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 REVISION INDICATING
T. OF C. 7-34 53-00-00 2, 4 NEW,REVISED, AND/OR DELETED PAGES REVISED TO REFLECT THIS REVISIONEFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-00-00 602- 604, 606, 609 EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-12-11 401- 402, 407- 408, 410- 411 CORRECTION/ADDITION/AMPLIFICATION ADDED REMOVAL OF THE THIRD OCCUPANT SEAT.
53-12-12 402- 403, 407- 408, 411, 415-416, 418, 420- 425 EFFECTIVITY UPDATEDEFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-15-11 408, 411, 414, 433, 436, 438, 443, 445-446, 451-452 EFFECTIVITY UPDATEDCORRECTION/ADDITION/AMPLIFICATION ADDED APPLICATION OF SEALANT FOR ARRESTORPICK-UP FITTING INSTALLATION.EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-15-11 602, 605, 608, 610-611, 613-615 CORRECTION/ADDITION/AMPLIFICATION REVISED INSPECTION PROCEDURE OF THE RADOMETO GIVE MORE INSTRUCTIONS FOR PERMANENTREPAIR AT SUBSEQUENT CHECK.
151-199, 401-499, 151-199, 401-499,ALL
001-049, 054-099, 101-149,151-199, 201-299, 301-399,401-499,
ALL
062-099, 106-149, 151-199,204-299, 301-399, 401-499,ALL
CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
53-15-11 CORRECTION/ADDITION/AMPLIFICATION ALL 802, 804 ADDED QUARTZ RADOME P/N D53132010000.
53-16-11 MOD.32088K7755 INCORPORATED ALL
401- 408 EQUIPMENT FURNISHINGS-CURTAINS AND PARTITIONS-MODIFIED INTRUSION AND PENETRATION RESISTANT COCKPIT DOOR SB 25-1305 06 INCORPORATED ALL EQUIPMENT/FURNISHINGS - PASSENGER COMPARTMENT
-INTRODUCE A MODIFIED INTRUSION AND PENETRA
TION RESISTANT COCKPIT DOOR
NEW TOPIC/NEW CONFIGURATION
53-19-00 EFFECTIVITY UPDATED 601- 610, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 612
53-19-41 EFFECTIVITY UPDATED 401- 408 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-19-42 EFFECTIVITY UPDATED 401- 411 CIRCUIT BREAKER(S) DATA UPDATED
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-20-00 EFFECTIVITY UPDATED 1, 3, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 8, 11,
15, 18-
20
53-21-00 EFFECTIVITY UPDATED 626, 629-MOD.25141P3955 INCORPORATED 632, 674-NACELLES/PYLONS-PYLON STRUCTURE-678, 681, ADAPT PRIMARY STRUCTURE TO A321-200 684, 692, VERSION 694, 697, LAYOUT IMPROVED/MATERIAL RELOCATED
A600-A606, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
A624-A628,
A644-A648,
A667-A670,
A696-B603
53-22-12 EFFECTIVITY UPDATED
ALL
001-049, 054-099, 101-149,
151-199, 201-299, 301-399,
401-499,
001-049, 054-099, 101-149,
151-199, 201-299, 301-399,
401-499,
106-149, 154-199, 207-299,
301-399, 401-499,
106-149, 154-199, 207-299,
301-399, 401-499,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
401-499,
301-399,
ALL
001-049, 051-099, 101-149,
151-199, 201-299, 401-499,
53-HIGHLIGHTS Page 2 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
401- 402, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
404, 408-
410
53-22-14 EFFECTIVITY UPDATED
402, 406- EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
419
53-25-11 EFFECTIVITY UPDATED
401- 404, MOD.30626K6443 INCORPORATED
406- 414 AIR CONDITIONING-AIR COOLING-
INSTALL A NEW ECS
MOD.35481P9181 INCORPORATED
AIR CONDITIONNING-AIR COOLING-REMOVE
A318 TYPE ECS FROM A320 FURTHER TO MSCN
REJECTION. ANTI-MOD TO MOD 33780
MOD.35482P9182 INCORPORATED
AIR CONDITIONNING-AIR COOLING-REMOVE
A318 TYEP ECS FROM A321 FURTHER TO MSCN
REJECTION. ANTI-MOD OF MOD 33827
CIRCUIT BREAKER(S) DATA UPDATED
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-29-00 EFFECTIVITY UPDATED
1, 3 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
53-29-41 EFFECTIVITY UPDATED
401- 402, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
404, 407,
409
53-30-00 EFFECTIVITY UPDATED
1, 3, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
5
53-31-00 EFFECTIVITY UPDATED
6-9, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
15-16
53-31-00 EFFECTIVITY UPDATED
624, 627- CORRECTION/ADDITION/AMPLIFICATION
628, 635- STORAGE PRESERVATION MATERIAL REFERENCE
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