24-CONTENTS
GUN Page 3 Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
CHAPTER 24 - ELECTRICAL POWER
TABLE OF CONTENTS_________________
Chapter
Section
Subject_______ Subject_______ Page____
FAULT SENSING 24-23-00
Description and Operation 1
General 1
Component Details 1
Current Transformer 1
Assemblies
Operation 4
BITE 13
Functional Description 4
Component Location 101
Component Index
Component Location
ASSEMBLY - CURRENT TRANSFORMER 24-23-01
Removal/Installation 401
HYDRAULIC MOTOR GENERATOR SYSTEM 24-25-00
Description and Operation 1
General 1
Component Details 1
Generator Control Unit 7
Hydraulic Accumulator 8
Hydraulic Flow Limiters 8
Hydraulic Generator Power 8
Control Panel P71
Hydraulic Motor Generator 1
Hydraulic Motor Generator 10 7
KVA
Hydraulic Shutoff Valve 8
Test Switch 9
Transformer Rectifier Unit 8
Operation 9
Functional Description 9
[*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
Component Location 101 Component Index Component Location
[*] AIRPLANES WITH 5 KVA HYDRAULIC MOTOR GENERATOREffectivityALL
ALL
ALL[*]
CONFIG 1 [*]
24-CONTENTS
GUN Page 4 May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL CHAPTER 24 - ELECTRICAL POWER TABLE OF CONTENTS
_________________
Chapter
Section
Subject_______ Subject_______ Page____
Component Location 101
Component Index
Component Location
[*] AIRPLANES WITH 10 KVA HYDRAULIC MOTOR GENERATOR;
Adjustment/Test 501 Operational Test 501 System Test 508
[*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
ACCUMULATOR - HYDRAULIC MOTOR 24-25-04 GENERATOR Removal/Installation 401 [*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
GENERATOR - HYDRAULIC MOTOR 24-25-01 Removal/Installation 401 [*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
LIMITER - HYDRAULIC FLOW 24-25-06 Maintenance Practices 201 Installation of the Flow 203
Limiter Removal of the Flow Limiter 201 The Test of the Hydraulic 204
Flow Limiter [*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
UNIT - HMG TRANSFORMER RECTIFIER 24-25-05 Removal/Installation 401 [*] AIRPLANES WITH 10 KVA HYDRAULIC MOTOR GENERATOR
UNIT - HYDRAULIC MOTOR GENERATOR 24-25-02 CONTROL Removal/Installation 401 [*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
VALVE - HYDRAULIC MOTOR 24-25-03 GENERATOR SHUTOFF Removal/Installation 401 [*] AIRPLANES WITH HYDRAULIC MOTOR GENERATOR
EffectivityCONFIG 2 [*]
[*]
[*]
[*]
[*]
[*]
[*]
[*]
24-CONTENTS
GUN Page 5 Jan 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
CHAPTER 24 - ELECTRICAL POWER
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject ____ Effectivity_______ Page ___________
AC GENERATION ANNUNCIATION 24-27-00
Description and Operation 1 ALL General 1 Component Details 1
Electrical System Control 1
Panel
Generator Field and 1
Hydraulic Control Panel
Operation 1
Functional Description 1
AC METERS 24-28-00
Description and Operation 1 ALL General 1 Operation 1
Functional Description 1
DC GENERATION 24-30-00
_____________ Description and Operation 1 ALL General 1 Battery/Battery Charger System 1 Standby Power System 1 Adjustment/Test 501 ALL Operational Test - Battery 506 Charger and Current Monitor Operational Test - DC Generation 501 System Operational Test - DC Tie 510 Control Unit and DC Tie Relay
24-CONTENTS 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：757 AMM 飞机维护手册 电源 ELECTRICAL POWER 1(2)
