001-049, 051-099, 101-149,151-199, 201-299, 401-499,
001-049, 051-099, 101-101,106-149, 201-299, 301-399, 401-499,
ALL
ALL
ALL
001-049, 051-099, 101-149, 151-199, 201-299, 301-399,001-049, 051-099, 101-149, 151-199, 201-299, 301-399, 401-499,
151-199, 401-499,
151-199, 401-499,
151-199, 401-499,
151-199, 401-499,
ALL
001-049, 051-099, 101-149,
 53-HIGHLIGHTS Page 3 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES

655, 657-658, 660, 668, 671-672, 674-675, 677-679, 690-692, 694, 697,A609-A612,A614-A616,A634, A669,A673-A675,A677-A678,A680-A681,A683, A686,A690-A691,A693, A696,B600-B601,B603, B606,B610-B611,B613, B616-B617, B620-B621, B623,B625-B626 
53-31-00 703  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-32-00 1  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-32-12 401- 403, 407- 409  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-35-00 601- 602, 605, 607, 612- 614, 619- 620  EFFECTIVITY UPDATEDMOD.20003K0002 INCORPORATED STRUCTURE- REAR FUSELAGE- DEFINESECTIONS 16,17,18,19 OF THE BASICAIRCRAFT -LAYOUT IMPROVED/MATERIAL RELOCATED EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-35-11 401- 402, 404, 406, 408, 410,  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
CES 

151-199, 201-299, 301-399,401-499,
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

ALL
001-049, 051-099, 101-149,
 151-199, 201-299, 401-499,

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

 53-HIGHLIGHTS Page 4 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES

431- 432,
 436- 440,
 445- 448 
53-35-13  EFFECTIVITY UPDATED
 402- 403,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
405, 408, 
413, 415-
421, 425-
426, 428-
430, 432,
 435, 437,
 442- 445 
53-40-00  EFFECTIVITY UPDATED
 1, 3,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
5 
53-41-00  EFFECTIVITY UPDATED
 617, 620,  MOD.23643K3245 INCORPORATED 
635- 636,  FUSELAGE - FLOOR PANELS - INTRODUCE
 638- 640,  CFRP IN PAX COMPARTMENT
 651, 654,  CORRECTION/ADDITION/AMPLIFICATION 
A611,A613,  NTM REFERENCE ADDED. 
A615,A620,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
A656,A660, 
A676,A681, 
A686-A687, 
A695,A698-
A699,B601, 
B603,B606, 
B609-B610, 
B612,B614, 
B617-B618, 
B620,B622, 
B641-B642, 
B644-B645, 
B648,B651-
B652,B658, 
B661-B662, 
B666,B668, 
B670,B674-
B676,B678, 
B681,B698-
B699,C601-
C604,C631, 
C635-C648,

001-049, 051-099, 101-149,151-199, 201-299, 401-499,
151-199, 201-220, 222-223,225-227, 229-299, 301-399, 401-499,
ALL
301-399,
001-049, 051-099, 101-149, 151-199, 201-299, 401-499, CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES

C655-C657, C660 
53-41-00 705, 715, 718  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-42-12 401- 402, 404, 408-409  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-42-14 402, 404, 407- 414  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-42-17 402- 403, 409- 418  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-43-00 1, 3  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-43-11 401- 402, 404, 407-408  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-49-21 402- 403, 405, 408-412  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-56-11 402- 403, 406- 407, 410- 412, 415- 416, 420- 421  EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 
53-58-11 401- 454  EFFECTIVITY UPDATEDMOD.22003K2103 INCORPORATED PNEUMATIC - ADAPT SYSTEM TO A321 DEFINITION CIRCUIT BREAKER(S) DATA UPDATED 
CES 

151-199, 401-499,
151-199, 401-499,
001-049, 051-099, 101-101,106-149, 201-299, 301-399, 401-499,
151-199, 201-220, 222-223,225-227, 229-299, 301-399, 401-499,
151-199, 401-499,
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FUSELAGE 機身1(2)