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 Angle Gearboxes 13
 Flap/Slat Depressurization 10
 Module
 Flap/Slat Electronics Units 19
 Rotary Actuators and Pinion 13
 Gears
 Slat Bypass Valve 10
 Slat Cables 5
 Slat Drive Torque Tubes 12
 Slat Loss Detection 13
 Slat Position Transmitters 13
 Slat PDU 5
 Slats 13
 Operation 29
 Control 38
 Functional Description 29
 Component Location 101  ALL
 Component Index
 Component Location
 Maintenance Practices 201  ALL
 Deactivation of the LE Slats 201
 Operation of the LE Slat 210
 System
 Adjustment/Test 501  ALL
 Adjustment - LE Slat System 515
 Operational Test - LE Slat 501
 System
 System Test - LE Slat System 533
 Test of the Auto Slat 559
 Extension and Retraction
 Test of the LE Slat Loss 561
 Detection Switches
 ACTUATOR - LEADING EDGE SLAT 27-81-18
 DRIVE ROTARY
 Removal/Installation 401  ALL

 27-CONTENTS

 GUN Page 28 Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 757 MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS
 TABLE OF CONTENTS_________________
 Subject_______  Chapter SectionSubject_______  Page____  Effectivity___________
 Inspection/Check 601 [*] -32 (MOD A OR B), -37 (MOD A OR B), OR -40 FSEU [*]

 COMPONENTS - LEADING EDGE SLAT  27-81-08
 POWER DRIVE UNIT
 Maintenance Practices  201  ALL
 Install the Components for the LE Slat PDU 207
 Remove the Components for the LE Slat PDU 201
 GEARBOX - LEADING EDGE SLAT  27-81-15
 DRIVE ANGLE
 Removal/Installation MODULE AND COMPONENTS - LEADING  27-81-06 401  ALL
 EDGE SLAT POWER DRIVE UNIT
 CONTROL VALVE
 Maintenance Practices  201  ALL
 Install the Control Valve  209
 Module and the Autoslat
 Solenoid Valve
 Remove the Control Valve  201
 Module and the Autoslat
 Solenoid Valve
 SLAT - INBOARD LEADING EDGE  27-81-01
 Removal/Installation Inspection/Check SLAT - OUTBOARD LEADING EDGE  27-81-02 401 601  ALLALL
 ú  Removal/Installation Inspection/Check SWITCH - INBOARD LEADING EDGE  27-81-41 401 601  ALLALL
 ú  SLAT LOSS SENSING
 ú  Removal/Installation Adjustment/Test Adjust the Loss Sensing Switch for the Inboard LE 401 501 501 ALLALL
 Slat
 SWITCH - OUTBOARD LEADING EDGE  27-81-42
 SLAT LOSS SENSING
 Adjustment/Test Adjust the Loss Sensing Switch for the Outboard LE 501 501 ALL
 Slat
 Removal/Installation  401  ALL

 27-CONTENTS

 GUN.1 Page 29 Sep 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 Subject
_______
TRACK - INBOARD LEADING EDGE
SLAT AUXILIARY Removal/Installation Inspection/Check
TRACK - INBOARD LEADING EDGE
SLAT MAIN Removal/Installation Inspection/Check
TRACK - OUTBOARD LEADING EDGE
SLAT AUXILIARY Removal/Installation Inspection/Check
TRACK - OUTBOARD LEADING EDGE
SLAT MAIN Removal/Installation Inspection/Check
TUBE - LEADING EDGE SLAT DRIVE
TORQUE Removal/Installation Approved Repairs
UNIT - LEADING EDGE SLAT POWER DRIVE Removal/Installation VALVE - LEADING EDGE SLAT BYPASS Removal/Installation LEADING EDGE SLAT POSITION INDICATING SYSTEM
 Description and Operation General General Description
Flap/Slat Position Indication on Primary Power
 Flap/Slat Positoin Indication on Alternate Power
 Takeoff Warning
Component Location
Component Index
 Component Location

 Chapter SectionSubject
27-81-11
27-81-10
27-81-13
27-81-12
27-81-20
27-81-07
27-81-0927-88-00
Page____  Effectivity___________
401  ALL
601  ALL
401  ALL
601  ALL
401  ALL
601  ALL
401  ALL
601  ALL
401  ALL
801  ALL
401  ALL
401  ALL
1  ALL
1
　
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本文鏈接地址：757 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 1(10)