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A320飞机维护手册 AMM AIR 空气

日期: 2011-03-27 17:07:36

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 75 L.E.P. 1...

A320飞机维护手册 AMM 发动机燃油和控制 ENGINE FUEL AND CONTRO

日期: 2011-03-27 17:01:24

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 73 L.E.P. 1...

A320飞机维护手册 AMM ENGINE 发动机 2

日期: 2011-03-27 16:58:50

3. Job Set-up __________ Subtask 72-23-00-941-085 A. Safety Precautions (1) On the center pedestal, on the ENG panel 115VU: (a) Put a warning notice to tell persons not to start the engine. (2) Make sure that the engine 1(2) shutdown occur...

A320飞机维护手册 AMM ENGINE 发动机 1

日期: 2011-03-27 16:55:51

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 72 L.E.P. 1...

A320飞机维护手册 AMM OIL 滑油

日期: 2011-03-27 12:59:21

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 79 L.E.P. 1...

A320飞机维护手册 AMM 动力装置 POWER PLANT 2

日期: 2011-03-27 12:57:20

(Ref. Fig. 401/TASK 71-22-11-991-300) Subtask 71-22-11-020-051 A. Removal of the Aft Engine Mount. NOTE : Removal of the hardware that attach the aft engine mount to the ____ engine is the same at the three engine flanges. (1) Remove the r...

A320飞机维护手册 AMM 动力装置 POWER PLANT 1

日期: 2011-03-27 12:54:10

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 71 L.E.P. 1...

A320飞机维护手册 AMM WINGS 机翼5

日期: 2011-03-27 12:52:14

(3) Remove and discard the cover(s) from the applicable inspection hole(s) on the front spar. (4) Make sure that the applicable inspection hole is clear of unwanted material. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,...

A320飞机维护手册 AMM WINGS 机翼4

日期: 2011-03-27 12:50:25

R (b) Set the access panel (2) so that: R - dimension X is between 0.1 mm (0.0039 in.) and 4.3 mm (0.1692 R in.) along the full length of the panel. Try and set the R clearance as near as possible to 2.0 mm (0.0787 in.). R - dimension Z is...

A320飞机维护手册 AMM WINGS 机翼3

日期: 2011-03-27 12:43:00

-the clearance between the wing-skin and the edges of the panels. The clearance must be not less than 0.5 mm (0.0196 in.). Subtask 57-41-37-390-050 B. Seal Installation (Ref. Fig. 805/TASK 57-41-37-991-017) NOTE : The procedure that follow...

A320飞机维护手册 AMM WINGS 机翼2

日期: 2011-03-27 12:40:41

5. Close-up ________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499, Subtask 57-21-00-410-070 A. Close Access (1) Make sure that the work area is clean and clear of tool(s) and other items. (2) Install the applicable acces...

A320飞机维护手册 AMM WINGS 机翼1

日期: 2011-03-27 12:37:55

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 57 L.E.P. 1-18 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM IGNITION 点火

日期: 2011-03-27 09:01:39

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 74 L.E.P. 1...

A320飞机维护手册 AMM STANDARD PRACTICES - ENGINES

日期: 2011-03-27 09:00:01

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 70 L.E.P. 1...

A320飞机维护手册 AMM WINDOWS 风挡 窗户

日期: 2011-03-27 08:58:10

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 56 L.E.P. 1- 4 REVISED TO REFLECT THIS RE...

A320飞机维护手册 AMM STABILIZERS 安定面

日期: 2011-03-27 08:55:33

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 55 L.E.P. 1- 4 REVISED TO REFLECT THIS RE...

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...