ASSEMBLY - AILERON CONTROL DRUM Maintenance Practices Aileron Control Drums and Bus Force Limiter - Test Install Aileron Control Drum and Components Remove Aileron Control Drum Components MECHANISM - AILERON QUADRANT AND
OVERRIDE Removal/Installation Inspection/Check
MECHANISM - LATERAL CONTROL FEEL, CENTERING, AND TRIM Maintenance Practices Feel, Centering, and Trim Mechanism - Adjustment/Test
Feel, Centering, and Trim Mechanism and Its Components - Removal
Feel, Centering, and Trim Mechanism and Its Components - Installation
MECHANISM - LATERAL CONTROL OVERRIDE Removal/Installation
WHEEL - LATERAL CONTROL
Removal/Installation
Inspection/Check
Chapter SectionSubject_______ Page____
27-11-20
201 205
201
215
27-11-2127-11-03 213601 401 601 201 211
206
201
27-11-17
27-11-14 401 601
201 212
201
206
27-11-16
27-11-02 401 401 601
Effectivity
ALL
ALL
ALLALLALL
ALLALL
ALL
ALL
ALL
ALL
27-CONTENTS
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757 MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject ____ Effectivity_______ Page ___________
AILERON POSITION INDICATING SYSTEM 27-18-00
Description and Operation 1 ALL General 1 Component Details 1
Aileron Position Transmitter 1 Flight Control Surface 1 Position Indicator
Operation 1
Control 1
Functional Description 1
Component Location 101 ALL Component Index Component Location Figure Not Used 104
Adjustment/Test 501 ALL Adjustment - Aileron Position 505 Indicating System Operational Test - Aileron 501 Position Indicating System TRANSMITTER - AILERON POSITION 27-18-01 Removal/Installation 401 ALL
RUDDER & TAB 27-20-00
____________
27-CONTENTS
GUN Page 5 Mar 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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____
RUDDER AND RUDDER TRIM CONTROL 27-21-00
SYSTEM
Description and Operation 1
General 1
Component Details 2
Autopilot Rollout Guidance 7
Servos
AFT Quadrant, Feel, 4
Centering and Trim
Mechanism
Forward Quadrant and 2
Jackshaft Assembly
Linear Variable Differential 9
Transformer (LVDT)
Pedal Adjustment Crank 2
Power Control Actuators 11
(PCAs)
Primary Control Linkage 9
PCA Linkages 16
PCA Reaction Link 16
Rudder Control Cables 4
Rudder Pedals 2
Rudder Ratio Changer 9
Actuator (RRCA)
Rudder Ratio Changer 7
Mechanism
Rudder Structure 16
Rudder Thermal Compensating 7
Linkage
Rudder Trim Actuator 4
Rudder Trim Control Switch 18
Indicator
Secondary Control Linkage 9
Yaw Damper Servos 11
Yaw Damper Summing Lever 11
Operation 19
Built in Test Equipment 37
(BITE)
Control 38
Functional Description 19
Effectivity
ALL
27-CONTENTS
GUN Page 6 Sep 20/98
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____
Component Location 101
Component Index
Component Location
Adjustment/Test 501
Adjustment - Rudder and Rudder 525
Trim Control System
Operational Test - Rudder and 501
Rudder Trim Control System
System Test - Rudder and 554
Rudder Trim Control
ACTUATOR - RUDDER RATIO CHANGER 27-21-13
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