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时间:2011-03-30 06:50来源:蓝天飞行翻译 作者:航空
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Stabilizer speed does not increase with flaps down Stabilizer light does not illuminate with airplane out of trim  Stabilizer trim servo Pitch channel  Test autopilot stabilizer trim servo (Refer to 22-11-81, Autopilot Stabilizer Trim Servo). Press autopilot stabilizer trim warning light. If light illuminates, pitch channel is faulty  Replace autopilot stabilizer trim servo (Refer to 22-11-81, Autopilot Stabilizer Trim Servo). Replace pitch channel 

TROUBLE  PROBABLE CAUSE  ISOLATION PROCEDURE  REMEDY 
Roll channel does not  Roll channel  Check meter on front of roll  Replace roll channel 
engage (air data  channel. If meter does not 
computer vertical  read in red, roll channel is 
gyro, directional gyro  faulty 
and power ok)  Aileron force limiter Autopilot accessory box or control panel Roll CWS force transducer  Conduct self-test of roll channel. If channel falls self-test, roll channel is faulty Disconnect D443 on force limiter; apply P8-v dc to pin 1 and ground pin 2 of force limiter. Check for continuity between pins 3 and 4. If no continuity, force limiter is faulty Replace autopilot accessory box. Attempt to engage roll channel. If roll channel engages, accessory box was faulty. If roll channel does not engage, autopilot control panel is probably faulty Check roll control wheel steering transducer null voltage (Refer to 22-11-111, Roll Control Wheel Steering Force Transducer.) If voltage unsatisfactory, transducer is faulty  Replace aileron force limiter (Refer to  22-11-131, Aileron Force Limiter). Replace autopilot accessory box. Replace autopilot control panel Adjust or replace roll control wheel steering force transducer (Refer to 22-11-111, Roll Control Wheel Steering Force Transducer). 

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22-11-0  Feb 15/69 
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TROUBLE  PROBABLE CAUSE  ISOLATION PROCEDURE  REMEDY 
Ailerons kick sharply on engagement NOTE: Ailerons may kick when airplane on ground due to wings leveling circuit. Maximum allowable control wheel rotation is 6 degrees. Roll channel disengages intermittently (interlocks known good) Roll channel inoperative or intermittent  Roll channel Roll channel or control panel. Roll channel Autopilot accessory box Control panel  Conduct self-test of roll channel. If roll channel fails self-test, roll channel is faulty. Replace roll channel. Engage roll channel. If fault persists, control panel is probably faulty. Engage roll channel and move control wheel. If ailerons do not respond, see Hydraulic Power Pack Component, Trouble Shooting Chart. If system does not operate, roll channel is probably faulty. If roll channel has intermittent operation, replace autopilot accessory box If intermittent fault persists, autopilot control panel is faulty  Replace roll channel. Replace roll channel. Replace control panel. Replace roll channel. Replace autopilot accessory box Replace control panel 

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Aug 01/74  22-11-0 
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TROUBLE  PROBABLY CAUSE  ISOLATION PROCEDURE  REMEDY 
Roll axis stabilization is poor (vertical gyro known good) Roll channel does not respond to control wheel steering inputs Roll control wheel steering oversensitive or erratic  Roll channel Roll channel or control wheel steering transducer Control wheel detent breakout forces out of tolerance (roll force transducer misrigged)  Conduct self-test of roll channel. If roll channel fails self-test, roll channel is faulty Conduct roll channel self-test. If roll channel fails self-test 3 or more, roll channel is faulty. If roll channel ok, roll control wheel transducer is faulty With autopilot disengaged and hydraulic pressure off apply 90 pound-inches of torque on control wheel while monitoring at roll channel TP-18. Check voltage is between 4.0 and 6.0 VAC  Replace roll channel  Replace roll channel. Adjust or replace roll CWS transducer (Ref 22-11-111, Roll Control Wheel Steering Force Transducer) Voltage erratic. Replace roll channel  

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22-11-0  Feb 15/77 
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BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


T51755
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Feb 15/77  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  22-11-0 Page 120A 


TROUBLE  PROBABLE CAUSE  ISOLATION PROCEDURE  REMEDY 
Force limiter forces or bank limits are not correct for cam-out Airplane rolls wings level when in attitude hold and bank angle exceeds 5 degrees Airplane does not return to wings level when bank angle less than 5 degrees and in heading hold mode  Force limiter Roll channel Roll channel  Conduct aileron force limiter test (Refer to 22-11-131, Aileron Force Limiter.) If forces and limits are not correct, force limiter is faulty Conduct self-test of roll channel. If roll channel fails self-test 2 or more, roll channel is faulty Conduct self-test of roll channel. If roll channel fails self-test 2 or more, roll channel is faulty  Replace aileron force limiter (Refer to 22-11-131, Aileron Force Limiter) Replace roll channel Replace roll channel. 
 
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