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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
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 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Position Operation 4 Effectivity ALL ALL ALL ALL 27-CONTENTS GUN Page 1 Feb 18/02 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 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 GUN Page 2 Feb 18/02 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. 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 GUN Page 3 Feb 18/02 BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details. A 747-400 MAINTENANCE MANUAL CHAPTER 27 - FLIGHT CONTROLS www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：747-400 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1
