• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-10-11 13:04来源:蓝天飞行翻译 作者:航空
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

A

757
MAINTENANCE MANUAL


757
MAINTENANCE MANUAL

 CHAPTER 29 - HYDRAULIC POWER
 TABLE OF CONTENTS
_________________
 Chapter Section Subject_______ Subject_______ Page
HYDRAULIC POWER 29-00-00
_______________
 Description and Operation 1 General 1 Auxiliary Hydraulic Systems 1 Ground Servicing System 4 Indicating Systems 4 Main Hydraulic Systems 1
 Inspection/Check 601
MAIN 29-10-00
____ MAIN (LEFT, RIGHT, AND CENTER) 29-11-00 HYDRAULIC SYSTEMS
 Description and Operation 1 General 1 Alternating Current Motor Pump 1
 (ACMP) ACMP Pressure/Case Drain 12
 Filter Module Center System Module 12 Left and Right System 12
 Modules Engine Driven Pump (EDP) 1 EDP Pressure/Case Drain Filter 9
 Module EDP Supply Shutoff Valve 12 Ground Power Connections 14 Heat Exchanger 14 Hydraulic Control Panel 14 Hydraulic Reservoir 6 Isolated ACMP Shutoff Valves 12 Reservoir Pressurization 8
 Module Return Filter Modules 8 Operation 14
 Functional Description 14 Functional Description 24
 Component Location 101 Component Index Component Location
Effectivity
ALL
ALL
ALL
ALL
 29-CONTENTS

 GUN Page 1 Mar 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL CHAPTER 29 - HYDRAULIC POWER TABLE OF CONTENTS
_________________
 Chapter
 Section
 Subject_______  Subject_______  Page____ 
Maintenance Practices  201 
Flush the Left or Right  219
 Hydraulic System
 Hydraulic System Fluid  221
 Replacement
 Pressurize the Left or Right  210
 Main Hydraulic System with an
 EDP
 Pressurize the Main Hydraulic  204
 Systems with a Hydraulic
 Service Cart
 Pressurize the Main Hydraulic  209
 Systems with an ACMP
 Pressurize the Reservoirs in  212
 the Main Hydraulic System
 with an External Air Source
 Remove the Hydraulic Power  217
 Remove the Pressure from the  214
 Main Hydraulic Systems and
 Reservoirs
 Adjustment/Test  501 
Operational Test - Engine  534
 Driven Pump Pressure Switch
 Operational Test - Hydraulic  511
 Pressure on the EICAS Display
 for the Engine-Driven Pump
 (EDP) in the Left (Right)
 Hydraulic System
 Operational Test - Main (Left,  501
 Right, and Center) Hydraulic
 Systems
 Operational Test - Reserve  509
 Brake System
 
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 液压 CHAPTER 29 - HYDRAULIC POWER 1