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

 GUN Page 4 Sep 20/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ____ 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

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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