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时间:2011-03-21 08:13来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 Operation 10 ALL Control and Indicating Circuits 10 ALL Electrical Emergency 31 ALL Configuration Electrical Smoke Configuration 61 ALL Electrical Configuration in case 73 001-049, 051-061 of Failure of Both Engines 101-105, 201-203 Electrical Configuration in case 74 062-099, 106-149 of Failure of Both Engines 204-299, Electrical Configuration in case 74 151-199, 301-399 of Failure of Both Engines 401-499,
 AC EMERGENCY GENERATION (CSM/G, GCU) 24-24-00
 ADJUSTMENT/TEST 501 ALL
 Operational Test of the Emergency 501 ALL
 Generation System
 Operational Test of the Emergency 506 ALL

 24-CONTENTS Page 8 Aug 01/05 R CES


 CHAPTER 24
__________
 ELECTRICAL POWER
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Generation System with either the Blue Electric Pump or a Ground Hydraulic Cart Operational Test of the Emergency 511 ALL Generator Control Unit (GCU) from Centralized Fault Display System (CFDS)
 CONTROL UNIT - CSM/G 24-24-34
 REMOVAL/INSTALLATION 401 ALL Removal of the CSM/G Control Unit 401 ALL (1XE) Installation of the CSM/G Control 404 ALL Unit (1XE)
 GENERATOR - CONSTANT SPEED MOTOR 24-24-51
 (CSM/G)

 REMOVAL/INSTALLATION 401 ALL Removal of the Constant Speed 401 ALL Motor/Generator (CSM/G) (8XE) Installation of the Constant Speed 405 ALL Motor/Generator (CSM/G) (8XE)
 CONTACTOR 24-24-55
 REMOVAL/INSTALLATION 401 ALL Removal of the Emergency Generator 401 ALL Line Contactor (EMER GLC) 2XE) Installation of the Emergency 405 ALL Generator Line Contactor (EMER GLC) (2XE) Removal of the AC ESS BUS 408 ALL Contactor (15XE) Installation of the AC ESS BUS 412 ALL Contactor (15XE)
 AC ESSENTIAL GENERATION SWITCHING 24-25-00
 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL Operation 1 ALL
 AC ESSENTIAL GENERATION SWITCHING 24-25-00
 ADJUSTMENT/TEST 501 ALL Operational Test of the AC 501 ALL Essential Generation Switching
 CONTACTOR 24-25-55
 REMOVAL/INSTALLATION 401 ALL
 Removal of the AC Essential Bus 401 ALL

 24-CONTENTS Page 9 Aug 01/05 R CES


 CHAPTER 24
__________
 ELECTRICAL POWER
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________ Switching Contactor (3XC) Installation of the AC Essential 405 ALL Bus Switching Contactor (3XC)
 GALLEY SUPPLY CONTROL 24-26-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL Component Location 1 ALL System Description 4 ALL Operation/Control and Indicating 9 ALL Galley Automatic Shedding 9 001-049, 051-060 101-102, 201-201 Overload detected by a GCU 9 001-049, 051-060 101-102, 201-201 Galley Automatic Shedding 13 061-099, 103-149 151-199, 202-299 301-399, 401-499 Overload detected by a GCU 13 061-099, 103-149 151-199, 202-299 301-399, 401-499
 GALLEY SUPPLY CONTROL 24-26-00
 ADJUSTMENT/TEST 501 ALL Operational Test of the Manual and 501 001-049, 051-060 Automatic Shedding of the Galleys 101-102, 201-201 Operational Test of the Manual and 504 061-099, 103-149 Automatic Galley and Bus Shedding 151-199, 202-299
 301-399, 401-499
 AC GENERATION MONITORING AND INDICATING 24-27-00 DESCRIPTION AND OPERATION 1 ALL General 1 ALL System Description 1 ALL Operation/Control and Indicating 1 ALL Operation 1 ALL Description 1 ALL
 AC GENERATION MONITORING AND 24-27-00
 INDICATING
 ADJUSTMENT/TEST 501 ALL
 Operational Test of the GEN FAULT 501 ALL
 Warning
 Operational Test of the Automatic 503 ALL
 Galley Shedding

 24-CONTENTS Page 10 Aug 01/05 R CES


 CHAPTER 24
__________
 ELECTRICAL POWER
 TABLE OF CONTENTS
_________________
 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY________ C ____ ___________
 STATIC INVERTER (GENERATION) 24-28-00
 DESCRIPTION AND OPERATION 1 ALL
 General 1 ALL
 Component Location 1 ALL
 System Description 1 ALL
 Operation/Control and Indicating 4 ALL
 Test 4 ALL

 STATIC INVERTER (GENERATION) 24-28-00
 ADJUSTMENT/TEST 501 ALL
 Operational Test of the Static 501 ALL
 Inverter (3XB) when the Aircraft
 Electrical Circuits are Energized
 from the External Power
 Operational Test of the Static 506 ALL
 Inverter (3XB) when the Aircraft
 Electrical Circuits are Energized
 from the APU

 STATIC INVERTER 24-28-51
 REMOVAL/INSTALLATION 401 ALL
 Removal of the Static Inverter 401 ALL
 (3XB)
 
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