27-HIGHLIGHTS Page 9 of 17 REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
27-54-55 EFFECTIVITY UPDATED
402-A404 MOD.31446K6889 INCORPORATED
WINGS-INBOARD FLAP-INTRODUCE OPTIMIZED
DRIVE STRUT TRACK 1/2 DESIGN
MOD.32419K7879 INCORPORATED
WINGS - INBOARD FLAP - SIMPLIFY
ATTACHEMENT DESIGN FLAP TO TRACK 2
CORRECTION/ADDITION/AMPLIFICATION
MINOR TEXT CHANGES TO STEP (2).
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
27-54-61 EFFECTIVITY UPDATED
401- 404, CORRECTION/ADDITION/AMPLIFICATION
406, 408- TORQUE ADAPTOR 98D27504035000 REFERENCE
410, 414- ADDED.
421, 423- CIRCUIT BREAKER(S) DATA UPDATED
438, 440-
A443 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
27-54-61 EFFECTIVITY UPDATED
602- 604, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
606- 608
27-54-62 EFFECTIVITY UPDATED
401- 434, TITLE OF TASK(S) DATA UPDATED
478- 479, CIRCUIT BREAKER(S) DATA UPDATED
481- 482,
484- 485, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
487
27-54-62 EFFECTIVITY UPDATED
602- 604, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
606- 607
27-54-63 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
404, 410
27-55-00 EFFECTIVITY UPDATED
1-2, CORRECTION/ADDITION/AMPLIFICATION
4, 6, FIGURE TITEL CLARIFIED.
8-10 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
27-60-00 EFFECTIVITY UPDATED
201, 203- TECHNICAL CORRECTIONS
205 ADDED A NEW STEP TO MAKE SURE THAT THE
CES
106-149, 159-199, 211-299,401-499,
106-149, 213-299, 401-499,
001-049, 051-099, 101-105,151-158, 201-210, 301-399,001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
001-049, 051-099, 101-149,151-199, 201-299, 401-499,
001-049, 051-099, 101-149,151-199, 201-299, 401-499, 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
001-049, 051-099, 101-149,151-199, 201-299, 401-499,
ALL
001-049, 051-099, 101-149,
151-199, 201-299, 401-499,
001-049, 051-099, 101-149,
151-199, 201-299, 401-499,
001-049, 051-099, 101-149,151-199, 201-299, 401-499,
001-049, 051-099, 101-149,151-199, 201-299, 401-499,
ALL
106-149, 303-399, 401-499,
ALL
27-HIGHLIGHTS Page 10 of 17 REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
SERVOCONTROL IS IN OPERATION POSITION.
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
27-64-00 EFFECTIVITY UPDATED
1, 3, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
5
27-64-00 EFFECTIVITY UPDATED
401- 403, TECHNICAL CORRECTIONS
406- 413 REVISED NOTE TO EXPLAIN THAT
NO ACTION IS REQUIRED ON THE SYMMETRIC
SPOILER SERVOCONTROL.
WARNING/NOTE/REASON FOR THE JOB AMENDED
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
27-64-00 EFFECTIVITY UPDATED
514, 533- CIRCUIT BREAKER(S) DATA UPDATED
542 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
27-64-41 EFFECTIVITY UPDATED
402- 403, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
406, 408-
409, 412,
414- 415,
421- 423,
429- 432
27-64-41 EFFECTIVITY UPDATED
602- 603, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
606
27-64-42 EFFECTIVITY UPDATED
402- 403, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
406, 408-
409, 412,
414- 415,
418- 420,
426- 428
27-64-42 EFFECTIVITY UPDATED
602- 603, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
606
27-64-43 EFFECTIVITY UPDATED
CES
001-049, 052-099, 101-149,
151-199, 201-299, 301-399,
401-499,
151-199, 401-499,
ALL
ALL
001-049, 052-099, 101-149,
151-199, 201-299, 301-399,
401-499,
151-199, 401-499,
151-199, 301-399, 401-499,
004-049, 053-099, 101-149,
151-199, 201-299, 301-399,
401-499,
004-049, 053-099, 101-149,
151-199, 201-299, 401-499,
004-049, 053-099, 101-149,
151-199, 201-299, 301-399,
401-499,
004-049, 053-099, 101-149, 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵1(4)
