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 24
L.E.P. 1- 9 REVISED TO REFLECT THIS REVISION INDICATING
NEW,REVISED, AND/OR DELETED PAGES
T. OF C. REVISED TO REFLECT THIS REVISION
1-24
24-ECAM MOD.30352P6562 INCORPORATED
101- 145 ELECTRICAL POWER - AC GENERATION -
ADAPT NEW ELECTRICAL GENERATION CONCEPT
ON CFM56-5A/5B ENGINES
MOD.32875P7945 INCORPORATED
ELECTRICAL POWER - AC MAIN GENERATION-
INSTALL NEW GCU SOFTWARE STD 5.1 ON SA
A/C EQUIPPED WITH ENHANCED EPGS
24-LOCAL MOD.27140P4801 INCORPORATED
101- 106 ELECTRICAL POWER-GENERAL-DEFINE NEW
ELECTRICAL GENERATION CONCEPT FOR
SINGLE AISLE A/C
24-OBSV MOD.27140P4801 INCORPORATED
102, 106- ELECTRICAL POWER-GENERAL-DEFINE NEW
113 ELECTRICAL GENERATION CONCEPT FOR
SINGLE AISLE A/C
24-CFDS MOD.23529P3112 INCORPORATED
101- 114 NAVIGATION - INSTALL A TCAS II COLLINS
SYSTEM
MOD.27140P4801 INCORPORATED
ELECTRICAL POWER-GENERAL-DEFINE NEW
ELECTRICAL GENERATION CONCEPT FOR
SINGLE AISLE A/C
MOD.28138P5905 INCORPORATED
COMMUNICATIONS-SATELLITE COMMUNICATION-
INSTALL A COLLINS AERO I SATCOM AVIONIC
(6 CHANNELS)
MOD.28208P5932 INCORPORATED
COMMUNICATIONS-SATELLITE COMMUNICATION-
INSTALL COLLINS AERO I SATCOM AVIONIC
401-499,
401-499,
401-499,
401-499,
ALL
106-149, 229-299, 303-399,
401-499,
401-499,
401-499,
CES
CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
(3 CHANNELS)
MOD.32004P7572 INCORPORATED 106-149, 229-299, 303-399,
ELECTRICAL POWER INTEGRATED DRIVE 401-499,
GENERATOR SYSTEM-INTRODUCE NEW GCU AND
GAPCU SOFWARES STD 5.0
24-00-00 EFFECTIVITY UPDATED
204- 258 MOD.20141P0115 INCORPORATED 401-499,
POWER PLANT - ENGINE - INSTALL
CFM 56-5A1 ENGINE RATED AT 25.000 LBS
MOD.23083P2566 INCORPORATED 401-499,
POWER PLANT - INSTALL CFM 56-5B1 ENGINES
RATED AT 30.000 LBS FOR A321.
MOD.30352P6562 INCORPORATED 106-149, 229-299, 303-399,
ELECTRICAL POWER - AC GENERATION -401-499,
ADAPT NEW ELECTRICAL GENERATION CONCEPT
ON CFM56-5A/5B ENGINES
MOD.30626K6443 INCORPORATED ALL
AIR CONDITIONING-AIR COOLING-
INSTALL A NEW ECS
MOD.32004P7572 INCORPORATED 106-149, 229-299, 303-399,
ELECTRICAL POWER INTEGRATED DRIVE 401-499,
GENERATOR SYSTEM-INTRODUCE NEW GCU AND
GAPCU SOFWARES STD 5.0
MOD.35481P9181 INCORPORATED ALL
AIR CONDITIONNING-AIR COOLING-REMOVE
A318 TYPE ECS FROM A320 FURTHER TO MSCN
REJECTION. ANTI-MOD TO MOD 33780
MOD.35482P9182 INCORPORATED ALL
AIR CONDITIONNING-AIR COOLING-REMOVE
A318 TYEP ECS FROM A321 FURTHER TO MSCN
REJECTION. ANTI-MOD OF MOD 33827
LAYOUT IMPROVED/MATERIAL RELOCATED ALL
CIRCUIT BREAKER(S) DATA UPDATED ALL
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) ALL
24-20-00 EFFECTIVITY UPDATED
201-D201 MOD.20249P0342 INCORPORATED 401-499,
INSTALLATION OF SUNDSTRAND ELECTRICAL SUPPLY
(TYPE A310) ON A/C A320 N 1 (WIRING)
MOD.20349P0468 INCORPORATED 401-499,
ELECTRICAL POWER - MODIFY BTC1 CONTACTOR
SUPPLY POWER
MOD.20589P0993 INCORPORATED 401-499,
ELECTRICAL GENERATION-SEGREGATION OF BATTERY
POWER CENTER WITH REGARD TO NORMAL
GENERATION POWER CEN TER (120VU)
MOD.22278P2640 INCORPORATED 401-499,
CES
CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE
REFERENCE OF THE THREE PHASE 50A
CIRCUIT-BREAKER
MOD.22448P2640 INCORPORATED 401-499,
ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE
REFERENCE OF THE THREE PHASE 50A
CIRCUIT-BREAKER
CORRECTION/ADDITION/AMPLIFICATION 001-049, 051-099, 101-149,
REPLACED AWM BY ESPM CROSS-REFERENCE 151-199, 201-299, 301-399,
LAYOUT IMPROVED/MATERIAL RELOCATED ALL
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 1
