircraft floor whenever necessary. For the disconnection the following steps must be taken. Lift the flap of the girt extension to gain access to the white disconnect handle. Pull the handle. The girt extension incorporates a quick release feature, a daisy chain, which permits rapid detachment of the inflatable from the aircraft.

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PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENT EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE DESCRIPTION/DEPLOYMENT

TMUESFB03-T01 LEVEL 3

UFD4200

Once detached from the floor the inflatable drops from the aircraft but remains attached to the girt bar by means of a string, which must be cut by using the knife located next to it, on the girt extension. The inflatable is then completely disconnected from the aircraft.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 PASSENGER DOOR ESCAPE SLIDE DISCONNECTION

TMUESFG02 LEVEL 3

UFD4200

CONTENTS: Passenger Door Escape Slide Disconnection

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE DISCONNECTION Passenger Door Escape Slide Disconnection

TMUESFG02-T01 LEVEL 3

UFD4200

Disconnect the electrical line. Tie the retaining cord to the slide handle. Disconnect the slide attaching device by removing the safety pin. Undo the lacing system. Remove the girt bar by unlocking the door threshold supports. Using the retaining cord, take the escape slide away.

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE DISCONNECTION EFFECTIVITY EFFECTIVITY ALL

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TMUESFG02 LEVEL 3

UFD4200

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25 - EQUIPMENT/FURNISHINGS 25-62-00 PASSENGER DOOR ESCAPE SLIDE INSTALLATION

TMUESFA03 LEVEL 3

UFD4200

CONTENTS: Passenger Door Escape Slide Installation

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE INSTALLATION PASSENGER DOOR ESCAPE SLIDE INSTALLATION

TMUESFA03-T01 LEVEL 3

UFD4200

Check that door emergency opening percussion system behind the door support arm, is in the disarmed position. First, connect the electrical line... place it on the right-hand side or left-hand side according to the door. Fit the girt bar into the mooring line and slide it into the slide attaching device. Connect to the standby percussion system. Connect to the normal percussion system. Fit the slide assembly into the door slide hooks. Connect to electrical connector. Screw the container in place. Arm the slide system. Lift the door... and close the door again. Fit the girt bar into the door threshold supports. Close the door and check the slide mechanism is correct. Lift the door and check that the slide mechanism is properly attached to the door. Remove the safety pin from the slide percussion system. Fit the slide cover.

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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25 - EQUIPMENT/FURNISHING 25-61-00 PASSENGER DOOR ESCAPE SLIDE RAFT DESCRIPTION / DEPLOYMENT

TMUESRB01 LEVEL 3

UFD4200

CONTENTS: Description Normal Operation Manual Operation

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE RAFT DESCRIPTION / DEPLOYMENT NOTE : In this module the PASSENGER DOOR SLIDE DESCRIPTION / DEPLOYMENT is described on the A320 but the principle is the same for the A319 and the A321. DESCRIPTION The forward and rear cabin doors of the A320 are equipped with slide rafts. The inflation and deployment sequence is automatically initiated when the door is opened in armed configuration. The slide raft is ejected out of its container, and remains folded by restraint devices which break at determined pressure points to allow correct deployment. The slide raft is stowed in a container connected to the cabin door.

TMUESRB01-T01 LEVEL 3

UFD4200

NORMAL OPERATION As soon as the door handle is lifted, the door is pneumatically pushed open and the slide raft, fixed with a girt bar to the cabin floor, is pulled out of the container, drops down and inflates automatically. As the inflatable falls down, the inflation system is activated. The gas stored in the inflation cylinder is discharged through flexible hoses to the aspirators. The aspirator flaps open and ambient air is drawn in under partial vaccum, created by the high velocity in the venturi. Then the flaps close and the remaining gas, tops up the inflatable to its operational pressure.

EFFECTIVITY EFFECTIVITY ALL

Should the automatic inflation system fail, the slide raft must be inflated manually. MANUAL OPERATION For that, the red manual inflation handle located on the right hand side of the girt extension must be pulled. A lighting system is fitted on both sides and on the runway end of the inflatable. The power supply for this lighting system is provided by the cabin emergency power supply units. Two assist handles are located on both sides at the lower end of the inflatable, to allow assisting people to hold on. In case of a ditching, prior to door opening the survival kit must be connected to the slide raft. The survival kit is stored in the nearest overhead bin. Place the survival kit on the floor, forward of the door, detach the lanyard from the girt bar. Pull the lanyard and the hook, to snap on front of the survival kit. Then open the door. The slide raft drops out of the container and deploys.

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PASSENGER DOOR ESCAPE SLIDE RAFT DESCRIPTION / DEPLOYMENT EFFECTIVITY EFFECTIVITY ALL

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TMUESRB01 LEVEL 3

UFD4200

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25 - EQUIPMENT/FURNISHING 25-61-00 PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.

TMUESRG01 LEVEL 3

UFD4200

CONTENTS: PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION.

TMUESRG01-T01 LEVEL 3

UFD4200

PASSENGER DOOR ESCAPE SLIDE RAFT DISCONNECTION. Disconnect the pack-assembly electrical supply. The quick-disconnect connector is installed below the cable routing velcro. Open the girt flap. Open the lanyard velcro and remove the survival kit attach-loop from the telescopic end fitting of the girt bar. Open the blue and the green velcros and separate the survival kit lanyard and the girt bar release-strap. Remove the girt bar release-strap from the girt bar release-lever. Pull the mooring line from the girt pocket and support the escape slide raft with the mooring line. Pull the release handle, release the mooring line slowly and let the girt lace-up joint and the girt assembly release from the girt bar. Carefully lower the escape slide raft to the ground. Make sure that you do not damage the reservoir when you lower the slide raft to the ground. Hold the girt bar and push in the girt bar release-lever by hand. Remove the girt bar from the floor attach fittings. Remove the mooring line loop-end from the girt bar and keep the girt bar with the aircraft. Lift the empty pack assembly soft-cover clear of the passenger/crew door and close the door. Remove the pack assembly decorative-cover and keep it with the aircraft. Loosen the link nut and remove and retain the attach link and the pull-handle from the stud assembly. Remove the stud assemblies, with the allen key, from the door attach anchor nuts.

EFFECTIVITY EFFECTIVITY ALL

Move the packboard inboard on its supports and hold it. Disconnect the pack assembly connector from the electrical connector installed on the passenger/crew door. Remove the packboard from the passenger crew door supports. Service the door damper and emergency operation cylinder.

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TMUESRG01 LEVEL 3

UFD4200

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25 - EQUIPMENT/FURNISHING 25-61-00 PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.

TMUESRA01 LEVEL 3

UFD4200

CONTENTS : PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.

TMUESRA01-T01 LEVEL 3

UFD4200

PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION. Make sure that the operation striker lever of the door damper and emergency operation cylinder is in the DISARMED position. Make sure that the passenger/crew door on which you will install the pack assembly is closed and locked. Make sure that the emergency control handle is in the DISARMED position and that the safety pin is installed. Make sure that the lockpin assembly is installed in the operating head of the slide raft inflation reservoir. Check the pack electrical supply-cable, and make sure that the cable is installed for the left door or the right door as required. Make sure that the short girt flap is on the top of the long girt flap. Attach a temporary tie to the small cord loop. Put the girt bar in place. Make sure that the girt bar end fittings point away from the slide raft pack, and that the telescopic end is in the forward position in relation to the aircraft. Install the mooring line loop on the girt bar rear end. Pull the cord loops attached to the long girt flap up through the grommets in the short girt flap. Put the loops through each other from each end of the girt towards the center. Put the parachute pin through the small cord loop and remove and discard the temporary tie. Safety the parachute pin in position with nylon thread with a breaking strain.

EFFECTIVITY EFFECTIVITY ALL

Put the girt bar release strap through the girt bar release lever and position the release strap along the slide raft girt. Attach the survival kit lanyard to the release strap with the same color velcros and position the lanyard along the slide raft girt. Fold the long girt flap over the girt bar and attach it to the short girt flap velcro attach strips. Lift the slide raft pack assembly onto the passenger/crew door supports. Carefully move the packboard assembly inboard at an angle onto its supports and hold it. Connect the pack assembly connector on the electrical connector on the passenger/crew door. Move the pack assembly in position and install the stud assemblies in the door attach anchor nuts. Carefully tighten the two stud assemblies with the allen key, until there is no play between the door and packboard assembly. Connect the two pull handles to the stud assemblies with the attach links. Remove the safety pin from the emergency control handle and set the handle to the ARMED position. Hold the passenger/crew door to prevent it moving outboard and set the door control handle to the OPEN position. Install the girt bar into the floor attach fittings. Slowly move the door control handle to CLOSED position, and move the emergency control handle to the DISARMED position. Set the door control handle to the OPEN position.

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PASSENGER DOOR ESCAPE SLIDE RAFT INSTALLATION.

TMUESRA01-T02 LEVEL 3

UFD4200

PASSENGER (Cont‘d)

DOOR

ESCAPE

SLIDE

RAFT

INSTALLATION.

Make sure that the control shaft levers and the telescopic forks on the door have engaged correctly with the girt bar. Set the door control handle to the CLOSED position, and set the emergency control handle to the ARMED position. Hold the passenger/crew door to prevent it moving outboard and set the door control handle to the OPEN position. Make sure that the girt bar has engaged correctly with the floor attach fittings. Set the door control handle to the CLOSED position. Set the emergency control handle to the DISARMED position and install the safety pin. Remove the lockpin assembly from the operating head of the slide raft inflation reservoir and put the lockpin assembly in the stowage pocket installed on the pack assembly soft-cover. Put the pack assembly decorative-cover in position. Connect the cover attach straps. Check the indication of the decorative cover bracket and girt-bar visual indicator. Make sure that the operation striker lever of the door damper and emergency operation cylinder is in the ARMED position.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 OFFWING ESCAPE SLIDE DEPLOYMENT

TMUESFC01 LEVEL 3

UFD4200

CONTENTS: Offwing Escape Slide Deployment

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE DEPLOYMENT

TMUESFC01-T01 LEVEL 3

UFD4200

NOTE : In this module the OFFWING ESCAPE SLIDE DEPLOYMENT is described on the A320 but the principle is the same for the A319. The offwing escape slide is packed in a container assembly, which in turn is mounted into the centre fuselage belly fairing. Two type "3" exits are located over each wing and are always in armed configuration. Two emergency lights underneath the wing exits light the escape way leading to the escape slide which is pointed out with red fluorescent arrows. The opening of one wing exit will initiate the deployment sequence. The escape slide is ejected out of its, container and deploys in approximately four seconds. The inflation system consists of an inflation cylinder, which is located in the aft cargo compartment. Activation of the release mechanism initiates the inflation sequence. The gas stored in the cylinder is discharged to the inflatable slide through flexible hoses and an aspirator. The aspirator flaps open and ambient air is drawn into the slide. The slide remains folded by restraint devices, which break at a predetermined force, to permit correct deployment. Two black arrows located on the ramp section indicate the direction of the escape route. A lighting system is provided on the slide. The lights are located on the ramps along the side tubes and across the runway end.

EFFECTIVITY EFFECTIVITY ALL

A red manual inflation handle, located in each exit frame, must be pulled to manually activate the inflation and deployment sequence, in case of automatic release failure. If the slide is deployed but not inflated, it still can be used as a hand-held escape chute. On the ramp section top, a hook is located and this hook must be connected to an attachment fitting on the wing. Two red NO FAIL HANDLES are located on both sides of the escape slide on the runway end. Four able bodied men must hold the deflated slide extended, by means of the no fail handles, to allow the passengers on the wing to descend.

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OFFWING ESCAPE SLIDE DEPLOYMENT EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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25 - EQUIPMENT/FURNISHINGS 25-62-00 OFFWING ESCAPE SLIDE REMOVAL

TMUESFE01 LEVEL 3

UFD4200

CONTENTS: Offwing Escape Slide Removal

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE REMOVAL

TMUESFE01-T01 LEVEL 3

UFD4200

NOTE : In this module the OFFWING ESCAPE SLIDE REMOVAL is described on the A320 but the principle is the same for the A319. Push in the flapper valves of the aspirator and release the pressure from the offwing escape slide. Disconnect the inflation hose from the stowage compartment union. Disconnect the electrical connectors at the emergency lighting supply cable. Undo the strap press-studs, to separate the container panel from the escape slide. To release the TOP girt bar assembly, support the slide and open the girt flap. Remove the girt release handle, and pull it. Undo the laces. Follow the same procedure to release the LOWER and FORWARD girt assemblies. Carefully lower the offwing escape slide to the ground. Remove and retain the seal attach plate screws. Remove and retain the seal attach plate and the seal strips. Loosen the attach panel studs. Move the top of the stowage compartment outboard at an angle and hold it. Disconnect the inflation hose from the fuselage union. Disconnect the emergency lighting electrical connector, and remove the escape slide stowage compartment from the aircraft. The inflation reservoir has to be replaced.

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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25 - EQUIPMENT/FURNISHINGS 25-62-00 OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION

TMUESFL01 LEVEL 3

UFD4200

CONTENTS: Removal Installation Test

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION REMOVAL WARNING Make sure that the lockpin assembly is correctly installed in the valve assembly head of the inflation cylinder to prevent an accidental extension of the escape slide. The cylinder is pressurized with gas to 3000 psi (207 bar). The removal/installation procedures of the left and right cylinders are almost identical. ACCESS Open the AFT cargo door. Put the access platform in position. Remove the access panels. Open the circuit breakers. Install the lockpin on the cylinder valve assembly. NOTE: The lockpin is stowed in the stowage pocket.

TMUESFL01-T01 LEVEL 3

UFD4200

CABLE ASSEMBLIES Loosen the knurled sleeve nut and remove the two collets. Move the two cable assemblies apart.

CYLINDER REMOVAL Remove and keep the bolt that supports the flexible hose assembly. Loosen the attach clamp screws. Remove the inflation cylinder. INSTALLATION CYLINDER INSTALLATION Make sure that the lockpin assembly is correctly installed in the valve assembly head of the inflation cylinder to prevent an accidental extension of the escape slide. Install the cylinder assembly in the support bracket. Tighten the attach clamp screws when in position. FLEXIBLE HOSE ASSEMBLIES Put the flexible hose assembly in position and tighten the bolt by hand. Remove the blanking caps and connect the flexible hose to the bulkhead union. Tighten the bolt. ELECTRICAL CONNECTOR Remove the blanking caps and install the electrical connector.

ELECTRICAL CONNECTOR Disconnect and put blanking caps on the electrical connectors. FLEXIBLE HOSE ASSEMBLY Disconnect the flexible hose assembly from the bulkhead union. Put blanking plugs on the disconnected line ends.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE CYLINDER REMOVAL/INSTALLATION TEST ADJUSTMENT After test tool installation and setting the cursor to zero, (adjusting the flexible assembly nuts if necessary) set the emergency exit hatch in armed position and remove it. Remove the cap and connect the RELEASE TEST TOOL and CABLE ESCAPE SLIDE adapter to the flexible control assembly. Set the cursor to zero. Put the forward emergency exit-hatch in the armed position and remove the hatch. Make sure that the test tool cursor has moved to show a minimum indication of 50 mm (1.9685 in.). Adjust conduit, adjust nuts on the flexible control assembly. Make an adjustment of the conduit length. Set the cursor on the test tool to zero.

CLOSE UP Install the access panels. Remove the platform. Close the cargo doors.

TMUESFL01-T01 LEVEL 3

UFD4200

CABLE ASSEMBLIES Connect the two cable assemblies. Install the two collets and tighten the knurled sleeve nut. FUNCTIONAL CHECK Lift the door lever up to check that the resistance and the play between the flexible control and release cable assembly are satisfactory. LOCKPIN ASSEMBLY Remove the lockpin from the cylinder and put it in the stowage pocket.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 OFFWING ESCAPE SLIDE INSTALLATION

TMUESFD01 LEVEL 3

UFD4200

CONTENTS: Offwing Escape Slide Installation

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INSTALLATION NOTE : In this module the OFFWING ESCAPE SLIDE INSTALLATION is described on the A320 but the principle is the same for the A319.

TMUESFD01-T01 LEVEL 3

UFD4200

Put the escape slide stowage compartment in position. Move the top of the stowage compartment outboard at an angle and hold it. Connect the inflation hose to the fuselage union. Connect the emergency lighting electrical connector. Put the stowage compartment in position and tighten the attach panel studs. Put the seal strips and the seal attach plate in position and install and tighten the screws.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INSTALLATION EFFECTIVITY EFFECTIVITY ALL

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TMUESFD01 LEVEL 3

UFD4200

THIS PAGE INTENTIONALLY LEFT BLANK

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 EMERGENCY EQUIPMENT/ EMERGENCY EXIT ESCAPE SLIDE DESCRIPTION/DEPLOYMENT

TMUESES05 LEVEL 3

UFD4200

CONTENTS: Description/Deployment

EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT/ EMERGENCY EXIT ESCAPE SLIDE DESCRIPTION/DEPLOYMENT The escape slide for the type "C" doors, is stored underneath the door inside the fuselage. The inflation cylinder is located in the overhead bin, over the door.

The escape slide for the type "C" doors is stowed in a special compartment in the fuselage, underneath the door.

The cylinder is in a protection box and can be seen through a plexiglass window.

The deployment sequence starts as soon as the door is opened in armed configuration.

The pressure can be checked on the pressure level indicator. For correct pressure the needle must be in the green section.

One aspirator is connected to the inflation cylinder by means of a flexible hose.

To initiate the slide deployment, the door must be opened in the armed configuration.

TMUESES05-T01 LEVEL 3

To open the door, uncover the control handle, lift the handle fully up, and release!

UFD4200

The transparent protective cover must be taken off and the red handle pulled to initiate the manual slide inflation.

The door opens outwards. The escape slide in the meantime inflates and deploys completely. The escape slide is ready for use when the door is locked in the fully open position.

During the door opening the inflation cylinder regulator value is actuated, and primary gas is supplied to the aspirator. The aspirator flaps open and outside air is drawn in. The flaps close as soon as the correct pressure is reached. The slide has a single lane sliding surface with a brake path at the bottom end, which slows down the speed of the evacuees.

Should the door open but the escape slide not inflate, a red handle for manual inflation is located in the door upper right hand frame.

EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT - EMERGENCY EXIT ESCAPE SLIDE - DESCRIPTION/DEPLOYMENT EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT/ EMERGENCY EXIT ESCAPE SLIDE A lighting system is fitted along both sides and at the bottom of the slide. The lights automatically come on during the slide deployment. They remain on as long as the emergency power supply operates. A reentry strap is fixed on one side of the slide. A yellow life line is fixed along the outside of the inflation chambers on both sides. Red no-fail handles are located on both sides for assisting people to hold the slide in case it is used not inflated as an evacuation chute.

TMUESES05-T01 LEVEL 3

UFD4200

The slide is slightly canted in order to deploy at safe distance away from the engine.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 EMERGENCY EQUIPMENT EMERGENCY EXIT ESCAPE SLIDE DISCONNECTION

TMUESED05 LEVEL 3

UFD4200

CONTENTS: Disconnection

EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT EMERGENCY EXIT ESCAPE SLIDE DISCONNECTION The disconnect handle and a knife are located on the girt extension close to the door step. The knife is on the left hand side in a clearly marked pouch. A disconnect handle is located under a velcro flap marked "FOR DITCHING USE". To release the slide, lift the flap, grasp the white handle and pull. Should the slide not drop immediately, push down on the girt extension. The daisy-chain on the packboard releases, and the slide is free to drop. The slide remains attached to the aircraft by means of a mooring line.

TMUESED05-T01 LEVEL 3

UFD4200

This line must be cut by means of the hook knife.

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EMERGENCY EQUIPMENT - EMERGENCY EXIT ESCAPE SLIDE - DISCONNECTION EFFECTIVITY EFFECTIVITY ALL

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TMUESED05 LEVEL 3

UFD4200

THIS PAGE LEFT INTENTIONALLY BLANK.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 PASSENGER DOOR ESCAPE SLIDE INFLATION CYLINDER CHECK

TMUESFJ01 LEVEL 3

UFD4200

CONTENTS: Pressure Gauge Self Examination

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE INFLATION CYLINDER CHECK PRESSURE GAUGE

TMUESFJ01-T01 LEVEL 3

UFD4200

A pressure gauge viewing window is located on the cover protecting the escape slide. It allows the check of the cylinder pressure. The indication must be in the green GO band.

EFFECTIVITY EFFECTIVITY ALL

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PASSENGER DOOR ESCAPE SLIDE INFLATION CYLINDER CHECK EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUESFJ01 LEVEL 3

UFD4200

Where must the pressure indication be? A - In the green GO band. B - In the red band. C - At zero.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK

TMUESFN01 LEVEL 3

UFD4200

CONTENTS: Cylinder Pressure Check (From Cargo Compartment) Cylinder Pressure Check From PTP (Low Press Configuration) Cylinder Pressure Check From PTP (Press OK Configuration) Self Examination

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK CYLINDER PRESSURE CHECK (FROM CARGO COMPARTMENT)

TMUESFN01-T01 LEVEL 3

UFD4200

A pressure gauge is installed on the cylinder valve assembly. The pressure gauge indicator arrow must be in the green GO band.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK CYLINDER PRESSURE CHECK (FROM CARGO COMPARTMENT) EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK CYLINDER PRESSURE CONFIGURATION)

CHECK

FROM

PTP

(LOW

PRESS

TMUESFN01-T02 LEVEL 3

UFD4200

The SYSTEM STATUS line key must be pressed to check the slide pressure. SLIDES PRESS LOW line key is pressed to get the information messages. The slides where the pressure is low are displayed on the screen.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK CYLINDER PRESSURE CHECK FROM PTP (LOW PRESS CONFIGURATION) EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK CYLINDER PRESSURE CONFIGURATION)

CHECK

FROM

PTP

(PRESS

OK

TMUESFN01-T03 LEVEL 3

UFD4200

The SYSTEM STATUS line key must be pressed to see the slide pressure. If the pressure is ok, the SLIDES PRESS OK message appears.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE INFLATION CYLINDER CHECK CYLINDER PRESSURE CHECK FROM PTP (PRESS OK CONFIGURATION) EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUESFN01 LEVEL 3

UFD4200

From where is the inflation cylinder checked? A - From the cargo compartment only. B - From the PTP only. C - From the cargo compartment or from the PTP.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-62-00 OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION

TMUDOFR01 LEVEL 1

UFD4200

CONTENTS: General Latch Pin Manual Release Handles Release Cable Path

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION GENERAL

TMUDOFR01-T01 LEVEL 1

UFD4200

The escape slide release mechanism consists of three different portions: - the latch pin, - the manual release handles, - the release cable path.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - GENERAL EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION LATCH PIN

TMUDOFR01-T02 LEVEL 1

UFD4200

The latch pin has two positions, the normal "armed" position and a retracted position used for maintenance operations. Using a hexagonal socket wrench, the latch pin can be pushed into the normal "armed"position and locked in this position by rotating it quater of a turn.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - LATCH PIN EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION MANUAL RELEASE HANDLES

TMUDOFR01-T03 LEVEL 1

UFD4200

In case of failure the slide can be released manually with the manual release handles, via the catch lever. The release lever is operated by the latch pin in armed position, upon inward removal of the hatch. This movement, via the shaft, rod, spring rod, and double lever, pulls the release cable.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - MANUAL RELEASE HANDLES EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION RELEASE CABLE PATH

TMUDOFR01-T04 LEVEL 1

UFD4200

The release cable transmits the double lever movement to the connection point in the aft cargo compartment where it is connected to the escape slide cylinder.

EFFECTIVITY EFFECTIVITY ALL

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OFFWING ESCAPE SLIDE RELEASE MECHANISM DESCRIPTION - RELEASE CABLE PATH EFFECTIVITY EFFECTIVITY ALL

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TMUDOFR01 LEVEL 1

UFD4200

THIS INTENTIONALLY LEFT BLANCK

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-60-00 EMERGENCY EQUIPMENT COMPONENTS

TMUESFZ03 LEVEL 3

UFD4200

CONTENTS: Passenger Doors-Escape Slide Emergency Exits-Escape Slide Emergency Exits-Inflation Cylinders Escape Ropes

EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT COMPONENTS PASSENGER DOORS-ESCAPE SLIDE IDENTIFICATION FIN: 7500MM, 7501MM, 7502MM, 7503MM LOCATION ZONE: 831, 841, 832, 842 EMERGENCY EXITS-ESCAPE SLIDE IDENTIFICATION FIN: 7504MM, 7505MM

TMUESFZ03-T01 LEVEL 3

UFD4200

LOCATION ZONE: 193, 194

EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT COMPONENTS-ESCAPE SLIDES EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT COMPONENTS EMERGENCY EXITS-INFLATION CYLINDERS IDENTIFICATION FIN: 7506MM, 7507MM

TMUESFZ03-T02 LEVEL 3

UFD4200

LOCATION ZONE: 151, 152

EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT COMPONENTS-INFLATION CYLINDERS EFFECTIVITY EFFECTIVITY ALL

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EMERGENCY EQUIPMENT COMPONENTS ESCAPE ROPES IDENTIFICATION FIN: 1MM, 2MM

TMUESFZ03-T03 LEVEL 3

UFD4200

LOCATION ZONE: 211, 212

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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EMERGENCY EQUIPMENT COMPONENTS-ESCAPE ROPES EFFECTIVITY EFFECTIVITY ALL

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TMUESFZ03 LEVEL 3

UFD4200

THIS PAGE LEFT INTENTIONALLY LEFT BLANK

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-50-00 CARGO COMPARTMENT PRESENTATION

TMUECLP08 LEVEL 1

UFD4200

CONTENTS: General FWD Cargo Compartment AFT Cargo Compartment Bulk Cargo Compartment Access

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT PRESENTATION GENERAL

BULK CARGO COMPARTMENT

The lower deck is divided into three cargo compartments. The different cargo compartments are: - The FWD cargo, - The AFT cargo, - The Bulk cargo compartment. The FWD and AFT cargo compartments can be optionally equipped with a semi-automatic cargo loading system. Basically they have tie-down/attachment points for the nets and straps which keep the bulk cargo in place.

The Bulk cargo compartment can only be loaded with bulk and loose baggage A divider net with a screen separates the bulk cargo compartment from the AFT cargo compartment.

FWD CARGO COMPARTMENT The FWD cargo compartment is basically equipped to be loaded with bulk and loose baggage. The optional semi-automatic cargo loading system transports pallets and containers and is operated from a control panel installed on the cargo door.

ACCESS Access to the FWD, Aft and Bulk cargo compartments is gained by two outwards opening doors. Access to the bulk cargo compartment can also be gained by the optional bulk cargo door, if it is installed. The cargo doors are located on the right hand side of the fuselage. The FWD and AFT cargo doors are operated upward by two hydraulic actuators with pressure provided by the yellow electric pump (normal operation) or by a hand pump (manual operation).

TMUECLP08-T01 LEVEL 1

UFD4200

AFT CARGO COMPARTMENT The AFT cargo compartment is basically equipped to be loaded with bulk and loose baggage. The optional semi-automatic cargo loading system transports pallets and containers and is operated from a control panel installed on the cargo door.

EFFECTIVITY EFFECTIVITY ALL

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25 EQUIPMENT/FURNISHINGS

CARGO COMPARTMENT PRESENTATION EFFECTIVITY EFFECTIVITY ALL

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TMUECLP08 LEVEL 1

UFD4200

THIS PAGE INTENTIONALLY LEFT BLANK

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-50-00 CARGO COMPARTMENT INTERIOR

TMUECCI01 LEVEL 1

UFD4200

CONTENTS: General FWD Cargo Compartment AFT And Bulk Cargo Compartment Compartment Drainage Self Examination

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT INTERIOR GENERAL

TMUECCI01-T01 LEVEL 1

UFD4200

The inside of the cargo compartments is fitted with floor and ceiling panels, sidewall linings and partition walls. All the linings are sealed to prevent leakage of water and spilt fluids. Rapid decompression panels are installed in the cutouts of the ceiling panels and lateral right sidewall lining.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT INTERIOR EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT INTERIOR FWD CARGO COMPARTMENT

TMUECCI01-T02 LEVEL 1

UFD4200

The floor panels, the ceiling panels and the sidewall linings prevent damage to the aircraft structure. The floor panels are of sandwich construction and have non slip surfaces. The ceiling panels are of a sandwich construction and are made of flame resistant synthetic material and permit fast decompression.They are attached to the structure with quick release fasteners. The sidewall linings are of a sandwich construction and are made of flame resistant synthetic material. They are attached to the structure with quick release fasteners. The FWD cargo compartment is fitted with two fixed partition walls. They are of a sandwitch construction and are made of flame resistant synthetic material.They are attached to the structure with quick release fasteners.

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CARGO COMPARTMENT INTERIOR EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT INTERIOR AFT AND BULK CARGO COMPARTMENT

TMUECCI01-T03 LEVEL 1

UFD4200

The floor panels, the ceiling panels and the sidewall linings prevent damage to the aircraft structure. The floor panels are of sandwich construction and have non slip surfaces. The ceiling panels are of a sandwich construction and are made of flame resistant synthetic material and permit fast decompression. They are attached to the structure with quick release fasteners. The sidewall linings are of a sandwich construction and are made of flame resistant synthetic material. They are attached to the structure with quick release fasteners.They are equipped with access panels to give access to other systems. The AFT cargo compartment is fitted with two fixed partition walls.The partition walls are of a sandwich construction and are made of flame resistant synthetic material.They are attached to the structure with quick release fasteners.

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CARGO COMPARTMENT INTERIOR EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT INTERIOR COMPARTMENT DRAINAGE

TMUECCI01-T04 LEVEL 1

UFD4200

The FWD and AFT cargo compartments have drainage systems.

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SELF EXAMINATION the rapid decompression panels installed? in the cutouts of the ceiling panels. in the fixed partition walls. in the cutouts of the ceiling panels and lateral right sidewall linings.

TMUECCI01 LEVEL 1

UFD4200

Where are A B C -

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES

TMUCLSB01 LEVEL 1

UFD4200

CONTENTS: General FWD Cargo Compartment AFT/Bulk Cargo Compartment Self Examination

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES GENERAL

TMUCLSB01-T01 LEVEL 1

UFD4200

Here are the cargo loading capabilities. The FWD, AFT and bulk cargo compartments are basically equipped to be loaded with bulk and loose baggage. If the cargo loading system option is installed, the FWD and AFT cargo compartments can be loaded with containers or pallets.

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CARGO COMPARTMENT CAPABILITIES - GENERAL EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES FWD CARGO COMPARTMENT

TMUCLSB01-T02 LEVEL 1

UFD4200

The FWD cargo compartment can be basically loaded with bulk and loose baggage. If the cargo loading system is installed in the FWD cargo compartment, it is possible to load 3 Unit Load Devices (ULDs) which can be mixed (containers or pallets). For the bulk loading, the FWD cargo compartment is divided into 2 zones by a lateral divider net. A longitudinal door net is installed around the door to keep the cargo door area free.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - FWD CARGO COMPARTMENT EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES AFT AND BULK CARGO COMPARTMENTS

TMUCLSB01-T03 LEVEL 1

UFD4200

The AFT cargo compartment can be basically loaded with bulk and loose baggage. If the cargo loading system is installed in the AFT cargo compartment, it is possible to load 4 Unit Load Devices (ULDs) which can be mixed (containers or pallets). For the bulk loading, the AFT cargo compartment is divided into 3 zones by 2 lateral divider nets. A longitudinal door net is installed around the door to keep the cargo door area free. The bulk cargo compartment can only be loaded with bulk loading. It is separated from the AFT cargo compartment by a lateral divider net. If the bulk door option is installed, a door net prevents damage to the bulk door and keeps the cargo door area free.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - AFT AND BULK CARGO COMPARTMENTS EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUCLSB01 LEVEL 1

UFD4200

How many Unit Load Devices (ULDs) can be loaded in the FWD cargo compartment, if the Cargo Loading System is installed ? A - with 0 ULD. B - with 2 ULDs. C - with 3 ULDs.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES

TMUCLSB07 LEVEL 1

UFD4200

CONTENTS: General FWD Cargo Compartment AFT/Bulk Cargo Compartment Self Examination

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES GENERAL

TMUCLSB07-T01 LEVEL 1

UFD4200

Here are the cargo loading capabilities.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - GENERAL EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES FWD CARGO COMPARTMENT

TMUCLSB07-T02 LEVEL 1

UFD4200

The FWD cargo compartment can be loaded with containers, pallets or with bulk loading. In the FWD cargo compartment, it is possible to load 2 Unit Load Devices (ULDS) which can be mixed (containers or pallets). For the bulk loading, the FWD cargo compartment is divided into 2 zones by 1 lateral divider net. Lateral and longitudinal door nets are installed around the door to keep the cargo door area free.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - FWD CARGO COMPARTMENT EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES AFT/BULK CARGO COMPARTMENT

TMUCLSB07-T03 LEVEL 1

UFD4200

The AFT/Bulk cargo compartment can be loaded with containers, palets or with bulk loading. In the AFT cargo compartment, it is possible to load 2 Unit Load Devices (ULDS) which can be mixed (containers or pallets) and 1 narrower additional container (option). For the bulk loading, the AFT cargo compartment is divided into 2 zones by 1 lateral divider net. Lateral and longitudinal door nets are installed around the door to keep the cargo door area free. The bulk cargo conpartment can only be loaded with bulk loading. It is separated from the AFT cargo compartment by a lateral divider net.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - AFT AND BULK CARGO COMPARTMENT EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUCLSB07 LEVEL 1

UFD4200

How many Unit Load Devices (ULDS) can be loaded in the FWD cargo compartment? A - with 0 ULD. B - with 2 ULDS. C - with 3 ULDS.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES

TMUCLSB0A LEVEL 1

UFD4200

CONTENTS: General FWD Cargo Compartment AFT and Bulk Cargo Compartments Self Examination

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES GENERAL

TMUCLSB0A-T01 LEVEL 1

UFD4200

Here are the cargo loading capabilities. The FWD, AFT and bulk cargo compartments are basically equipped to be loaded with bulk and loose baggage. If the cargo loading system option is installed, the FWD and AFT cargo compartments can be loaded with containers or pallets.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - GENERAL EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES FWD CARGO COMPARTMENT

TMUCLSB0A-T02 LEVEL 1

UFD4200

The FWD cargo compartment can be basically loaded with bulk and loose baggage. If the cargo loading system is installed in the FWD cargo compartment it is possible to load 5 Unit Load Devices (ULDS) which can be mixed (containers or pallets). For the bulk loading, the FWD cargo compartment is divided into 3 zones by 2 lateral divider nets. Lateral and longitudinal door nets are installed around the door to keep the cargo door area free.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - FWD CARGO COMPARTMENT EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES AFT AND BULK CARGO COMPARTMENTS

TMUCLSB0A-T03 LEVEL 1

UFD4200

The AFT cargo compartment can be basically loaded with bulk and loose baggage. If the cargo loading system is installed in the AFT cargo compartment, it is possible to load 5 Unit Load Devices (ULDS) which can be mixed (containers or pallets). For the bulk loading, the AFT cargo compartment is divided into 3 zones by 2 lateral divider nets. Lateral and longitudinal door nets are installed around the door to keep the cargo door area free. The bulk cargo compartment can only be loaded with bulk loading. It is separated from the AFT cargo compartment by a lateral divider net. A door net prevents damage to the bulk door and keeps the cargo door area free.

EFFECTIVITY EFFECTIVITY ALL

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CARGO COMPARTMENT CAPABILITIES - AFT AND BULK CARGO COMPARTMENTS EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION

TMUCLSB0A LEVEL 1

UFD4200

How many Unit Load Devices (ULDS) can be loaded in the AFT cargo compartment, if the cargo loading system is installed ? A - with 0 ULDS. B - with 5 ULDS. C - with 6 ULDS.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHING 25-50-00 CARGO LOADING SYSTEM PRESENTATION

TMUECCL09 LEVEL 1

UFD4200

CONTENTS: Logic Transport Components Guidance Components Latching Components Control Components Self Examination

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION The semi-automatic cargo loading systems in the forward and after compartments are identical, they have the same components and operate similarly. LOGIC forward and aft cargo loading system is controlled a control panel installed on the cargo door. no electrical power available, it is possible to or unload the Unit Loading Devices manually.

TMUECCL09-T01 LEVEL 1

UFD4200

Each from With load

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION - LOGIC EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION TRANSPORT COMPONENTS BALL MATS The ball mats are installed in the door area in the FWD and AFT compartments. The ball mats extend across the full length of the FWD and AFT compartments. They are used to change the direction of the Unit Load Devices (ULDs) during loading and unloading operations.

TMUECCL09-T02 LEVEL 1

UFD4200

ROLLER TRACKS The roller tracks are installed on the centerline of the FWD and AFT cargo compartment floors. Each roller track is fitted with rollers which permit ULDs to move in the longitudinal direction. POWER DRIVE UNITS (PDUs) The Power Drive Units are installed in the FWD and AFT cargo compartments for lateral and longitudinal movements. There is one PDU for lateral movement on each ball mat area, three PDUs for longitudinal movement on the roller track of the FWD cargo compartment, and four PDUs for longitudinal movement on the roller track of the AFT cargo compartment. The PDUs operate with 115 VAC, 400 HZ, and have a thermal overload protection.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION - TRANSPORT COMPONENTS EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION GUIDANCE COMPONENTS ENTRANCE GUIDE Two entrance guides are installed on each door sill of the FWD and AFT cargo compartments. The entrance guides fitted with a vertical roller to align the ULD in the X and Y directions and prevent damage to the door frame.

TMUECCL09-T03 LEVEL 1

UFD4200

Y-GUIDE A Y-guide is installed in the FWD cargo compartment. The Y-guide is fitted with three vertical rollers which prevent friction between the ULD and the guide.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION - GUIDANCE COMPONENTS EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION LATCHING COMPONENTS DOOR SILL LATCH Two door sill latches are installed on the sills of each cargo compartment. Each sill latch has a housing, a manually operated YZ-latch, an overridable Y-latch a guide-in roller, a limit switch. It prevents the roll out of a ULD, and locks it in position.

END STOP Two end stops are installed in the roller track of each cargo compartment. They hold the ULDs in X and Z directions.

TMUECCL09-T04 LEVEL 1

UFD4200

FIXED YZ-LATCH The fixed YZ-latches are installed on each sidewall frame of the FWD and AFT cargo compartments. The fixed YZ-latches are equipped with a roller exept three YZ-latches in front of each cargo door. They hold the ULDs in the Y and Z directions. A vertical roller guides the ULDs in the X direction. XZ-SINGLE LATCH 32 Two XZ-single latch 32 are installed in the roller track of the FWD cargo compartment, and three XZ-single latch 32 are installed in the roller track of the AFT cargo compartment. They hold the ULDs in the X and Z directions. Each XZ-single latch 32 is fitted with a proximity switch which energizes a PDU only if the latch is lowered.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION - LATCHING COMPONENTS EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION CONTROL COMPONENTS CONTROL PANEL The control panels are installed on the inner face of each cargo door. They are equipped with: - a power ON/OFF switch, - a joystick, - a door sill latch switch, - a power indicator light.

TMUECCL09-T05 LEVEL 1

UFD4200

CONTROL BOX A control box is installed behind the sidewall panel of both the FWD and AFT cargo compartments. Each control box contains three power relays, an electronic circuit card, terminal junctions and two electrical connectors.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING SYSTEM PRESENTATION - CONTROL COMPONENTS EFFECTIVITY EFFECTIVITY ALL

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SELF EXAMINATION How is the PDU energized ? A - by 26 VAC. B - by 28 VAC. C - by 115 VAC.

TMUECCL09 LEVEL 1

UFD4200

The cargo loading control box being supplied, which latch ensures the energization of the PDUs ? A - the door sill latch. B - the XZ-single latch 32. C - the fixed YZ latch.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHING 25-52-00 CARGO LOADING OPERATIONS

TMUECLO03 LEVEL 3

UFD4200

CONTENTS: Cargo Loading Cargo Unloading Manual Loading Manual Unloading

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING OPERATIONS

TMUECLO03-T01 LEVEL 3

UFD4200

CARGO LOADING The cargo compartments can be loaded with different types of containers : - full size container. - half size container. - pallet. The FWD cargo compartment of the A320 can receive three containers or pallets and the Aft cargo compartment four. Let’s have a look to the A320 aft compartment loading and unloading. Switch on the compartment lights. Lower the two manual sill latches. Lower the XZ-latches. Switch on the power on the control panel. The cargo loading system is ready to be used. The container itself lowers the overridable sill latches. When the container is over the lateral Power Drive Unit, move the joystick to the "IN" position. At the end of the lateral travel, move the joystick to the longitudinal position. The longitudinal Power Drive Units move the container. When the container is in position, lift the corresponding XZ-latch. It locks the container and de-energizes the PDU underneath it. Load the other containers by following the same procedure. When the last container is loaded, lift up the two manual sill latches then check that the two overridable sill latches are up.

EFFECTIVITY EFFECTIVITY ALL

When the cargo loading is completed, the power can be switched off. CARGO UNLOADING For the cargo unloading, first of all, lower the manual sill latches, then switch the power ON. Lower and hold down the sill latch switch, the overridable sill latches lower. Move the joystick to the "OUT" position, the first container moves out. Lower the XZ-latch locking the next container. The associated PDU is available. Unload the container using the joystick. Do not forget to lower the overridable sill latches before moving the joystick to "OUT". Unload the other containers using the same procedure. When the cargo compartment is empty, switch off the power and lift-up the manual sill latches.

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25 EQUIPMENT/FURNISHINGS

CARGO LODING OPERATIONS EFFECTIVITY EFFECTIVITY ALL

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MANUAL LOADING For the manual cargo loading, the compartment preparation is the same as that for cargo loading with the automatic system. The containers are pushed by hand instead of using the PDUs. MANUAL UNLOADING

TMUECLO03-T02 LEVEL 3

UFD4200

For manual unloading, lower the two manual sill latches, then lower the overridable sill latches using the override handle. The containers are unloaded by hand instead of using the PDUs. At the end of the manual unloading, do not forget to release the overridable sill latches by pushing the handle, then to lift up the manual sill latches.

EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-50-00 CARGO BULK LOADING

TMUECLB03 LEVEL 3

UFD4200

CONTENTS: FWD Cargo Bulk Loading AFT Cargo Bulk Loading Bulk Cargo Compartment

EFFECTIVITY EFFECTIVITY ALL

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CARGO BULK LOADING FWD CARGO BULK LOADING

TMUECLB03-T01 LEVEL 3

UFD4200

The FWD cargo compartment is provided with items enabling occasional bulk loading: - Tie down points. - Net attachment points. - Load placards. - Markings to show ceiling clearance. - Divider nets/door nets.

EFFECTIVITY EFFECTIVITY ALL

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CARGO BULK LOADING - FWD CARGO BULK LOADING EFFECTIVITY EFFECTIVITY ALL

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CARGO BULK LOADING AFT CARGO BULK LOADING

TMUECLB03-T02 LEVEL 3

UFD4200

The AFT cargo compartment is provided with items enabling occasional bulk loading: - Tie down points. - Net attachment points. - Load placards. - Markings to show ceiling clearance. - Divider nets/door nets. A divider net isolates the AFT cargo compartment from the bulk cargo compartment.

EFFECTIVITY EFFECTIVITY ALL

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CARGO BULK LOADING - AFT CARGO BULK LOADING EFFECTIVITY EFFECTIVITY ALL

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CARGO BULK LOADING BULK CARGO COMPARTMENT

TMUECLB03-T03 LEVEL 3

UFD4200

The bulk cargo compartment is only provided with items enabling bulk loading. Access to the bulk cargo compartment is gained through the bulk cargo door, if the option is installed or through the AFT cargo door. The items for bulk loading are : - Typical tie down points, - Tie down points, - Typical attachment points, - Typical multiple attachment points, - Door nets.

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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CARGO BULK LOADING - BULK CARGO COMPARTMENT EFFECTIVITY EFFECTIVITY ALL

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TMUECLB03 LEVEL 3

UFD4200

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EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-53-00 DRAINING SYSTEM DESCRIPTION/OPERATION

TMUCLSG01 LEVEL 3

UFD4200

CONTENTS: FWD Cargo Compartment AFT Cargo Compartment

EFFECTIVITY EFFECTIVITY ALL

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DRAINING SYSTEM DESCRIPTION/OPERATION FWD CARGO COMPARTMENT Three outlet assemblies and a drain valve ensure the draining of the FWD cargo compartment. The three outlet assemblies are installed at the Aft end of the compartment in the floor panel. Each consists of a filter, a fitting and a tube down into the bilge of the fuselage. The drain valve is provided in the fuselage to clean the system. AFT CARGO COMPARTMENT

TMUCLSG01-T01 LEVEL 3

UFD4200

Three outlet assemblies and a drain valve ensure the draining of the AFT cargo compartment. The three outlet assemblies are installed at the Aft end of the compartment in the floor panel. Each consists of a filter, a fitting and a tube down into the bilge of the fuselage. The drain valve is provided in the fuselage to clean the system.

EFFECTIVITY EFFECTIVITY ALL

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DRAINING SYSTEM DESCRIPTION/OPERATION EFFECTIVITY EFFECTIVITY ALL

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TMUCLSG01 LEVEL 3

UFD4200

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EFFECTIVITY EFFECTIVITY ALL

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25 - EQUIPMENT/FURNISHINGS 25-52-00 CARGO LOADING COMPONENTS

TMUECLL07 LEVEL 3

UFD4200

CONTENTS: Ball Mats Rollers Door Sill Latches YZ-Latches XZ-Single Latches 32 Entrance Guides Y-Guide Power Drive Units End Stops Control Panels Control Boxes

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS BALL MATS IDENTIFICATION FIN: 2500MM, 2600MM LOCATION ZONE: 130, 150

TMUECLL07-T01 LEVEL 3

UFD4200

COMPONENT DESCRIPTION The ball mats are installed across the full width of the cargo compartment floor between the entrance guides. They enable the Unit Load Devices (ULDs) to be moved in the longitudinal and lateral directions.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS - BALL MATS EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS ROLLERS IDENTIFICATION FIN: 2501MM, 2601MM LOCATION ZONE: 130, 150

TMUECLL07-T02 LEVEL 3

UFD4200

COMPONENT DESCRIPTION Roller tracks are installed on the centerline of the FWD and AFT cargo compartment floors, and they are equipped with rollers. They enable ULDs to be moved in the longitudinal direction. Guide rollers prevent damage to the door sill and linings.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS - ROLLERS EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS DOOR SILL LATCHES IDENTIFICATION FIN: 2404VU1, 2404VU2, 2404VU3, 2404VU4 LOCATION ZONE: 132, 154

TMUECLL07-T03 LEVEL 3

UFD4200

COMPONENT DESCRIPTION Two door sill latches are installed on each cargo compartment door sill. Each door sill latch is provided with : - A manually operated YZ-latch. - An overridable Y-latch. - A guide roller. - A limit switch.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS - DOOR SILL LATCHES EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS YZ LATCHES IDENTIFICATION FIN: 2502MM, 2602MM LOCATION ZONE: 131, 132, 150, 153, 154

TMUECLL07-T04 LEVEL 3

UFD4200

COMPONENT DESCRIPTION The fixed YZ-latches are installed on each frame on the cargo compartment sidewalls. There are 12 YZ-latches with transport rollers and 3 YZ-latches in the FWD and 18 YZ-latches with transport rollers and 3 YZ-latches in the AFT cargo compartments.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS - YZ-LATCHES EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS XZ SINGLE LATCHES 32 IDENTIFICATION FIN: 2503MM, 2603MM LOCATION ZONE: 130, 150

TMUECLL07-T05 LEVEL 3

UFD4200

COMPONENT DESCRIPTION Manually operated XZ single latches 32 are installed in the roller tracks on the centerline of the cargo compartment floor. There are 2 XZ single latches 32 in the FWD and 3 XZ single latches 32 in the AFT cargo compartments. They can lock one or two ULDs. Proximity switches below are wired in series with the Power Drive Units. The Power Drive Unit can only be powered when the latches are lowered.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS - XZ-SINGLE LATCHES 32 EFFECTIVITY EFFECTIVITY ALL

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ENTRANCE GUIDES

Y GUIDE

IDENTIFICATION FIN: Not listed

IDENTIFICATION FIN: Not listed

LOCATION ZONE: 132, 154

LOCATION ZONE: 130

COMPONENT DESCRIPTION Two fixed entrance guides are installed on the door sills in each cargo compartment. They align the ULDs in the X and Y directions.

COMPONENT DESCRIPTION A fixed Y guide is installed across the forward end of the ball mats in the FWD cargo compartment. It is equipped with three vertical rollers to align the ULDs in the ball mat area.

TMUECLL07-T06 LEVEL 3

UFD4200

CARGO LOADING COMPONENTS

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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CARGO LOADING COMPONENTS - ENTRANCE GUIDES - Y-GUIDE EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS POWER DRIVE UNITS IDENTIFICATION FIN: 14MY, 15MY, 17MY, 19MY, 110MY, 112MY, 114MY, 115MY, 117MY LOCATION ZONE: 130, 150

TMUECLL07-T07 LEVEL 3

UFD4200

COMPONENT DESCRIPTION There are 3 Power Drive Units (PDUs) installed in the roller track of the FWD cargo compartment and 4 Power Drive Units (PDUs) installed in the roller track of the AFT cargo compartment for longitudinal movement, and one PDU in each entrance area for lateral movement. The PDU is energized with 115 / 200 VAC, 400 Hz. When the PDU operates in the opposite direction the supply phases are changed and the gears operate in the opposite direction.

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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CARGO LOADING COMPONENTS - POWER DRIVE UNITS EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS END STOPS IDENTIFICATION FIN: Not listed LOCATION ZONE: 130, 150

TMUECLL07-T08 LEVEL 3

UFD4200

COMPONENT DESCRIPTION The end stops are installed on each end of the roller tracks. They lock the Unit Load Devices (ULDs) in the X and Z directions.

EFFECTIVITY EFFECTIVITY ALL

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CARGO LOADING COMPONENTS - END STOPS EFFECTIVITY EFFECTIVITY ALL

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CONTROL PANELS

CONTROL BOXES

IDENTIFICATION FIN: 2020VU1, 2020VU2

IDENTIFICATION FIN: 1MY, 101MY

LOCATION ZONE: 825, 826

LOCATION ZONE: 132, 154

COMPONENT DESCRIPTION The control panels are located on the forward edge on each cargo door inner face. They comprise : - A power ON / OFF toggle switch. - A four position joystick ( IN - OUT - FWD - AFT ). - A door sill latch toggle switch. - A power indicator light.

COMPONENT DESCRIPTION The control boxes supply the PDUs with 115/200 VAC. They also supply 28 VDC to : - The door sill latch actuators. - The relays in all the PDUs. - The proximity switches. - The control panels.

TMUECLL07-T09 LEVEL 3

UFD4200

CARGO LOADING COMPONENTS

EFFECTIVITY EFFECTIVITY ALL

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UFD4200

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CARGO LOADING COMPONENTS - CONTROL PANELS - CONTROL BOXES EFFECTIVITY EFFECTIVITY ALL

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TMUECLL07 LEVEL 3

UFD4200

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EFFECTIVITY EFFECTIVITY ALL

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