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时间:2011-03-30 15:13来源:蓝天飞行翻译 作者:航空
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Control Display Unit ................................................................................................. 34-18-21 Servicing (Relamping) Removal/Installation
Mode Annunciator Unit ............................................................................................ 34-18-31 Removal/Installation Subject Subject No.
5C8 
Contents 34 Page 2  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Feb 20/89 


ATTITUDE AND DIRECTION
COMPASS SYSTEM. ................................................................................................. *[3] 34-21-0

Description and Operation *[4] 34-21-02 AFCS Controller *[4] Compass Controller *[4] Compass Coupler *[4] Directional Gyros Flight Instrument Accessory Box *[3] Horizontal Situation Indicator (HSI) Instrument Amplifiers Rack Mountings *[3] Radio Magnetic Indicator (RMI) Remote Compass Transmitter (Flux Valve)
Trouble Shooting
Maintenance Practices (Compass Swinging)
Adjustment/Test

Remote Compass Transmitter................................................................................. 34-21-11 Removal/Installation
Directional Gyro ....................................................................................................... 34-21-21 Removal/Installation
ATTITUDE REFERENCE SYSTEM ........................................................................... *[3] 34-22-0

Description and Operation *[4] 34-22-01 Attitude Director Indicator (ADI) Flight Instrument Amplifier Rack *[3] Vertical Gyro
Trouble Shooting
Adjustment/Test

Vertical Gyro ............................................................................................................ 34-22-11 Removal/Installation
TURN AND BANK INDICATOR.................................................................................. 34-23-0 Description and Operation Maintenance Practices
MAGNETIC STANDBY COMPASS ............................................................................ 34-24-0 Description and Operation Maintenance Practices
Precautions
Demagnetization of the Nose Gear Strut Assembly
Demagnetization of Remote Compass Transmitter Area

Magnetic Standby Compass.................................................................................... 34-24-11 Maintenance Practices (Compass Swing) Removal/Installation Subject Subject No.
5C8 
Aug 01/95  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Contents 34 Page 3 


STANDBY ARTIFICIAL HORIZON SYSTEM ............................................................. *[9] 34-25-0

Description and Operation
Standby Artificial Horizon Indicator
Standby Attitude Phase Converter

Adjustment/Test
STANDBY ARTIFICIAL HORIZON SYSTEM ............................................................. *[10] 34-25-01 Description and Operation
FLIGHT DIRECTOR SYSTEM.................................................................................... *[1] 34-26-0

Description and Operation
Air Data Computer
Approach Progress Display
Attitude Director Indicator
Flight Director (Steering) Computer
Flight Director Control Panel (Mode Selector Panel)
Horizontal Situation Indicator

Trouble Shooting
Adjustment/Test

FLIGHT DIRECTOR SYSTEM.................................................................................... *[2] 34-26-01 Description and Operation
Attitude Director Indicator ........................................................................................ 34-26-11 Removal/Installation
Horizontal Situation Indicator................................................................................... 34-26-21 Removal/Installation
Flight Director (Steering) Computer......................................................................... *[1] 34-26-31 Removal/Installation
Approach Progress Display ..................................................................................... *[1] 34-26-41 Removal/Installation
Flight Director Control Panel.................................................................................... *[1] 34-26-51 Removal/Installation
Flight Instrument Accessory Unit ............................................................................. 34-26-61 Removal/Installation
NAVIGATION WARNING SYSTEM............................................................................ *[3] 34-29-0 Description and Operation *[4] 34-29-01 Adjustment/Test
Comparator Warning Unit ........................................................................................ 34-29-0 Removal Installation
Navigation Warning Annunciator ............................................................................. 34-29-21 Removal/Installation Subject Subject No.
 
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