EffectivityALL
ALL
ALL
ALLALL
 27-CONTENTS
 GUN Page 15 Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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747-400 MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
 HINGE - STABILIZER 27-41-02 Maintenance Practices 201 ALL
 Adjustment 216 Stabilizer Hinge 216 Operational Test 221 Stabilizer Hinge 221 Removal/Installation 201 Stabilizer Hinge Pivot 201
 Pins Stabilizer Hinge 210 Inspection/Check 601 ALL
 Horizontal Stabilizer 603 Flutter Free Play Limit Inspection
 Horizontal Stabilizer Hinge 601 Wear Limits Inspection
 Horizontal Stabilizer Inner 603 and Outer Pivot Pin Corrosion Inspection
 MECHANISM - STABILIZER TRIM 27-41-06
 DRIVE Removal/Installation 401 ALL Adjustment/Test 501 ALL
 Operational Test 501 Inspection/Check 601 ALL
 Horizontal Stabilizer Upper 606 and Lower Gimbal Pin Limits for Corrosion
 Stabilizer Trim Drive 615 Mechanism Visual Inspection
 27-CONTENTS
 GUN Page 16 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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___________
 MODULE - STABILIZER TRIM CONTROL 27-41-04
 Maintenance Practices  201  ALL
 General  201
 Operational Test  206
 Stabilizer Trim Control  206
 Module
 Removal/Installation  207
 Pressure Switch  207
 Removal/Installation  201
 Stabilizer Trim Control  201
 Module
 Filter Screen  222
 Motor Operated Shutoff  215
 Valve
 Shutoff Valve Electric  219
 Motor
 Solenoid Valve Assembly  211
 MODULE - STABILIZER TRIM/RUDDER 27-41-01
 RATIO
 Removal/Installation  401  ALL
 MOTOR - STABILIZER TRIM 27-41-10
 HYDRAULIC
 Removal/Installation  401  ALL
 STABILIZER TRIM DRIVE MECHANISM 27-41-13
 LIP SEAL
 Removal/Installation  401  ALL
 SWITCH - MANUAL STABILIZER TRIM 27-41-11
 Removal/Installation  401  ALL
 SWITCH, LIMIT - STABILIZER TRIM 27-41-08
 Removal/Installation  401  ALL
 Fuel Range Limit Switch  409
 Stabilizer Trim Limit Switch  401
 Adjustment/Test  501  ALL
 SWITCHES - STABILIZER TRIM 27-41-07
 ELEVATOR CONTROL ACTUATED LIMIT
 Adjustment/Test  501  ALL
 Adjustment  501
 Operational Test  506

 27-CONTENTS
 GUN Page 17 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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___________
 STABILIZER TRIM INDICATING SYSTEM  27-48-00
 Description and Operation  1  ALL
 General  1
 Indicator - Stabilizer Trim  1
 Position
 Transmitter - Stabilizer  1
 Position
 Unit - Flap Control  1
 Operation  3
 Adjustment/Test  501  ALL
 Adjustment  504
 Operational Test  501
 INDICATOR - STABILIZER TRIM  27-48-02
 POSITION
 Removal/Installation  401  ALL
 SWITCH - NOSE GEAR PRESSURE  27-48-03
 Removal/Installation  401  ALL
 Adjustment/Test  501  ALL
 TRANSMITTER - HORIZONTAL  27-48-01
 STABILIZER POSITION
 Removal/Installation  401  ALL
 FLAPS_____ 27-50-00
 Component Location  101  ALL
 Component Index
 Component Location

 27-CONTENTS
 GUN Page 18 Feb 18/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 
747-400 
MAINTENANCE MANUAL
　
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