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 FUSELAGE 机身1(2)
