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A320飞机维护手册 AMM NACELLES/PYLONS

日期: 2011-03-27 08:52:56

HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 54 L.E.P. 1- 4 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM FUSELAGE 机身3

日期: 2011-03-27 08:50:16

Detailed Visual Inspection of AFT Cargo Door Lock Fittings and Surrounding Structure between FR53 and FR55A from Stringer 41 RH to Door Sill (6 places) 1. Reason for the Job __________________ Refer to the MPD TASK: 534156-01 2. Job Set-up...

A320飞机维护手册 AMM FUSELAGE 机身2

日期: 2011-03-27 08:47:27

3. Job Set-up __________ Subtask 53-21-00-010-070 A. Get Access (1) Put an access platform in position at the zone 825. (2) Open the forward cargo-compartment door 825 (Ref. TASK 52-30-00-860-001). R **ON A/C 001-049, 051-099, 101-149, 201...

A320飞机维护手册 AMM FUSELAGE 机身1

日期: 2011-03-27 08:44:13

HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 53 L.E.P. 1-14 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM DOORS 舱门8

日期: 2011-03-27 00:08:25

R R R 1. On the ECAM control panel, push the DOOR key: 2. On the circuit breaker panel 121VU: - open the circuit breaker 2WV. - open the circuit breakers 15WN and 2WW. 3. On the circuit breaker panel 121VU: - close the circuit breakers 2WV...

A320飞机维护手册 AMM DOORS 舱门7

日期: 2011-03-27 00:06:38

R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 52-42-00Page 414 1201-299, 1May 01/05 1 1 1CES 1R **ON A/C 106-149, 151-199, 201-299, 301-399, 401-499, Subtask 52-42-00-860-051 B. Put the aircraft back to its initial configuration. (1) Set...

A320飞机维护手册 AMM DOORS 舱门6

日期: 2011-03-27 00:00:11

R **ON A/C 401-499, R 52-32-21-991-019-C Fig. 403C **ON A/C 001-049, 053-099, 101-105, 201-220, 52-32-21-991-017 Fig. 417 **ON A/C 106-149, 221-299, 301-399, 52-32-21-991-017-B **ON A/C 151-199, Fig. 417A R 52-32-21-991-017-A **ON A/C 401-...

A320飞机维护手册 AMM DOORS 舱门5

日期: 2011-03-26 23:57:46

1EFF : ALL 1 52-32-00Page 71 1 1 Aug 01/05 1 1 1CES 1 The sequence shaft operates the link assy at the same time so that the target lever moves to the door sill. The related target operates the proximity switch 32WV (Ref. 52-71-00). When t...

A320飞机维护手册 AMM DOORS 舱门4

日期: 2011-03-26 23:54:35

3. Job Set-up __________ Subtask 52-30-00-860-050 A. Aircraft Maintenance Configuration (1) Make sure that the Yellow hydraulic system reservoir is pressurized (Ref. TASK 29-14-00-614-002). (2) Make sure that the level of the hydraulic flu...

A320飞机维护手册 AMM DOORS 舱门3

日期: 2011-03-26 23:52:04

4. Procedure _________ Subtask 52-13-31-020-051 A. Removal of the Stop Fittings (Ref. Fig. 402/TASK 52-13-31-991-002) (1) Remove the old sealant with CLEANING AGENTS (Material No. 11-004), MISCELLANEOUS (Material No. 19-003) and a non meta...

A320飞机维护手册 AMM DOORS 舱门2

日期: 2011-03-26 23:42:34

(b) With the door in the down position (door closed and locked): -make sure that the clearance J11 between the frame structure and the safety pin is 4 -1 +1 mm (0.1574 -0.0393 +0.0393 in.). (c) If the clearances J10 and J11 are not in the...

A320飞机维护手册 AMM DOORS 舱门1

日期: 2011-03-26 23:38:56

HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 52 L.E.P. 1-33 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM STANDARD PRACTICES AND STRUCTURES

日期: 2011-03-26 14:51:29

HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 51 L.E.P. 1- 2 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER 6

日期: 2011-03-26 14:47:34

| high | | ----+----------------------------------------+-------------------------+------- ------------------------------------------------------------------------------- FCN | Fault Description | CFDS Message | Class ----+----------------...

A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER5

日期: 2011-03-26 14:43:57

______________________ A. Fixtures, Tools, Test and Support Equipment -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ----------------------------------------------------------------...

A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER4

日期: 2011-03-26 14:41:53

Subtask 49-23-51-865-059 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD. Subtask 49-23-51-710-051 C. Do the operational test of the APU (Ref. TASK 49-00-00-710-008). (1) Do a check for leaks...

A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER3

日期: 2011-03-26 14:39:37

R EFF : 001-049, 101-105, 107-107, 151-199, 49-16-41Page 408 201-210, Config-2 Aug 01/05 CES DIVERTER - REMOVAL/INSTALLATION _______________________________ TASK 49-16-41-000-004 Removal of the fixed APU Diverter (APS 3200) 1. Reason for t...

A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER2

日期: 2011-03-26 14:35:49

5. Close-up ________ Subtask 49-11-00-410-051 A. Close Access (1) Make sure that the work area is clean and clear of tool(s) and other items. (2) Set the LIGHT control switch 11LJ to the off position. (3) Close the APU access doors 315AL,...

A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER1

日期: 2011-03-26 14:32:10

HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 49 L.E.P. 1-24 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM 起动 STARTING

日期: 2011-03-26 09:26:44

F E E C F M 『EE E E 56-5B EE HIGHLIGHTS __________ REVISION NO. 30 Aug 01/05 Pages which have been revised are outlined below, together with the Highlights of the Revision CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES CHAPTER 80 L.E.P. 1...