A319 A320 A321 飞机维护手册 AMM Aircraft Maintenance Manual 36.pdf467页

__________ 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 REVISION INDICATING NEW,REVISED, AND/OR DELETED PAGES T. OF C. REVISED TO REFLECT THIS REVISION 25 56-11-00 EFFECTIVITY UPDATED 1, 8- EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 12 56-11-11 401- 405, 408- 449 EFFECTIVITY UPDATED MOD.27156P9303 INCORPORATED FUSELAGE - MAIN STRUCTURE IMPROVE INSTALLATION OF COCKPIT WINDOWS TECHNICAL CORRECTIONS REVISED CLEARANCES. LAYOUT IMPROVED/MATERIAL RELOCATED WARNING/NOTE/REASON FOR THE JOB AMENDED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) CORRECTION/ADDITION/AMPLIFICATION ADDED NOTE.

001-049, 101-149, 151-199, 201-299, 301-399, 401-499, 109-149, 401-499, 001-049, 151-199, ALL ALL 001-049, 151-199, ALL 051-099, 101-108, 201-299, 301-399, 051-099, 101-108, 201-299, 301-399,

56-11-11 602- 603, 605, 611612 56-11-12 408- 409, 411- 428

EFFECTIVITY UPDATED MOD.27156P9303 INCORPORATED FUSELAGE - MAIN STRUCTURE IMPROVE INSTALLATION OF COCKPIT WINDOWS CORRECTION/ADDITION/AMPLIFICATION REVISED CURE TIME FOR DAPCO 72. CIRCUIT BREAKER(S) DATA UPDATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)

109-149, 401-499, 051-099, 001-049, 201-299, 001-049, 201-299, 101-149, 301-399, 101-149, 301-399, 151-199, 401-499, 151-199, 401-499,

56-11-12 613- 634

EFFECTIVITY UPDATED CIRCUIT BREAKER(S) DATA UPDATED

001-049, 101-149, 151-199, 56-HIGHLIGHTS Page REVISION NO. 30 1 of 2 Aug 01/05

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