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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
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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
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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 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
