27-CONTENTS
GUN Page 16 Jan 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ___________
MODULE - STABILIZER TRIM CONTROL 27-41-05
Maintenance Practices 201 ALL
Install the Stabilizer Trim 207
Control Modules (STCMs) and
the Solenoid Valves
Remove the Stabilizer Trim 201
Control Modules (STCMs) and
the Solenoid Valves
MOTOR - STABILIZER TRIM DRIVE 27-41-11
HYDRAULIC
Removal/Installation 401 ALL
SWITCH - ALTERNATE STABILIZER 27-41-03
TRIM
Removal/Installation 401 [*]
[*] AIRPLANES WITH ALTERNATE STAB TRIM SWITCHES ON THE CONTROL STAND
SWITCH - STABILIZER STANDBY TRIM 27-41-15
Removal/Installation 401 [*]
[*] AIRPLANES WITH STAB TRIM LEVERS ON THE CONTROL STAND
SWITCH - STABILIZER TRIM CONTROL 27-41-07 MODULE BRAKE PRESSURE Removal/Installation 401 ALL SWITCH - STABILIZER TRIM CONTROL 27-41-01 WHEEL Removal/Installation 401 ALL TABS - HORIZONTAL STABILIZER 27-41-17 ALIGNMENT Removal/Installation 401 ALL
27-CONTENTS
GUN Page 17 May 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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____
STABILIZER TRIM POSITION 27-48-00
INDICATING SYSTEM
Description and Operation 1
General 1
Component Details 1
Stabilizer Position 1
Indicators
Stabilizer Position Modules 6
(SPM's)
Stabilizer Trim Limit Switch 1
and Transmitter Modules
(LSTM)
Operation 6
Control 6
Functional Description 6
Component Location 101
Component Index
Component Location
Adjustment/Test 501
Stabilizer Takeoff Warning 510
System - Operational Test
Stabilizer Trim Position 513
Indicating System -
Adjustment
Stabilizer Trim Position 501
Indicating System - Operation
Test
Stabilizer Trim Position 521
Indicating System - System
Test
INDICATOR - STABILIZER TRIM 27-48-06
POSITION
Removal/Installation 401
MODULE - STABILIZER POSITION 27-48-03
Removal/Installation 401
MODULE - STABILIZER TRIM LIMIT 27-48-01
SWITCH AND POSITION TRANSMITTER
Removal/Installation 401
FLAPS_____ 27-50-00
Effectivity
ALL
ALLALL
ALLALL
ALL
27-CONTENTS
GUN Page 18 May 28/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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____
TRAILING EDGE FLAP SYSTEM 27-51-00
Description and Operation 1
General 1
Component Details 15
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