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时间:2011-04-21 08:02来源:蓝天飞行翻译 作者:航空
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A

757 MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS
 TABLE OF CONTENTS
_________________
 Chapter
 Section
 Subject_______  Subject_______ 
VALVES - RUDDER AND ELEVATOR  27-23-01
 HYDRAULIC SHUTOFF
 Maintenance Practices 
Rudder and Elevator 
Hydraulic Shutoff Valves -
Installation
 Rudder and Elevator 
Hydraulic Shutoff Valves -
Removal
 RUDDER POSITION INDICATING SYSTEM  27-28-00
 Description and Operation 
General 
Component Details 
EICAS Position Indicator 
Position Transmitter 
Operation 
Component Location 
Component Index
 Component Location
 Adjustment/Test 
Rudder Position Indicating 
System - Adjustment
 Rudder Position Indicating 
System - Operational Test
 TRANSMITTER - RUDDER POSITION  27-28-01
 Maintenance Practices 
Rudder Position Transmitter 
- Installation
 Rudder Position Transmitter 
- Removal
 ELEVATOR & TAB______________ 27-30-00

Page____  Effectivity___________
201  ALL
203
201
1  ALL
1
1
1
1
1
101  ALL
501  ALL
504
501
201  ALL
204
201


 27-CONTENTS

 GUN Page 10 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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____ 
ELEVATOR CONTROL SYSTEM  27-31-00
 Description and Operation  1 
General  1
 Component Details  6
 Asymmetry Limiter Actuator  14
 Control Column  6
 Elevator  11
 Elevator Control Aft  6
 Quadrants
 Elevator Control AFT  6
 Mechanism Torque Box
 Elevator Feel Computer  11
 Elevator Feel Unit and  11
 Actuator
 Elevator Power Control  11
 Actuator (PCA)
 Elevator Pressure Reducer  14
 and Bypass Valves
 Forward Quandrant/Tension  6
 Regulators
 Neutral Shift and Override  14
 Mechanism
 Operation  14
 Control  20
 Fault Indication  20
 Functional Description  14
 Component Location  101 
Component Index
 Component Location
 Adjustment/Test  501 
Elevator Column and Quadrant  582F
 Override Test
 Elevator Control System - 527
 Adjustment
 Elevator Control System - 501
 Operational Test
 Elevator Control System - 563
 System Test
 Elevator Pressure Bypass Valve  582J
 Test
 ú Single Hydraulic Source - Test  582R

EffectivityALL
ALLALL

 27-CONTENTS

 GUN.1 Page 11 Sep 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 ___________
 ACTUATOR - ASYMMETRY LIMITER 27-31-03 Removal/Installation 401 ALL ACTUATOR - ELEVATOR FEEL 27-31-18 Removal/Installation 401 ALL ACTUATOR/REACTION LINK -27-31-05
 ELEVATOR POWER CONTROL Removal/Installation 401 ALL Inspection/Check 601 ALL
 ASSEMBLY - CONTROL COLUMN 27-31-23 OVERRIDE Adjustment/Test 501 ALL Adjust the Override Assembly 501 BEARING - CONTROL COLUMN TORQUE 27-31-11 TUBE Removal/Installation 401 ALL BOX - ELEVATOR CONTROL AFT 27-31-16 MECHANISM TORQUE Removal/Installation 401 ALL
 COLUMN - CONTROL 27-31-10 Removal/Installation 401 ALL Inspection/Check 601 ALL
 COMPUTER - ELEVATOR FEEL 27-31-19 Removal/Installation 401 ALL
 ELEVATOR 27-31-01 Removal/Installation 401 ALL Inspection/Check 601 ALL
 LINKAGE - ELEVATOR POWER CONTROL 27-31-06 ACTUATOR (PCA) INPUT Removal/Installation 401 ALL MECHANISM - ELEVATOR NEUTRAL 27-31-21
 SHIFT AND OVERRIDE Removal/Installation 401 ALL Inspection/Check 601 ALL
 PLATE - ELEVATOR INDEX 27-31-02 Removal/Installation 401 ALL QUADRANTS - ELEVATOR AFT 27-31-15 Removal/Installation 401 ALL REGULATOR - ELEVATOR FORWARD 27-31-12 QUADRANT/TENSION Removal/Installation 401 ALL
 
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