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A300600 FCOM VOL.1 REV029

CROSS REFERENCE TABLE

THIS TABLE GIVES, FOR EACH AIRCRAFT INCLUDED IN THE MANUAL, THE CROSS REFERENCE BETWEEN : - THE MANUFACTURING SERIAL NUMBER (MSN) WHICH APPEARS IN THE LIST OF EFFECTIVE PAGES - THE REGISTRATION NUMBER OF THE AIRCRAFT AS KNOWN BY AIRBUS INDUSTRIE. ---------------------------------------------------------------------------MSN REGISTRATION ---------------------------------------------------------------------------0540 0556 0604 0605

G-MONR G-MONS G-MAJS G-OJMR

MON 01 FEB 2004

1.00.02 PAGE : CRT001

A300600

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HIGHLIGHTS

REV029

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1 00 00

003

001 REV029 -

1 00 03

001

1 01 00

001

1)Letter of transmittal for revision 29.

001 REV029 -

LETTER OF TRANSMITTAL

LIST OF NORMAL REVISIONS

1)List of normal revisions updated.

105 REV029

M:12557=12715

- INCORPORATION OF MOD 12557 - INCORPORATION OF MOD 12715 1)Doors chapter reissued. 1 01 00

002

001 REV029 -

1 01 30

001

1)Doors chapter reissued.

200 REV029

M:6240+12557

- INCORPORATION OF MOD 12557 1)Doors chapter reissued. 1 01 30

002

001 REV029 -

1 01 35

001

1)Doors chapter reissued.

110 REV029

M:12693=12715=(12557+12693)

- INCORPORATION OF MOD 12557 - INCORPORATION OF MOD 12693 1)Doors chapter reissued. 1 01 35

002

100 REV029

M:12557 OR 12715

- INCORPORATION OF MOD 12557 - INCORPORATION OF MOD 12715 1)Doors chapter reissued. 1 01 35

003

110 REV029

M:12671=(12557+12671)

- INCORPORATION OF MOD 12557 - INCORPORATION OF MOD 12671 1)Doors chapter reissued. 1 01 35

004

100 REV029

M:12557=12715

- INCORPORATION OF MOD 12557 - INCORPORATION OF MOD 12715 1)Doors chapter reissued. 1 01 35

005

105 REV029

M:12671

- INCORPORATION OF MOD 12671 01 FEB 2004

MON

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REV029

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1)Doors chapter reissued. 1 01 35

006

100 REV029

M:12671

- INCORPORATION OF MOD 12671 1)Doors chapter reissued. 1 01 38

001

400 REV029 -

1 01 40

007

M:5051+5448+5455+5725

INCORPORATION INCORPORATION INCORPORATION INCORPORATION

OF OF OF OF

MOD MOD MOD MOD

05051 05448 05455 05725

1)Doors chapter reissued.

200 REV029

M:4803+12557

- INCORPORATION OF MOD 12557 1)Description of CONSOLE FLOOD LT Switch is given for captain side. 2)The cockpit door OPEN FAULT light and the cockpit door cont panel lights are added to the list of light bulbs that are not automatically tested. 1 02 30

008

100 REV029 -

1 03 20

001

006

001

002

001

1)A text is added to indicate that the VHF3 can be used in voice mode by pressing the corresponding pushbutton.

100 REV029 -

1 07 10

1)For CAT 2 capability, only one Pitch Trim is required as correctly stated in FCOM 2.02.03 page 11.

001 REV029 -

1 06 50

1)The 8 deg./second throttle levers speed rate also applies to the Thrust Latch mode, which is associated with the alpha-floor activation.

001 REV029 -

1 05 70

1)Page changed to indicate the tolerance between the cabin altimeter on the overhead panel and the ECAM display.

001 REV029 -

1 03 50

M:5448

M:6214

1)Correction of AC power feeding conditions.

045 REV029

M:4803+12557

- INCORPORATION OF MOD 12557 01 FEB 2004

MON

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1 07 10

001

045 REV029 -

1 07 20

005

003

002

001

001

002

1 10 22

003

M:5051

1)The reference to 1-09-50 p 1 is added to see the description of the correct configuration of each system monitored by the take off warning.

001 REV029 -

01 FEB 2004

STD=8903+11340

1)Clarification about slats (or flaps) FAULT lights illumination (steady illuminated or flashing).

105 REV029 -

MOD 5408+11442

1)With the carbon rudder installed, the high speed range envelope for rudder travel limiting system is extended from 310 to VMO.

001 REV029 -

1 09 50

1)Note added to indicate that observations from the ground when hydraulics are switched off, should not be used for aileron zero position.

200 REV029 -

1 09 24

1)Note added to indicate that observations from the ground when hydraulics are switched off, should not be used for elevator zero position.

001 REV029 -

1 09 14

1)The mask stowage procedure is added to prevent oxygen depletion if the hose is pierced due to improper stowage.

001 REV029 -

1 09 13

1)Text changed to reflect the reinforced cockpit door installation.

001 REV029 -

1 09 12

M:4803+12557

1)The description of cockpit information about VMAX is expanded to point out that the VMAX warning is independent of the VMAX displayed on the PFD. For example, in case of jammed slats/ flaps surface, the VFE on the PFD corresponding to the S/F lever MON

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REV029

V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------position may be above the VFE corresponding to the actual S/F configuration. Whatever the S/F lever position, the VMAX warning is triggered anytime the VFE corresponding to the actual S/F configuration is exceeded. 1 10 24

004

001 REV029 -

1 10 41

002

001 REV029 -

1 10 81

002

001

1)Inhibition logic of the altitude alert is removed since it is already in 1.10.41 page 1.

105 REV029 -

1 10 82

1)Clarification of the conditions for display of the ILS/DME distance on the PFD.

CODE 0110

1)The description of GPWS mode 4 warnings is set in accordance with description of GPWS LDG SLATS/FLAPS switch given in 1.10.82 page 2.

100 REV029

M:11894

- INCORPORATION OF MOD 11894 1)Page introduced to reflect EGPWS complete test sequence. 1 10 82

003

200 REV029 -

1 11 00

002

1 11 10

001

003

M:4607+4801

1)Refueling and defueling is also possible via the MAINT BUS switch using an external power, as mentioned in 1.11.60 page 3.

001 REV029 -

01 FEB 2004

M:4607+4801+6875

1)The T. FUEL indication on the ECAM MEMO page is displayed with only one digit after the dot.

200 REV029 -

1 11 40

1)No technical change.

300 REV029 -

CODE:0092

1)FUEL X FEED reference is deleted as it is not involved in AUTOFEED logic.

MON

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001

200 REV029 -

1 11 51

001

1 11 52

001

002

001

001

1)The TOTAL FUEL indication is displayed on the ECAM FUEL page with only one digit after the dot.

1)A transfer of less than 400 kg (880 lb) of fuel to the right inner tank induces the display of a dash on the FQI.

200 REV029 -

1 11 73

M:4801+5051

001 REV029 -

1 11 71

M:4801+6875

1)The display conditions of a dash instead of the last digit of the FQI are clarified. An indication is added to state that when it occurs the FQI is still operative.

200 REV029 -

1 11 60

1)The TOTAL FUEL indication on the ECAM FUEL page is displayed with only one digit after the dot.

230 REV029 -

M:4607+4801

M:4801+10778

1)The Weight and Balance System (WBS) is not fitted on the aircraft and does not provide any input to the CGCC. Only the FMS provides the ZFCG and the ZFW to the CGCC.

200 REV029

M:4801+6384

- INCORPORATION OF MOD 06384 1)When a pump is selected NORM but is not running, the pump symbol on the ECAM is in green. 2)With ECAM SGU W14, the transfer symbol has been deleted on the ECAM FUEL page. 1 15 11

001

100 REV029 -

1 15 11

002

01 FEB 2004

1)Clarification about description of warning annunciator lights on MSU.

100 REV029 -

M:4672

CODE 0002

1)Clarification about wind information presented on ISDU.

MON

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V CH SEC ---PAGE-- SEQ --REV-- ----VALIDATION CRITERIA---------------------------REASONS OF CHANGE-------------------------------------------------------------------------------------------------------1 15 22

002

100 REV029 -

1 15 24

003

006

005

002

001

001

006

003

M:5051

1)Total fuel indication on ECAM MEMO PAGE with only one digit after the decimal.

1)Coordinated use of ECAM and QRH is given in QRH 0.01 and 0.02.

100 REV029 -

01 FEB 2004

1)Total fuel indication on ECAM MEMO PAGE with only one digit after the decimal.

001 REV029 -

1 18 40

1)Total fuel indication on ECAM MEMO PAGE with only one digit after the decimal.

103 REV029 -

1 18 30

MOD 5051

001 REV029 -

1 18 20

GE

1)The TRP LIM MODE window displays TO when FLX TO mode is selected.

100 REV029 -

1 18 10

1)The altitude intercept point may be displayed either in blue or in amber.

010 REV029 -

1 18 00

1)Reason for altitude intercept point displayed in amber is added to the altitude intercept point description.

001 REV029 -

1 17 80

1)Enhanced description of ADF bearing information presented on the ND.

001 REV029 -

1 15 24

M:2962

M:5051

1)Incorporation of TR No. 91-1. The EMER AUDIO CANCEL pushbutton cancels all (E)GPWS and TCAS audio warnings. Sentence deleted.

MON

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--REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-----REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-------------EFFECTIVITY----------| ----------EFFECTIVITY--------------------------------------------------------------------------------------------------------------------------------------------| 1 00 00 001 001 REV027 CONTENTS | N 1 01 30 001 200 REV029 M:6240+12557 1 00 00 002 001 REV028 COMMENTS | N 1 01 30 002 001 REV029 ALL | ALL | R 1 00 00 003 001 REV029 LETTER OF TRANSMITTAL | N 1 01 35 001 110 REV029 M:12693=12715=(12557+12693) R 1 00 00 004 001 REV028 | N 1 01 35 002 100 REV029 M:12557 OR 12715 ALL | ALL | 1 00 01 001 001 REV028 ORGANIZATION OF THE MANUAL | N 1 01 35 003 110 REV029 M:12671=(12557+12671) 1 00 01 002 001 REV028 ORGANIZATION OF THE MANUAL | N 1 01 35 004 100 REV029 M:12557=12715 ALL | ALL | 1 00 01 003 001 REV028 ORGANIZATION OF THE MANUAL | N 1 01 35 005 105 REV029 M:12671 1 00 01 004 001 REV027 | N 1 01 35 006 100 REV029 M:12671 ALL | ALL | R 1 00 02 CRT 001 REV029 CROSS REFERENCE TABLE | N 1 01 38 001 400 REV029 M:5051+5448+5455+5725 ALL | ALL | R 1 00 02 HL 001 REV029 HIGHLIGHTS | 1 01 40 001 001 REV019 ALL | 1 01 40 002 001 REV011 | ALL R 1 00 02 LEP 001 REV029 LIST OF EFFECTIVE PAGES | ALL | 1 01 40 003 001 REV026 | 1 01 40 004 150 REV017 CODE 0140E R 1 00 02 LOM 001 REV029 LIST OF MOD/MP/SB | ALL ALL | | 1 01 40 005 020 REV005 MOD 4803 ALL/ALL R 1 00 03 001 001 REV029 LIST OF NORMAL REVISIONS | 1 01 40 006 020 REV019 MOD.4803 R 1 00 03 002 001 REV025 LIST OF NORMAL REVISIONS | ALL ALL | | N 1 01 40 007 200 REV029 M:4803+12557 1 00 04 000-LTR 001 LIST OF TEMPORARY REVISIONS | N 1 01 40 008 040 REV019 MOD.4803+5051 ALL | ALL | 1 00 04 001 001 REV026 LIST OF TEMPORARY REVISIONS | 1 01 40 009 001 AUG1983 ALL/ALL 1 00 04 002 001 REV026 LIST OF TEMPORARY REVISIONS | 1 01 40 010 001 REV019 ALL | ALL | 1 00 05 001 001 REV027 | 1 01 40 011-12 110 REV025 M:5544 OR (5544+10002) 1 00 05 002 001 REV027 | ALL ALL | | 1 01 50 001 110 REV027 M:4803 1 00 05 003 001 REV027 | ALL 1 00 05 004 001 REV027 | ALL | 1 01 50 001-2 020 REV008 M:4803 | ALL 1 00 05 005-6 001 REV021 | ALL | 1 02 00 001-2 001 REV005 ALL/ALL | ALL R 1 00 06 001 001 REV029 | R 1 00 06 002 001 REV013 | 1 02 10 001 001 REV012 ALL | 1 02 10 002 001 REV026 | ALL R 1 00 25 001 001 REV029 LIST OF CODES | R 1 00 25 002 001 REV029 LIST OF CODES | 1 02 20 001 100 REV026 M:7866 ALL | 1 02 20 002 001 REV011 | ALL R 1 00 25 003 001 REV029 LIST OF CODES | R 1 00 25 004 001 REV029 LIST OF CODES | 1 02 20 003 020 REV026 M:6444 ALL | 1 02 20 004 301 REV026 M:6334+6444+7866 | ALL R 1 00 25 005 001 REV029 LIST OF CODES | R 1 00 25 006 001 REV029 LIST OF CODES | 1 02 20 005 001 REV003 ALL/ALL ALL | 1 02 20 006 001 REV022 | ALL N 1 00 25 007 001 REV029 LIST OF CODES | ALL | 1 02 20 007 001 AUG1983 ALL/ALL | 1 02 20 008 056 REV026 M:6444+7866 N 1 01 00 001 105 REV029 M:12557=12715 | ALL N 1 01 00 002 001 REV029 | ALL | 1 02 20 009 001 REV013 | 1 02 20 010 305 REV027 M:6106+6444+7866 1 01 10 001 001 REV021 | ALL 1 01 10 002 100 REV018 MOD.5527 | ALL | 1 02 20 011 001 REV007 ALL/ALL | 1 02 20 012 001 REV021 1 01 10 003 100 REV018 MOD.5527 | ALL 1 01 10 004 200 REV022 CODE 0079 | ALL | 1 02 20 013 045 REV018 MOD.5448+6041 | 1 02 20 014 020 REV008 MOD.5051 1 01 10 005-6 001 REV003 ALL/ALL | ALL ALL | | 1 02 30 001 001 REV028 1 01 20 001 200 REV023 M:4803+5353 | 1 02 30 002 001 REV014 1 01 20 002 030 REV005 MOD 4803 ALL/ALL | ALL ALL | | 1 02 30 003 001 REV003 ALL/ALL 1 01 20 003 001 REV023 | 1 02 30 004 001 REV006 ALL/ALL 1 01 20 004 020 REV005 MOD 4803 ALL/ALL | ALL ALL | | |

01 FEB 2004

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--REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-----REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-------------EFFECTIVITY----------| ----------EFFECTIVITY--------------------------------------------------------------------------------------------------------------------------------------------| 1 02 30 005 001 REV002 ALL/ALL | 1 03 22 001 001 REV024 1 02 30 006 020 REV012 MOD 6044 | 1 03 22 002 001 REV024 ALL | ALL | R 1 02 30 007 020 REV021 MOD.6044 | 1 03 23 001 100 REV024 M:3791 R 1 02 30 008 100 REV029 M:5448 | 1 03 23 002 001 REV023 ALL | ALL | 1 02 30 009 001 REV021 | 1 03 24 001 001 REV024 1 02 30 010 100 REV028 M:5051 | 1 03 24 002 001 REV024 ALL | ALL | 1 02 40 001 030 REV010 MOD 5119 | 1 03 25 001 001 REV025 1 02 40 002 220 REV023 MOD 5119+7483 | 1 03 25 002 001 REV024 ALL | ALL | 1 02 40 003 025 REV006 MOD 5119 ALL/ALL | 1 03 26 001 105 REV023 M:5051 1 02 40 004 020 REV006 MOD 5119 ALL/ALL | 1 03 26 002 001 REV024 ALL | ALL | 1 02 40 005 001 REV010 | 1 03 30 001 001 REV024 1 02 40 006 045 REV012 MOD 5051+5119 | 1 03 30 002 001 REV023 ALL | ALL | 1 02 50 001-2 001 REV021 | 1 03 30 003 001 REV024 ALL | 1 03 30 004 001 REV024 | ALL 1 03 00 001 001 REV023 | 1 03 00 002 105 REV025 M:5051 | 1 03 31 001 001 REV024 ALL | 1 03 31 002 100 REV024 M:5051 | ALL 1 03 10 001 001 REV026 | 1 03 10 002 001 REV024 | 1 03 32 001 001 REV025 ALL | 1 03 32 002 001 REV023 | ALL 1 03 10 003 001 REV023 | 1 03 10 004 001 REV024 | 1 03 33 001 200 REV025 M:11442+11900 ALL | 1 03 33 002 200 REV025 M:11454+11900 | ALL 1 03 10 005 001 REV024 | 1 03 10 006 001 REV024 | 1 03 33 003 100 REV024 M:11454 ALL | 1 03 33 004 001 REV024 | ALL 1 03 11 001 100 REV027 M:11900 | 1 03 11 002 100 REV024 M:3791 | 1 03 40 001 001 REV024 ALL | 1 03 40 002 001 REV024 | ALL 1 03 11 003 100 REV023 M:3791 | 1 03 11 004 001 REV024 | 1 03 41 001 100 REV024 M:7187 ALL | 1 03 41 002 100 REV023 M:6036 | ALL 1 03 12 001 001 REV024 | 1 03 12 002 110 REV023 MOD 6036 | 1 03 41 003 001 REV023 ALL | 1 03 41 004 001 REV024 | ALL 1 03 12 003 001 REV024 | 1 03 12 004 001 REV024 | 1 03 42 001 100 REV025 M:11900 ALL | 1 03 42 002 100 REV025 M:11900 | ALL 1 03 12 005 001 REV024 | 1 03 12 006 001 REV023 | 1 03 42 003 100 REV025 M:11900 ALL | 1 03 42 004 100 REV025 M:11900 | ALL 1 03 12 007 001 REV024 | 1 03 12 008 001 REV024 | 1 03 43 001 001 REV024 ALL | 1 03 43 002 210 REV024 M:3791+6036 | ALL 1 03 12 009 001 REV024 | 1 03 12 010 001 REV024 | 1 03 43 003 001 REV023 ALL | 1 03 43 004 001 REV024 | ALL 1 03 13 001 001 REV023 | 1 03 13 002 100 REV024 M:7187 | 1 03 44 001 001 REV025 ALL | 1 03 44 002 001 REV023 | ALL 1 03 13 003 100 REV026 M:11900 | 1 03 13 004 100 REV025 M:11900 | 1 03 44 003 001 REV023 ALL | 1 03 44 004 001 REV023 | ALL R 1 03 20 001 001 REV029 | R 1 03 20 002 001 REV024 | 1 03 45 001 001 REV023 ALL | 1 03 45 002 001 REV024 | ALL 1 03 20 003 001 REV024 | 1 03 20 004 001 REV024 | 1 03 46 001 001 REV023 ALL | 1 03 46 002 001 REV024 | ALL 1 03 21 001 001 REV025 | 1 03 21 002 001 REV024 | 1 03 47 001 001 REV023 ALL | 1 03 47 002 001 REV023 | ALL | |

01 FEB 2004

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--REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-----REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-------------EFFECTIVITY----------| ----------EFFECTIVITY--------------------------------------------------------------------------------------------------------------------------------------------| 1 03 48 001 001 REV023 | 1 05 20 001 110 REV028 M:6213 1 03 48 002 001 REV023 | 1 05 20 002 001 REV025 ALL | ALL | 1 03 49 001 001 REV023 | 1 05 20 003 001 REV025 1 03 49 002 001 REV023 | 1 05 20 004 001 REV027 ALL | ALL | 1 03 50 001 001 REV024 | 1 05 20 005 001 REV025 1 03 50 002 001 REV025 | 1 05 20 006 001 REV025 ALL | ALL | 1 03 50 003 001 REV023 | 1 05 30 001 001 REV025 1 03 50 004 001 REV024 | 1 05 30 002 001 REV025 ALL | ALL | R 1 03 50 005 100 REV024 M:5051 | 1 05 30 003 001 REV025 R 1 03 50 006 001 REV029 | 1 05 30 004 001 REV025 ALL | ALL | 1 03 51 001 001 REV026 | 1 05 40 001 001 REV025 1 03 51 002 001 REV025 | 1 05 40 002 120 REV025 MOD : 4803 ALL | ALL | 1 03 52 001 100 REV024 M:3791 | 1 05 40 003 001 REV025 1 03 52 002 100 REV024 M:3791 | 1 05 40 004 001 REV025 ALL | ALL | 1 03 52 003 110 REV023 MOD 3791 | 1 05 50 001 001 REV025 1 03 52 004 100 REV023 M:3791 | 1 05 50 002 100 REV025 MOD : 4803 ALL | ALL | 1 03 53 001 001 REV024 | 1 05 50 003 001 REV025 1 03 53 002 001 REV023 | 1 05 50 004 001 REV025 ALL | ALL | 1 04 00 001-2 001 REV005 ALL/ALL | 1 05 60 001 001 REV025 ALL | 1 05 60 002 001 REV025 | ALL 1 04 10 001 200 REV023 M:5917+6299 = 5917+5918+6299 | 1 04 10 002 001 REV005 ALL/ALL | R 1 05 70 001 001 REV029 ALL | R 1 05 70 002 001 REV025 | ALL 1 04 10 003-4 020 REV013 MOD 6299 | ALL | 1 06 00 001 001 REV023 | 1 06 00 002 205 REV023 MOD 6214 + 7483 1 04 20 001 001 AUG1983 ALL/ALL | ALL 1 04 20 002 001 REV002 ALL/ALL | ALL | 1 06 10 001 100 REV026 M:6214 | 1 06 10 002 100 REV027 M:6214 1 04 30 001 001 REV002 ALL/ALL | ALL 1 04 30 002 001 REV027 | ALL | 1 06 20 001 001 REV024 | 1 06 20 002 001 REV023 1 04 40 001 001 REV002 ALL/ALL | ALL 1 04 40 002 001 REV012 | ALL | 1 06 21 001 001 REV024 | 1 06 21 002 001 REV023 1 04 50 001 020 REV013 M:6299 | ALL 1 04 50 002 001 REV002 ALL/ALL | ALL | 1 06 30 001 001 REV023 | 1 06 30 002 001 REV023 1 04 60 001 001 REV012 | ALL 1 04 60 002 001 REV022 | ALL | 1 06 30 003 001 REV023 | 1 06 30 004 001 REV024 1 04 70 001 001 REV010 | ALL 1 04 70 002 001 REV022 | ALL | 1 06 30 005 001 REV024 | 1 06 30 006 001 REV024 1 04 80 001 030 REV022 M:6299 | ALL 1 04 80 002 001 REV022 | ALL | 1 06 30 007 001 REV024 | 1 06 30 008 001 REV024 1 04 80 003-4 100 REV013 M:5051+6299 | ALL ALL | | 1 06 31 001 100 REV024 MOD 7341 1 04 90 001 001 REV022 | 1 06 31 002 001 REV024 1 04 90 002 001 REV009 | ALL ALL | | 1 06 31 003 105 REV026 M:6214=(6214+8905+10952) 1 05 00 001 001 REV025 | 1 06 31 004 001 REV024 1 05 00 002 100 REV025 M:4803 | ALL ALL | | 1 06 32 001 001 REV026 STD=M:8905+10952 1 05 00 003 001 REV025 | 1 06 32 002 001 REV026 STD=M:8905+10952 1 05 00 004 001 REV025 | ALL ALL | | 1 06 32 003 100 REV027 M:5051=(5051+8905+10952) 1 05 10 001 001 REV025 | 1 06 32 004 001 REV023 1 05 10 002 001 REV025 | ALL ALL | |

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--REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-----REV-- -----VALIDATION CRITERIA---- | M V CH SEC ---PAGE-- SEQ --REV-- -----VALIDATION CRITERIA-------------EFFECTIVITY----------| ----------EFFECTIVITY--------------------------------------------------------------------------------------------------------------------------------------------| 1 19 30 005 200 REV015 MOD 3791+6662+7421 | 1 19 40 031 120 REV012 MOD 3791+6662 1 19 30 006 120 REV017 MOD.3791+6662 | 1 19 40 032 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 30 007 120 REV012 MOD 3791+6662 | 1 19 40 033 120 REV012 MOD 3791+6662 1 19 30 008 120 REV012 MOD 3791+6662 | 1 19 40 034 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 30 009 120 REV012 MOD 3791+6662 | 1 19 40 035 120 REV012 MOD 3791+6662 1 19 30 010 120 REV014 CODE 1930C | 1 19 40 036 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 30 011 120 REV012 MOD 3791+6662 | 1 19 40 037 120 REV012 MOD 3791+6662 1 19 30 012 120 REV016 MOD 3791+6662 | 1 19 40 038 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 30 013 120 REV012 MOD 3791+6662 | 1 19 40 039 120 REV012 MOD 3791+6662 1 19 30 014 200 REV016 MOD 3791+6662+7421 | 1 19 40 040 120 REV014 MOD 3791+6662 ALL | ALL | 1 19 30 015 120 REV012 MOD 3791+6662 | 1 19 40 041 120 REV016 CODE 1940C 1 19 30 016 120 REV016 MOD 3791+6662 | 1 19 40 042 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 30 017 120 REV012 MOD 3791+6662 | 1 19 40 043 120 REV012 MOD 3791+6662 1 19 30 018 200 REV016 MOD 3791+4801+6662 | 1 19 40 044 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 30 019 120 REV012 MOD 3791+6662 | 1 19 40 045 120 REV012 MOD 3791+6662 1 19 30 020 120 REV012 MOD 3791+6662 | 1 19 40 046 200 REV016 MOD 3791+4801+6662 ALL | ALL | 1 19 40 001 120 REV012 MOD 3791+6662 | 1 19 40 047 200 REV016 MOD 3791+4801+6662 1 19 40 002 120 REV012 MOD 3791+6662 | 1 19 40 048 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 003 120 REV012 MOD 3791+6662 | 1 19 40 049 120 REV014 MOD 3791+6662 1 19 40 004 150 REV016 CODE 1940C | 1 19 40 050 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 005 120 REV016 CODE 1940C | 1 19 40 051 120 REV012 MOD 3791+6662 1 19 40 006 200 REV016 MOD 3791+4801+6662 | 1 19 40 052 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 007 200 REV016 MOD 3791+4801+6662 | 1 19 40 053 120 REV012 MOD 3791+6662 1 19 40 008 120 REV012 MOD 3791+6662 | 1 19 40 054 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 009 120 REV012 MOD 3791+6662 | 1 19 40 055 120 REV012 MOD 3791+6662 1 19 40 010 120 REV012 MOD 3791+6662 | 1 19 40 056 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 011 120 REV012 MOD 3791+6662 | 1 19 40 057 120 REV012 MOD 3791+6662 1 19 40 012 120 REV012 MOD 3791+6662 | 1 19 40 058 120 REV017 MOD.3791+6662 ALL | ALL | 1 19 40 013 120 REV012 MOD 3791+6662 | 1 19 40 059 120 REV012 MOD 3791+6662 1 19 40 014 120 REV012 MOD 3791+6662 | 1 19 40 060 120 REV013 MOD 3791+6662 ALL | ALL | 1 19 40 015 120 REV012 MOD 3791+6662 | 1 19 40 061 120 REV012 MOD 3791+6662 1 19 40 016 120 REV012 MOD 3791+6662 | 1 19 40 062 120 REV014 MOD 3791+6662 ALL | ALL | 1 19 40 017 120 REV012 MOD 3791+6662 | 1 19 40 063 120 REV012 MOD 3791+6662 1 19 40 018 120 REV012 MOD 3791+6662 | 1 19 40 064 120 REV016 MOD 3791+6662 ALL | ALL | 1 19 40 019 120 REV012 MOD 3791+6662 | 1 19 40 065 120 REV012 MOD 3791+6662 1 19 40 020 120 REV012 MOD 3791+6662 | 1 19 40 066 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 021 120 REV012 MOD 3791+6662 | 1 19 40 067 120 REV012 MOD 3791+6662 1 19 40 022 120 REV012 MOD 3791+6662 | 1 19 40 068 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 023 120 REV014 MOD 3791+6662 | 1 19 40 069 120 REV012 MOD 3791+6662 1 19 40 024 120 REV012 MOD 3791+6662 | 1 19 40 070 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 025 120 REV012 MOD 3791+6662 | 1 19 40 071 120 REV012 MOD 3791+6662 1 19 40 026 120 REV012 MOD 3791+6662 | 1 19 40 072 120 REV012 MOD 3791+6662 ALL | ALL | 1 19 40 027 120 REV012 MOD 3791+6662 | 1 19 40 073 120 REV012 MOD 3791+6662 1 19 40 028 120 REV012 MOD 3791+6662 | 1 19 40 074 120 REV021 MOD 3791+6662 ALL | ALL | 1 19 40 029 120 REV012 MOD 3791+6662 | 1 19 40 075 120 REV012 MOD 3791+6662 1 19 40 030 120 REV012 MOD 3791+6662 | 1 19 40 076 120 REV012 MOD 3791+6662 ALL | ALL | |

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2962 ...... ...........

REVISION : 029

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. 015

INSTALL 2ND ARINC 712 ADF SYSTEM ALL

. 015

OXYGEN - FLIGHT CREW SYSTEM - INCREASE CAPACITY OF CYLINDER ALL

. 015

INSTALL A REPLENISHMENT CONNECTOR OUTSIDE OXYGEN COMPARTMENT ALL

. 015

INSTALL FANS FOR MESSIER BRAKES ALL

. 015

INSTALL A TIRE PRESSURE INDICATING SYSTEM ALL

. 015

INSTALL 2 FNL FLIGHT MANAGEMENT SYSTEMS ALL

. 015

DELETE BATTERY COOLING FAN ALL

. 015

NAVIGATION - SUPPLY ADF1 EMERGENCY ELECTRICAL POWER ALL

. 015

FUEL - DELETE JETTISON SYSTEM ALL

. 015

NAVIGATION - INSTALL 3 HONEYWELL IRS ALL

. 015

FUEL - INSTALL TRIM TANK SYSTEM ALL

. 015

EQUIPMENT/FURNISHINGS - FLIGHT COMPARTMENT MODIFY DESIGN ALL

. 017

EXHAUST - IMPROVE THE SELECTION LOGIC OF THE FLIGHT IDLE ALL

2965 ...... ........... 3406 ...... ........... 3721 ...... ........... 3781 ...... ........... 3791 ...... ........... 4000 ...... ........... 4536 ...... ........... 4607 ...... ........... 4672 ...... ........... 4801 ...... ........... 4803 ...... ........... 4857 ...... ...........

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4917 ...... ...........

REVISION : 029

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. 027

FUEL - FEED SYSTEM - CENTER TANK DELETE ISOLATION VALVE ALL

. 015

INDICATING/RECORDING SYSTEMS - ECAM DELETE WLDP ALL

. 015

AIR CONDITIONING - AVIONICS COMPARTMENT VENTILATION - SIMPLIFY VENTILATION SYSTEM ALL

. 015

PNEUMATIC - BLEED AIR - MODIFY OVERHEAT DETECTION ALL

. 021

FLAP CONTROLS - SLAT AND FLAP CONTROL SYSTEM - MODIFY INPUT CONTROL ALL

. 015

EQUIPMENT/FURNIGHINGS - FLIGHT COMPART. INSTALL A 4TH OCCUPANT FOLDING SEAT ALL

. 015

FLIGHT CONTROLS - RUDDER CONTROLS REDUCE RUDDER DEFLECTION FROM 5
TO 3.5
IN HIGH SPEED FLIGHT ALL

. 015

OXYGEN - FLIGHT COMPARTMENT - RELOCATE PORTABLE OXYGEN EQUIPMENT ALL

. 015

INDICATING RECORDING SYSTEM - FLIGHT WARNING COMPUTER - INTRODUCE L 11 BATCH IMPROVEMENT ALL

. 015

INDICATING/RECORDING SYSTEMS - ECAM MODIFY SGU SOFTWARE ALL

. 015

DOORS - ACCESS DOORS 134AR AND 136AR MAKE PROVISIONS FOR DOORS WARNING SYSTEM ALL

5051 ...... ........... 5119 ...... ........... 5146 ...... ........... 5224 ...... ........... 5353 ...... ........... 5408 ...... ...........

5414 ...... ........... 5425 ...... ...........

5448 ...... ........... 5455 ...... ...........

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. 018

WINGS - INTRODUCE WING TIP FENCE ALL

. 015

LIGHTS - PASSENGER COMPARTMENT EMERGENCY LIGHTING CIRCUIT - MODIFY MINIMUM LIGHT FUNCTION ALL

. 015

FUEL - MODIFY FEED SYSTEM LOGIC DURING TAXI/TAKE OFF PHASE ALL

. 015

LANDING GEAR - INSTALLATION OF MESSIER CARBON BRAKES 76 MJ AND ASSOCIATED WHEELS ALL

. 015

NAVIGATION - GPWS - IMPROVE FUNCTION ALL

. 015

INDICATING/RECORDING SYSTEMS - FLIGHT WARNIN COMPUTER - INTRODUCE L12 BATCH IMPROVEMENT ALL

. 015

NAVIGATION - GPWS - ADD OVRD POSITION INDICATING ALL

. 015

FLIGHT CONTROLS - JAMMING DETECTION SYSTEM MODIFY JAMMING DETECTION UNIT ALL

. 015

AIRBORNE AUXILLIARY POWER - STARTING EXTEND RELIGHT ALTITUDE ALL

. 022

FUSELAGE - APU AIR INTAKE - INSTALL FIXED DIVERTER AND MODIFY FLUID BARRIERS ALL

. 015

FLIGHT CONTROLS - SFCC - MODIFY SOFTWARE ALL

5544 ...... ...........

5562 ...... ........... 5670 ...... ...........

5697 ...... ........... 5725 ...... ........... 5896 ...... ........... 5904 ...... ........... 5917 ...... ........... 5918 ...... ........... 5952 ...... ...........

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6007 ...... ...........

REVISION : 029

VALIDITY

. 015

PNEUMATIC - ENGINE BLEED AIR SUPPLY SYSTEM MODIFY TRIGGERING THRESHOLD OF BLEED VALVE FAULT WARNING ALL

. 015

AUTO FLIGHT - REPLACE FCO ALL

. 015

HYDRAULIC POWER - NOSE WHEEL STEERING COUPLER - DELETE HYDRAULIC LINE ALL

. 015

INDICATING/RECORDING SYSTEMS - ECAM INTRODUCE NEW SGU SOFTWARE ALL

. 015

AIR CONDITIONING - CABIN PRESSURE CONTROL SYSTEM - REPLACE VALVE POSITION INDICATORS ALL

. 015

AIR CONDITIONING - MODIFY PACK DISCHARGE TEMPERATURE LOW LIMIT IN MAX COOL MODE ALL

. 015

NAVIGATION - ACTIVATE AUTOMATIC RADIO ALTITU CALL-OUT ON FWC ALL

. 015

PNEUMATIC - ENGINE BLEED AIR SUPPLY SYSTEM INCREASE MINIMUM ENGINE IDLE ALL

. 021

HYDRAULIC POWER - PROVIDE SYSTEM PROVISIONS FOR AN AC/DC STANDBY GENERATOR HYDRO-ELECTRICAL ALL

. 015

ELECTRICAL POWER - INSTALL AN AC/DC STANDBY GENERATOR HYDRO-ELECTRICAL UNIT ALL

. 015

DOORS - PASSENGER/CREW DOORS - DAMPER AND EMERGENCY OPERATION CYLINDER - MODIFY STRIKER ALL

6036 ...... ........... 6038 ...... ........... 6041 ...... ........... 6044 ...... ...........

6106 ...... ........... 6119 ...... ........... 6120 ...... ........... 6213 ...... ...........

6214 ...... ........... 6240 ...... ...........

MON 01 FEB 2004

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6267 ...... 26-6038 03

REVISION : 029

VALIDITY

. 026

FIRE PROTECTION - MODIFY ENGINE AND APU FIRE DETECTION SYSTEM ALL

. 015

AIRBORNE AUXILIARY POWER - PROVIDE APU AIR INTAKE CLOSURE WHEN THE APU IS SWITCHED OFF ALL

. 015

AIR CONDITIONING - AIR CONDITIONING PACK CLOSING SIGNAL - MODIFY WIRING ALL

. 015

FUEL - FUEL PUMP SYSTEM - MODIFY ELECTRICAL POWER SUPPLY ALL

. 015

AIR-PYLON COOLING - MODIFY TURBINE CASE COOL WARNING SYSTEM ALL

N 029

INDICATING/RECORDING SYSTEMS - ECAM MODIFY SGU SOFTWARE ALL

. 015

AIR CONDITIONING - DELETE MAX COOL OFF MESSAGE ON ECAM DISPLAY UNIT ALL

. 015

INDICATING/RECORDING SYSTEMS - ECAM INTRODUCE FWC SOFTWARE S4 ALL

. 023

FUEL - FUEL PUMP SYSTEM - MODIFY TRANSFER VALVE POWER SUPPLY ALL

. 015

FUEL - MODIFY CENTER TANK PUMP CONTROL SYSTEM ALL

. 015

NAVIGATION - SMITHS FMS - INTRODUCE PERF2 SOFTWARE ALL

6299 ...... ........... 6334 ...... ........... 6368 ...... ........... 6383 ...... ........... 6384 ...... ........... 6444 ...... ........... 6445 ...... ........... 6497 ...... ........... 6519 ...... ........... 6662 ...... ...........

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6708 ...... ...........

REVISION : 029

VALIDITY

. 015

FUEL - FUEL FEED - IMPROVE REFUEL GALLERY DRAIN VALVES ALL

. 015

FUEL - OVERCOME INNER TANK NUISANCE ECAM WARNINGS ALL

. 015

FUEL - INTRODUCE NEW STANDARD INDICATOR ALL

. 015

NAVIGATION - MODIFY EFIS SGU ALL

. 025

AUTO FLIGHT - FAC - INTRODUCE NEW EQUIPMENT FOR 600R ALL

. 015

POWER PLANT - INSTALL GE CF680 C2A5 ENGINES ON A300-600R A/C ALL

. 015

AUTO FLIGHT - GENERAL - INSTALL COMPONENTS WITH AIRBORNE WINDSHEAR WARNING SYSTEM CAPACITY ALL

. 015

INDICATING/RECORDING SYSTEMS - ECAM MODIFY SGU SOFTWARE ALL

. 015

NAVIGATION - G.P.W.S. - INTRODUCE MODE 5 CONTROL SWITCH ALL

. 026

NAVIGATION - EFIS - MODIFY SGU SOFTWARE ALL

. 026

FIRE PROTECTION - ENGINE AND APU FIRE DETECTION - MODIFY FIRE WARNING SYSTEM ALL

. 015

ELECTRICAL POWER - MODIFY GCU SOFTWARE ALL

6845 ...... ........... 6875 ...... ........... 6908 ...... ........... 6970 ...... ........... 7008 ...... ........... 7187 ...... ...........

7259 ...... ........... 7288 ...... ........... 7307 ...... ........... 7340 ...... 26-6038 03 7341 ...... ...........

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REVISION : 029

VALIDITY

. 017

HYDRAULIC POWER - REPLACE RESERVOIR HYDRAULI FLUID QUANTITY INDICATORS. ALL

. 023

FUEL - MODIFY TAIL TANK PUMP CONTROL. ALL

. 015

NAVIGATION - FMS - MODIFY SMITHS FMC SOFTWAR TO COMPLY WITH GE CF6.80.C2 ENGINES. ALL

. 015

PNEUMATIC - OPTIMIZE ENGINE BLEED AIR SUPPLY SYSTEM ALL

. 015

FIRE PROTECTION - DELETE BATTERY SMOKE DETECTOR AND WARNING LIGHT ALL

. 015

LIGHTS - EMERGENCY LIGHTING - MODIFY AUTOMATIC SWITCHING MODE OF THE FPEEPMS ALL

. 025

AUTO FLIGHT - FAC - MODIFY SOFTWARE ALL

. 019

NAVIGATION - ATC - INSTALL ATC MODE/S ALL

. 019

ELECTRICAL POWER - MODIFY CONTACTOR DC TIE LOGIC ALL

. 017

LIGHTS - EMERGENCY LIGHTING - INSTALL FLOOR PATH MARKING AND LIGHTING (GRIMES) ALL

. 016

AIR CONDITIONING - INCREASE AIR CONDITIONING FLOW AND PASSENGER FLOOR STRUCTURE SUBSTANTIATION ALL

. 017

FIRE PROTECTION - MODIFY CARGO COMPARTMENT FIRE EXTINGUISHING SQUIBTESTS CIRCUIT ALL

7383 ...... ........... 7421 ...... ........... 7460 ...... ........... 7483 ...... ........... 7563 ...... ........... 7720 ...... ........... 7764 ...... 34-6026 14 7770 ...... ........... 7824 ...... ........... 7866 ...... ...........

8009 ...... 26-6017 04

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. 020

8099 ...... 26-6017 04

FIRE PROTECTION - MODIFY CARGO COMPARTMENT FIRE EXTINGUISHING SQUIBTESTS CIRCUIT G-MONR G-MONS

. 020

FUEL - TRIM TANK - INSTALL WATER SCAVENGE SYSTEM ALL

8679 ...... 28-6028 05

. 025

8834 22-6014

REVISION : 029

......

10778 ...... 31-6051 04

AUTO FLIGHT - FAC - MODIFY SOFTWARE ALL

. 021

INDICATING/RECORDING SYSTEMS - PROVIDE ALTERNATE SOURCE OF CG MONITORING ALL

. 023

FLIGHT CONTROLS - INHIBIT RUDDER TRIM CONTROL WITH YAW AUTO PILOT ENGAGED ALL

. 022A 11454 ...... 22-6032 02

AUTO FLIGHT - AUTO PILOT - PROVIDE PITCH DISCONNECTION BY STICK-FORCE APPLICATION IN ALL FLIGHT PHASES ALL

N 029

NAVIGATON - EGPWS - ACTIVATE ENHANCED FUNCTIONS OF EGPWS ALL

. 026A 11900 ...... 22-6038 01

AUTO FLIGHT-AUTOPILOT/FLIGHT DIRECTORINTRODUCE A310-A300/600 STANDARD P/N B 470ADM ALL

. 028

NAVIGATION - EGPWS - INHIBIT AUTOMATIC DEACTIVATION ALL

. 026

NAVIGATION - EGPWS - INSTALLATION OF EGPWS OLD SPEC ---> (BFE) ALL

. 026

NAVIGATION - GPWS - PROVIDE FMS1 INPUT INSTEAD OF IRS1 ALL

11442 ...... 27-6031 03

11894 ...... 34-6127 11

12062 ...... 34-6127 11 12161 ...... 34-6126 11 12255 ...... 34-6129 07

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REVISION : 029

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. 028

AUTO-FLIGHT-ELECTRIC PITCH TRIM-REPLACE OLD FAC SOFTWARE BY NEW ONE WITH
THETA TRIM
FUNCTION G-MONR G-MAJS

N 029

DOORS - FIXED INTERIOR DOORS IN PAX COMPARTMENT - INSTALL ELECTRICAL COCKPIT DOOR RELEASE (SHORT COCKPIT) ALL

N 029

DOORS - COCKPIT DOOR RELEASE SYSTEM INSTALL ELECTRICAL OVERRIDE SYSTEM FOR MMEL DISPATCH (SHORT COCKPIT) ALL

N 029

EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - INSTALL DECOMPRESSION PANEL IN COCKPIT DOOR (SHORT COCKPIT) ALL

12557 ...... 25-6169 03

12671 ...... 52-6068 01

12693 ...... 25-6176 01

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