Effectivity
ALL
ALLALL
ALLALL
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757 MAINTENANCE MANUAL CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
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_______
Adjustment/Test
Adjustment -Spoiler/Speedbrake Control System
Operational Test -Spoiler/Speedbrake Control System
System Test -Spoiler/Speedbrake Control System
ACTUATOR - SPOILER POWER CONTROL (PCA) Maintenance Practices Spoiler PCA and Its Components - Installation Spoiler PCA and Its Components - Removal SPOILERS Removal/Installation UNIT - SPOILER RVDT Removal/Installation AUTO-SPEEDBRAKE CONTROL SYSTEM
Description and Operation General 1 Component Details 1
Auto-Speedbrake Actuator and 1
No-Back Clutch Auto-Speedbrake Switches 1 Forward Thrust Lever 3
Position Switches Reverse Thrust Mechanism 1
Operation 3 Control 8 Functional Description 3
Component Location 101 Component Index Component Location Chapter SectionSubject_______ Page
501 512
501
547
27-61-02201 208
201
27-61-01401 27-61-04401 27-62-001
27-CONTENTS
GUN Page 26 May 28/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
_________________ Chapter
Section
Subject_______ Subject_______ Page____
Adjustment/Test 501
Adjustment - Auto-Speedbrake 510
System
Operational Test - 501
Auto-Speedbrake System
Speedbrake Lever Force Test 524
System Test - Auto-Speedbrake 525
System
LEVER - SPEEDBRAKE 27-62-01
Removal/Installation 401
MECHANISM - SPEEDBRAKE 27-62-02
Maintenance Practices 201
Arming Switch for the 221
Auto-Speedbrake Actuator
(S371) - Installation
Auto-Speedbrake Actuator 220
Arming Switch (s371) -
Removal
Auto-Speedbrake Mechanism 201
and its Components -
Removal
Auto-Speedbrake Mechansim 212
and its Components -
Installation
SWITCH - FORWARD THRUST LEVER 27-62-07
POSITION
Adjustment/Test 501
Position Switch for the 501
Forward Thrust Levers -
Operational Test
SWITCH - REVERSE THRUST LEVER 27-62-08
POSITION
Maintenance Practices 201
Position Switch for the 202
Reverse Thrust Levers -
Installation
Position Switch for the 201
Reverse Thrust Levers -
Removal
LIFT AUGMENTING_______________ 27-80-00
EffectivityALL
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27-CONTENTS
GUN Page 27 Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS_________________
Chapter
Section
Subject Subject Page_______ _______ ____ Effectivity___________
LEADING EDGE SLAT SYSTEM 27-81-00
Description and Operation 1 ALL
General 1
L.E. Slat System Purpose 1
Component Details 5
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