A 747-400 MAINTENANCE MANUAL
R = REVISED, A = ADDED OR D = DELETED CHAPTER 27 F = FOLDOUT PAGE EFFECTIVE PAGES E1 PAGE 20 FEB 18/02 CONTINUED
D633U101-E1
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
R = REVISED, A = ADDED OR D = DELETED CHAPTER 27 F = FOLDOUT PAGE EFFECTIVE PAGES E1 PAGE 21 FEB 18/02 LAST PAGE
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747-400 MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
Chapter Section
Subject_______ Subject_______ Page
FLIGHT CONTROLS 27-00-00
_______________ Description and Operation 1 General 1 Lateral Control and Speed Brake 7 Systems Lift Devices 17 Pitch Control System 16 Rudder Control System 16 FLIGHT CONTROL CABLES 27-00-01 Description and Operation 1 Cables - Flight Control 1 Locations - Flight Control 18 Safety Lanyard Receptacle Rivets - Shear 18 Seals - Flight Control Cable 18 Air Pressure SEAL, PRESSURE - RAISED CONTROL 27-00-02 CABLE AIR Removal/Installation 401 CONTROL WHEEL, RUDDER PEDAL, 27-08-00 CONTROL COLUMN, AND SPEED BRAKE LEVER POSITION INDICATION Description and Operation 1 General 1 Digitizer - Column/Rudder 4 Pedal Position Transmitter - Control Column 1 Position Transmitter - Control Wheel 1 Position Transmitter - Rudder Pedal 1 Position Transmitter - Speed Brake 4 Lever Position Operation 4
Effectivity
ALL
ALL
ALL
ALL
27-CONTENTS
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747-400 MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject
DIGITIZER - POSITION, 27-08-07 COLUMN/RUDDER PEDAL Removal/Installation TRANSMITTER - CONTROL COLUMN 27-08-03 POSITION Removal/Installation TRANSMITTER - RUDDER PEDAL 27-08-02 POSITION Removal/Installation TRANSMITTER ASSEMBLY - CONTROL 27-08-01 WHEEL POSITION Removal/Installation TRANSMITTER ASSEMBLY - SPEED 27-08-06 BRAKE LEVER POSITION Removal/Installation FLIGHT CONTROLS ELECTRONICS 27-09-00
Description and Operation
General
Module - Power Supply
Module - Stabilizer
Trim/Rudder Ratio
Module - Yaw Damper
Unit - Flap Control
Operation
Maintenance Practices
AILERONS 27-10-00
________
Component Location
Component Index
Component Location
Page____ Effectivity___________
401 ALL
401 ALL
401 ALL
401 ALL
401 ALL
1 ALL
1
4
4
4
1
4
201 ALL
101 ALL
27-CONTENTS
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A
747-400
MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
TABLE OF CONTENTS_________________
Chapter
Section
Subject Subject Page_______ _______ ____ Effectivity___________
AILERON AND AILERON TRIM CONTROL 27-11-00
SYSTEM
Description and Operation 1 ALL
General 1
Actuator, Electric Lockout -14
Outboard Aileron
Ailerons 2
Limiter, Load - Aileron 2
Control
Mechanism, Lockout - Outboard 13
Aileron
Mechanism, Trim and Feel -10
Aileron
Packages, Control - Central 11
Lateral
Packages, Power Control -13
Aileron
Programmers - Aileron 12
Adjustment/Test 501 ALL
Adjustment 516
Operational Test 507
System Test 528
ACTUATOR - ELECTRIC LOCKOUT 27-11-16
Removal/Installation 401 ALL
ACTUATOR, AILERON TRIM, AND 27-11-06
TRIM-AND-FEEL MECHANISM
Maintenance Practices 201 ALL
Adjustment/Test 215
Mechanism, Trim and Feel -215
Aileron
Inspection/Check 217
Removal/Installation 201
Aileron Trim Actuator 201
Aileron Trim-and-Feel 210
Mechanism
AILERON - INBOARD 27-11-01
Removal/Installation 401 ALL
Inspection/Check 601 ALL
27-CONTENTS
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747-400 MAINTENANCE MANUAL
CHAPTER 27 - FLIGHT CONTROLS
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