CES
CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
32-43-16 EFFECTIVITY UPDATED 401- 404, CIRCUIT BREAKER(S) DATA UPDATED 406- 414
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-43-27 EFFECTIVITY UPDATED 401- 410 CIRCUIT BREAKER(S) DATA UPDATED
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-43-31 EFFECTIVITY UPDATED 401- 402, CIRCUIT BREAKER(S) DATA UPDATED 404- 415, 418- 425 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-43-32 MOD.26925P4576 INCORPORATED
301- 305 LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE
BRAKING SYSTEM
NEW TOPIC/NEW CONFIGURATION
32-43-32 MOD.20011P0003 INCORPORATED
401- 420 ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20589P1002 INCORPORATED FLIGHT CONTROLS-MOD. OF THE LOGIC TO SWITCH ELAC 2 AND SEC 2 POWER SUPPLIES TO BATTERIES IN CASE OF EMERG. CONDITIONS MOD.22278P2640 INCORPORATED ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE REFERENCE OF THE THREE PHASE 50A CIRCUIT-BREAKER MOD.22448P2640 INCORPORATED ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE REFERENCE OF THE THREE PHASE 50A CIRCUIT-BREAKER MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM NEW TOPIC/NEW CONFIGURATION
32-43-34 MOD.20011P0003 INCORPORATED 401- 407 ELECTRICS- GENERATION- DISTRIBUTION-001-049, 051-099, 101-149,151-199, 201-299, 301-399,001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
001-049, 051-099, 101-149, 151-199, 201-299, 301-399,001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
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,
401-499,
401-499,
401-499,
401-499,
401-499,
401-499,
401-499,
401-499,
32-HIGHLIGHTS Page 16 of 28 REVISION NO. 30 Aug 01/05
CES CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20589P1002 INCORPORATED FLIGHT CONTROLS-MOD. OF THE LOGIC TO SWITCH ELAC 2 AND SEC 2 POWER SUPPLIES TO BATTERIES IN CASE OF EMERG. CONDITIONS MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM NEW TOPIC/NEW CONFIGURATION
32-43-35 MOD.20011P0003 INCORPORATED
401- 410 ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20589P1002 INCORPORATED FLIGHT CONTROLS-MOD. OF THE LOGIC TO SWITCH ELAC 2 AND SEC 2 POWER SUPPLIES TO BATTERIES IN CASE OF EMERG. CONDITIONS MOD.22278P2640 INCORPORATED ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE REFERENCE OF THE THREE PHASE 50A CIRCUIT-BREAKER MOD.22448P2640 INCORPORATED ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE REFERENCE OF THE THREE PHASE 50A CIRCUIT-BREAKER MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM NEW TOPIC/NEW CONFIGURATION
32-43-47 MOD.20011P0003 INCORPORATED
401- 407 ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20589P1002 INCORPORATED FLIGHT CONTROLS-MOD. OF THE LOGIC TO SWITCH ELAC 2 AND SEC 2 POWER SUPPLIES TO BATTERIES IN CASE OF EMERG. CONDITIONS MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM NEW TOPIC/NEW CONFIGURATION
401-499,
401-499,
401-499, 401-499,
401-499,
401-499,
401-499,
401-499,
401-499, 401-499,
401-499,
401-499,
401-499,
32-HIGHLIGHTS Page 17 of 28 REVISION NO. 30 Aug 01/05
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32-43-51 MOD.20011P0003 INCORPORATED
401- 413 ELECTRICS- GENERATION- DISTRIBUTION-V.U.'S AND AVIONICS- DEFINE SYSTEMS OF THE BASIC AIRCRAFT-MOD.20577P0907 INCORPORATED ELECTRICAL INSTALLATION-MODIFY CIRCUIT BREAKERS LO CATION IN 121VU MOD.20589P1002 INCORPORATED FLIGHT CONTROLS-MOD. OF THE LOGIC TO SWITCH ELAC 2 AND SEC 2 POWER SUPPLIES TO BATTERIES IN CASE OF EMERG. CONDITIONS MOD.22278P2640 INCORPORATED ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE REFERENCE OF THE THREE PHASE 50A CIRCUIT-BREAKER MOD.22448P2640 INCORPORATED ELECTRIC AND ELECTRONIC INSTALLATION - CHANGE REFERENCE OF THE THREE PHASE 50A CIRCUIT-BREAKER MOD.26925P4576 INCORPORATED LANDING GEAR-ALTERNATE BRAKING-INTRODUCE MODIFIED ALTERNATE BRAKING SYSTEM NEW TOPIC/NEW CONFIGURATION
32-44-00 TOPIC CANCELLED 1-12
32-44-00 01 SUPERSEDED BY CONFIGURATION(S) 1-12 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-44-00 02 MOD.26925P4576 INCORPORATED
1- 14 LANDING GEAR-ALTERNATE BRAKING-
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本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架1(7)
