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时间:2011-03-30 10:28来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

(4)  
Remove floor panels and/or cargo ceiling liners to inspect right cable run. Spin all pulleys, they should spin freely.

(5)  
Reconnect cable and inspect cable run. Check for hangups, deflecting fairleads or grommets and bent pulley brackets.


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Oct 20/89  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 102A 


3. Aileron and Aileron Trim Trouble Shooting Chart

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27-11-0 Page 102B  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Oct 20/89 


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May 15/81  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 103 


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27-11-0 Page 104  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Aug 01/94 


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Sep 20/81  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 105 


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27-11-0 Page 106  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Aug 01/94 


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Aug 01/94  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 107 


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27-11-0 Page 108  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Aug 01/94 


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Aug 01/94  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 109 


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27-11-0 Page 110  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 15/81 


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Aug 01/94  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 111 


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27-11-0 Page 112  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Aug 01/94 


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Aug 01/94  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  27-11-0 Page 113 


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27-11-0 Page 114  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Oct 20/84 


TROUBLE  PROBABLE CAUSE  ISOLATION PROCEDURE  REMEDY 
Control wheel does not rotate with initial trim knob input and does not re-center within 2 degrees with hydraulic power on At trimmed position, control wheel forces light in one or both directions with hydraulic power on  LH body cables AA and AB binding or misaligned, fairleads binding, brackets misaligned, or foreign object obstruction LH body cables excessive tension Centering spring and trim mechanism out of adjustment Roll force transducer wire bundle binding on Captain’s control column  Aileron trim mechanism excessive play Transfer mechanism lost motion device out of adjustment  Aileron trim mechanism excessive play  Check LH body cables for chafing or rubbing. Check for dirt or foreign objects Check cable tension per 27-11-0, Adjustment/Test Check mechanism per 27-11-81, Adjustment/Test Rotate control wheel full CCW. Check that wire bundle is not tight Rotate trim knob. Check trim shaft and trim gearbox control rod movement for worn gearbox or worn or loose parts Check if rig pin A/S-1 can be inserted in base of transfer mechanism Rotate trim knob. Check trim shaft and trim gearbox control rod movement for worn gearbox or worn or loose parts  Repair or replace components as necessary Adjust cables as necessary Adjust mechanism as necessary Loosen as necessary (22-11-111, Roll Control Wheel Steering Force Transducer – Adjustment/Test) Replace components as necessary (27-11-81, Removal/Installation) Adjust LH & RH body cables AA & AB per 27-11-0, Adjustment/Test Replace components as necessary (27-11-81, Removal/Installation) 

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Sep 20/81  27-11-0 
Page 115 
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details. 


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27-11-0 Page 116  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  May 15/81 


AILERON AND AILERON TRIM CONTROL SYSTEM - MAINTENANCE PRACTICES
1.  General
A.  Hydraulic systems A and B must be depressurized prior to performing maintenance on aileron control system components. This is to prevent injury to personnel, resulting from inadvertent operation of the control system while maintenance is being performed. Care must be exercised to locate maintenance stands and items of ground equipment beyond the limits of control surface travel.
 
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