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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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_______ HYDRAULIC POWER IS SUPPLIED. AILERONS, ELEVATORS, RUDDER, FLAPS, SLATS, SPOILERS, AND STABILIZER ARE FULLY POWERED SURFACES. INJURY TO PERSONS OR DAMAGE TO EQUIPMENT CAN OCCUR WHEN HYDRAULIC POWER IS SUPPLIED.
 (22) Supply pressure to the left, right, and center hydraulic systems (Ref 29-11-00/201).
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 S 714-037
 (23)
 Turn the control wheel clockwise and do this check:

 (a)  
Make sure the right aileron moves up and the left aileron moves down.


 S 714-038
 (24)
 Turn the control wheel counterclockwise and do this check:

 (a)  
Make sure the right aileron moves down and the left aileron moves up.


 S 864-061
 (25)
 Turn the captain's control wheel fully counterclockwise and use a clamp to hold it there.

 S 214-051

 (26)
 Turn the first officer's control wheel through its full travel range and do these checks:

 (a)  
Make sure the ailerons operate correctly.

 (b)  
Make sure the right aileron moves fully up.


 S 864-040
 (27)
 Remove the clamp from the captain's control wheel.

 F.
Put the Airplane Back to Its Usual Condition


 S 094-041
 WARNING:  USE THE PROCEDURE IN AMM 32-00-15 TO REMOVE THE DOOR LOCKS. THE DOORS OPEN AND CLOSE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (1)  
Remove the door locks from the landing gear doors and close the doors (Ref 32-00-15/201).

 S 864-042

 (2)  
Remove the power from the left, right, and center hydraulic systems (Ref 29-11-00/201).


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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 (3)  S 864-043Remove electrical power if it is not necessary (Ref 24-22-00/201).
 (4)  S 414-044Close the access panel, 661AB (Ref 06-44-00/201).

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 ALL  ú ú 01 Page 411 ú Sep 20/91
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757 MAINTENANCE MANUAL
 AILERON QUADRANT AND OVERRIDE MECHANISM -
_______________________________________ REMOVAL/INSTALLATION
____________________
 1.  General_______
 A.  This procedure contains two tasks. One task is to remove the aileron quadrant and override mechanism and the other is to install it.
 TASK 27-11-17-024-001
 2.  Remove the Aileron Quadrant and Override Mechanism__________________________________________________
 A.  Equipment
 (1)  
Landing Gear Door Locks (Ref 32-00-15)

 B.  
References

 (1)  
06-44-00/201, Wing Access Doors and Panels

 (2)  
24-22-00/201, Electrical Power - Control

 (3)  
29-11-00/201, Pressurize/Depressurize Main Hydraulic Systems

 (4)  
32-00-15/201, Landing Gear Door Locks

 (5)  
32-00-20/201, Landing Gear Downlocks

 C.  
Access

 (1)  
Location Zones
 568 Aileron (Left)
 668 Aileron (Right)
 730 Left Main Landing Gear and Doors
 740 Right Main Landing Gear and Doors


 (2)  
Access Panels
 561AB (Left Wing)
 561BB (Left Wing)
 661AB (Right Wing)
 661BB (Right Wing)


 D.  
Procedure

 (1)  
Supply electrical power (Ref 24-22-00).
 
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