F E E  C F M  『EE 
 E E  56-5B  EE
 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 73
L.E.P.
 1- 8 REVISED TO REFLECT THIS REVISION INDICATING NEW,REVISED, AND/OR DELETED PAGES
T.
 OF C.  REVISED TO REFLECT THIS REVISION 1-10
73-00-00  EFFECTIVITY UPDATED 1, 4, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 106-149, 212-299, 301-399, 8-9 401-499, 
73-10-00 EFFECTIVITY UPDATED
 1, 30, EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 001-049, 051-099, 101-149, 34, 36-151-199, 201-299, 301-399, 37 401-499, 
73-11-10 MOD.20011P0003 INCORPORATED ALL 401- 403, ELECTRICS- GENERATION- DISTRIBUTION-405, 407-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF 416 THE BASIC AIRCRAFT-
CORRECTION/ADDITION/AMPLIFICATION ALL REVISED PROCEDURE LAYOUT IMPROVED/MATERIAL RELOCATED ALL MODIFIED MALFUNCTION WORDING STRUCTURE ALL 
73-11-10 EFFECTIVITY UPDATED 624- 626 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 106-149, 212-299, 301-399, 401-499, 
73-11-10 MOD.20011P0003 INCORPORATED  ALL
 801- 806  ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF
 THE BASIC AIRCRAFT-LAYOUT IMPROVED/MATERIAL RELOCATED ALL
73-11-49 CORRECTION/ADDITION/AMPLIFICATION ALL 401- 402, ADDED CLOSING OF THE LP FUEL VALVE 407, 409-LAYOUT IMPROVED/MATERIAL RELOCATED ALL 410
 73-HIGHLIGHTS Page 1 of REVISION NO. 30 Aug 01/05
 CES
 F  『 
 E  C F M  E 
 E  E 
 E  56-5B  E 
 E  E 
CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES 
73-11-50  MOD.20011P0003 INCORPORATED  
401- 403,  ELECTRICS- GENERATION- DISTRIBUTION- 
408- 409,  V.U.'S AND AVIONICS- DEFINE SYSTEMS OF 
 413  THE BASIC AIRCRAFT- 
CORRECTION/ADDITION/AMPLIFICATION  
DELETED "FIRE SHUT OFF VALVE" TEST. 
 LAYOUT IMPROVED/MATERIAL RELOCATED  
73-20-00  EFFECTIVITY UPDATED 
 1,A021,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
A024,A026- 
A029  
73-21-10  MOD.20011P0003 INCORPORATED  
401- 403,  ELECTRICS- GENERATION- DISTRIBUTION- 
416, 424- V.U.'S AND AVIONICS- DEFINE SYSTEMS OF 
 426  THE BASIC AIRCRAFT- 
CORRECTION/ADDITION/AMPLIFICATION  
ADDED CAUTIONS 
 LAYOUT IMPROVED/MATERIAL RELOCATED  
73-21-60  EFFECTIVITY UPDATED 
 402- 403,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
410, 414- 
415, 418  
73-21-60  EFFECTIVITY UPDATED 
 511- 512,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
514, 516- 
517, 519,  
522- 523, 
 525, 527- 
528, 530, 
 532- 533, 
 535, 537- 
540  
73-21-90  EFFECTIVITY UPDATED 
 401, 405- EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
407, 409- 
411  
73-21-90  EFFECTIVITY UPDATED 
 501- 505,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
510- 512,  
514- 525  
73-25-00  EFFECTIVITY UPDATED 
 CES 
ALL
ALL
ALL 
063-099, 106-149, 153-199, 205-299, 301-399, 401-499, 
ALL
ALL
ALL 
051-055, 057-057, 059-060,106-149, 159-199, 210-299,301-399, 401-499, 
051-055, 057-057, 059-060,106-149, 212-299, 301-399,401-499,
063-099, 106-149, 153-199,205-299, 301-399, 401-499,
063-099, 106-149, 153-199,205-299, 301-399, 401-499,
 73-HIGHLIGHTS Page 2 of REVISION NO. 30 Aug 01/05CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
 F  『 
 E  C F M  E 
 E  E 
 E  56-5B  E 
 E  E 
76, 79,  EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
81  
73-25-34  CIRCUIT BREAKER(S) DATA UPDATED  
401- 402,  
406  
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)  
73-25-34  MOD.30626K6443 INCORPORATED  
501  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  
 
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 发动机燃油和控制 ENGINE FUEL AND CONTRO