737-300 400 500 AMM 飞机维护手册 飞行操纵 FLIGHT CONTROLS 1(3)

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 REDUCER - RUDDER PRESSURE 27-21-96 Maintenance Practices 201 [*]
 [*] AIRPLANES WITH A RUDDER PRESSURE REDUCER
 Removal/Installation 401 [*] [*] AIRPLANES WITH A RUDDER PRESSURE REDUCER
 RUDDER 27-21-11 Removal/Installation 401 [*]
 [*] AIRPLANES WITH GRAPHITE/COMPOSITE RUDDER
 RUDDER 27-21-12 Removal/Installation 401 [*]
 [*] AIRPLANES WITH A GRAPHITE OR ALUMINUM RUDDER
 RUDDER 27-21-11 Inspection/Check 601 ALL
 TORQUE TUBE - RUDDER CONTROL 27-21-71 Removal/Installation 401 ALL Adjustment/Test 501 ALL Inspection/Check 601 ALL
 UNIT - RUDDER FEEL AND CENTERING 27-21-82 Removal/Installation 401 ALL
 UNIT - RUDDER POWER CONTROL 27-21-91 Removal/Installation 401 ALL Adjustment/Test 501 ALL Inspection/Check 601 ALL

 27-CONTENTS

 BEJ Page 6 Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
_________________ Chapter
 Section
 Subject_______  Subject_______  Page____ 
VALVE - STANDBY RUDDER ACTUATOR  27-21-94
 SHUTOFF
 Maintenance Practices  201 
Motor  204
 Valve and Motor  201
 ELEVATOR________ 27-30-00
 ELEVATOR AND TAB CONTROL SYSTEM  27-31-00
 Description and Operation  1 
General  1
 Columns - Control  5
 Computer - Elevator Feel  7
 Elevator  3
 Mechanism - Elevator Tab  12
 Control
 Panels and Seals - Elevator  4
 Balance
 Quadrants - Elevator Aft  7
 Control
 Quadrants - Elevator Forward  5
 Control
 Tabs - Elevator  3
 Unit - Elevator Feel and  9
 Centering
 Unit - Elevator Power Control  10
 Operation  13
 Trouble Shooting  101 
Maintenance Practices  201 
Null Procedure - Mach Trim  205
 Actuator
 Pressurize the Elevator  203
 Hydraulic Systems A and B
 Put the Elevator Hydraulic  202
 Systems A and B Back to the
 Condition Before the Pressure
 Removal
 Put the Elevator Hydraulic  204
 Systems A and B Back to the
 Condition Before the
 Pressurization
 Remove the Pressure from the  201
 Elevator Hydraulic Systems A
 and B

Effectivity
ALL
ALL
ALLALL

 27-CONTENTS

 ú ú BEJ.101 Page 7 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL CHAPTER 27 - FLIGHT CONTROLS TABLE OF CONTENTS
_________________
 Chapter
 Section
 Subject_______  Subject_______  Page____ 
Adjustment/Test  501 
Adjustment  505
 Flight Test - Elevator Power  573
 Off
 Operational Test  501
 Operational Test - 504
 Differential Pressure Switch
 Operational Test - Elevator  503
 Manual Control System
 System Test - Elevator and Tab  547
 Control System
 System Test - Elevator Limit  548
 Travel
 System Test - Elevator Output  550
 Torque Tube Bus Linkage
 System Test - Elevator Surface  547
 Friction and Balance
 System Test - Elevator Tab  551
 Linkage
 System Test - Feel Force  564
 System and Autopilot
 Authority
 System Test - Mach Trim  561
 Actuator
 System Test - Manual Mode  552
 Operation
 System Test - Neutral Shift  560
 Operation
 System Test - Power Mode  553
 Operation
 System Test - Sensors Null  570
 (with the DFCS Computer BITE)
 ACTUATOR - FEEL  27-31-67
 Removal/Installation  401 
BEARING - CONTROL COLUMN SUPPORT  27-31-54
 Removal/Installation  401 
COLUMN - CONTROL  27-31-51
 Removal/Installation  401 
COMPUTER - ELEVATOR FEEL  27-31-37
 Removal/Installation  401 
Inspection/Check  601 
ELEVATOR  27-31-11
 Removal/Installation  401 
　
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