401-499,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
005-049, 055-099, 101-149,
151-199, 201-299, 301-399,
401-499,
005-049, 055-099, 101-149,
151-199, 201-299, 301-399,
401-499,
401-499,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
401-499,
401-499,
401-499,
401-499,
401-499,
32-HIGHLIGHTS Page 25 of 28
REVISION NO. 30 Aug 01/05
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 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 MOD.31152P7000 INCORPORATED LANDING GEAR-STEERING-SUPPLY NOSE WHEEL STEERING WITH YELLOW HYDRAULIC POWER IN PLACE OF GREEN HYDRAULIC POWER NEW TOPIC/NEW CONFIGURATION
32-51-22 MOD.20011P0003 INCORPORATED
401- 409 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 MOD.31152P7000 INCORPORATED LANDING GEAR-STEERING-SUPPLY NOSE WHEEL STEERING WITH YELLOW HYDRAULIC POWER IN PLACE OF GREEN HYDRAULIC POWER NEW TOPIC/NEW CONFIGURATION
32-51-23 MOD.20011P0003 INCORPORATED 401- 412 ELECTRICS- GENERATION- DISTRIBUTION-
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 26 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.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 MOD.31959P7545 INCORPORATED LANDING GEAR - STEERING - MODIFY NOSE WHEEL STEERING HYDRAULIC BLOCK NEW TOPIC/NEW CONFIGURATION
32-51-42 MOD.31152P7000 INCORPORATED
402- 414 LANDING GEAR-STEERING-SUPPLY NOSE
WHEEL STEERING WITH YELLOW HYDRAULIC
POWER IN PLACE OF GREEN HYDRAULIC POWER
TITLE OF TASK(S) DATA UPDATED
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-51-43 EFFECTIVITY UPDATED
402- 409 MOD.31152P7000 INCORPORATED
LANDING GEAR-STEERING-SUPPLY NOSE
WHEEL STEERING WITH YELLOW HYDRAULIC
POWER IN PLACE OF GREEN HYDRAULIC POWER
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
32-51-51 EFFECTIVITY UPDATED
402- 430 MOD.31152P7000 INCORPORATED
LANDING GEAR-STEERING-SUPPLY NOSE
WHEEL STEERING WITH YELLOW HYDRAULIC
POWER IN PLACE OF GREEN HYDRAULIC POWER
EFFECTIVITY UPDATED (THROUGHOUT THE TEXT)
401-499,401-499,
401-499,
401-499,
401-499,
401-499,
401-499, 401-499,
ALL
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
401-499,
001-049, 051-099, 101-149,
151-199, 201-299, 301-399,
401-499,
001-049, 051-099, 101-149,
32-HIGHLIGHTS Page 27 of 28 REVISION NO. 30 Aug 01/05
CES CH/SE/SU C REASON FOR CHANGE EFFECTIVITY PAGES
32-60-00 EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 1
32-61-00 EFFECTIVITY UPDATED
1-3, MOD.35270P9030 INCORPORATED 23, 25-INDICATING/RECORDING SYSTEMS - EIS -26, 28-RE-INSTALL EIS1 IN PLACE OF EIS2 30, 32-(ANTI-MOD 34571+31495+30368+30232) 35, 39-EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 40, 43
32-62-00 EFFECTIVITY UPDATED 4, 14-MOD.27520P5580 INCORPORATED
16 COMMUNICATIONS-SATCOM SYSTEM-INSTALL COMPLETE PROVISIONS FOR ROCKWELL COLLINS AERO I SATCOM SYSTEM EFFECTIVITY UPDATED (THROUGHOUT THE TEXT) 151-199, 201-299, 301-399,
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 LANDING GEAR 起落架1(11)
