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时间:2011-04-21 08:02来源:蓝天飞行翻译 作者:航空
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LIMITER - LEFT HYDRAULIC SYSTEM PRESSURE SENSITIVE FLOW Removal/Installation LINKAGE - INBOARD TRAILING EDGE FLAP AFT FLAP Removal/Installation LINKAGE - OUTBOARD TRAILING EDGE
FLAP AFT FLAP Removal/Installation Inspection/Check
MODULE AND COMPONENTS -FLAP/SLAT DEPRESSURIZATION Maintenance Practices
Install the Flap/Slat Depressurization Module and Components
 Operational Test for the Flap/Slat Depressurization Module
 Operational Test for the Flap/Slat Depressurization Module with Primary Control
 Operational Test for the Primary Valve
 Remove the Flap/Slat Depressurization Module and Components Chapter SectionSubject_______ Page____ Effectivity
27-51-10
401 ALL27-51-08
401 ALL27-51-18
401 ALL
27-51-32401 ALL601 ALL
27-51-24
401 ALL27-51-13
401 ALL27-51-23
401 ALL601 ALL27-51-29
201 ALL205
216
229
231
201

 27-CONTENTS

 GUN Page 22 May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 Subject
_______
MODULE AND COMPONENTS - TRAILING EDGE FLAP POWER DRIVE UNIT CONTROL VALVE
 Maintenance Practices Control Valve Module Component Test Control Valve Module
Installation Control Valve Module Removal Flap Load Relief Solenoid
Valve Coil Installation Flap Load Relief Solenoid Valve Coil Removal Flap Load Relief Solenoid Valve Installation Flap Load Relief Solenoid Valve Removal TRACK - INBOARD TRAILING EDGE FLAP Removal/Installation TRACK - OUTBOARD TRAILING EDGE
FLAP Removal/Installation Inspection/Check
TRANSMISSION - OUTBOARD TRAILING EDGE FLAP Removal/Installation TRANSMISSIONS - INBOARD TRAILING EDGE FLAP Removal/Installation TRANSMITTER - FLAP CONTROL LEVER POSITION Removal/Installation TUBES - TRAILING EDGE FLAP TORQUE Maintenance Practices
Approved Repairs for the Torque Tubes of the TE Flap System
 Install the Torque Tubes for the TE Flap Remove the Torque Tubes for the TE Flap
 Chapter SectionSubject_______ Page____ Effectivity
27-51-28201 ALL225 ALL
211 ALL201223 ALL
220 ALL218 ALL216 ALL
27-51-03401 ALL27-51-15401 ALL601 ALL27-51-17401 ALL27-51-06401 ALL27-51-33401 ALL27-51-25201 ALL213
204201

 27-CONTENTS

 GUN Page 23 May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 
MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS
 TABLE OF CONTENTS_________________
 Chapter
 Section
 Subject Subject Page_______ _______ ____  Effectivity___________
 UNIT - FLAP/SLAT ELECTRONIC 27-51-01
 Maintenance Practices 201  ALL
 Install Flap/Slat Electronic 204
 Unit
 Remove Flap/Slat Electronic 201
 Unit
 Test the FSEU 205
 UNIT - TRAILING EDGE FLAP POWER 27-51-26
 DRIVE
 Removal/Installation 401  ALL
 TRAILING EDGE FLAP POSITION 27-58-00
 INDICATING SYSTEM
 Description and Operation 1  ALL
 General 1
 Component Details 1
 Engine Indicating and Crew 4
 Alerting System (EICAS)
 Flap/Slat Electronic Unit 2
 (FSEU)
 Flap/Slat Position Indicator 1
 Resolvers 6
 Synchros 6
 Trailing Edge Light 2
 Operation 6
 Asymmetry 7
 Flap Load Alleviation 8
 Takeoff Configuration 8
 Uncommanded Motion (UCM) 6
 Adjustment/Test 501  ALL
 Test of the Position 501
 Indicating System for the TE
 Flaps
 TRANSMITTER - FLAP POSITION 27-58-03
 Removal/Installation 401  ALL


 27-CONTENTS

 GUN Page 24 May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
_________________ Chapter
 Section
 Subject_______  Subject_______  Page____ 
TRANSMITTER - TRAILING EDGE FLAP  27-58-01
 SYSTEM AND LEADING EDGE SLAT
 SYSTEM POSITION
 Adjustment/Test  501 
Adjust the Position  524
 Transmitter without HILDA
 Adjust the Position  501
 Transmitters with the -40
 FSEU or HILDA
 Test of the Position  540
 Transmitter Installation
 SPOILER, DRAG DEVICES AND VARIABLE__________________________________ 27-60-00
 
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