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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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 27-18-00
 ALL  ú ú 03 Page 504 ú Dec 20/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

 S 865-015
 (14)
 Open this circuit breaker on the P11 panel and attach a DO-NOT-CLOSE tag:

 (a)  
11J22 or 11J23, AILERON POS RIGHT


 S 215-016
 (15)
 Turn the control wheel clockwise and then counterclockwise and do the check that follows:

 (a)  
Make sure that the aileron position pointers do not move.


 S 825-017
 (16)
 Move the control wheel to its neutral position.

 S 865-018

 (17)
 Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P11 panel:

 (a)  
11J14, AILERON POS LEFT

 (b)  
11J22 or 11J23, AILERON POS RIGHT


 S 865-019
 (18)
 Remove the power from the left, right, and center hydraulic systems (Ref 29-11-00).

 S 865-020

 (19)
 Remove electrical power if it is not necessary (Ref 24-22-00).


 TASK 27-18-00-825-064
 3. Adjustment - Aileron Position Indicating System
_______________________________________________
 A. General
 (1)  
Make sure that the aileron PCAs are rigged correctly before you adjust the aileron position transmitters (Ref 27-11-00).

 B.
Equipment

 (1)  
Main Gear Door Locks (Ref 32-00-15)

 (2)  
Rig Pins from set B20003-XX (Ref 20-10-24)

 (a)  
A1 - P/N B20003-27

 (b)  
A2 - P/N B20003-25

 (c)  
A3 - P/N B20003-23

 (d)  
A4 - P/N B20003-23

 (3)
Equipment that is necessary for the adjustment (Procedure 1):

 (a)  
Angle Position Indicator (API) - 8810 North Atlantic Model (North Atlantic Industries Inc., Hauppauge, New York)

 (b)  
Breakout Box and Cables, Rigging, Flight Controls Position Sensors (from Breakout Box Equipment A27063-91): 1) Breakout Box - A27063-2 2) Cable Assembly A27063-19


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-18-00
 ALL  ú ú 01 Page 505 ú May 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL

HI

A27063-2
ASSEMBLY
BREAKOUT BOX
METHOD 1
Aileron Position-Transmitter Adjustment
Figure 502 (Sheet 1)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ú  01  Page 506
 ú  Mar 20/90 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL 
DVM 
SIG HI  SIG LO  TRANSMITTER CONNECTOR 


METHOD 2 BOX BREAKOUT A27063-2 
AIRPLANE  SIG SIG HI LO 1 DVM  TRANSMITTER CONNECTOR 


DVM - DIGITAL VOLTMETER
METHOD 3
____IF ONLY ONE DVM IS USED,NOTE: MONITOR THE AIRPLANE POWER

RIGHT AILERON
AS SHOWN (DMV 2). THEN
POSITION TRANSMITTER
CONNECT IT TO THE BREAKOUT
LEFT AILERON
BOX AS SHOWN (DVM 1) TO DO THE
POSITION TRANSMITTER
Aileron Position-Transmitter Adjustment
Figure 502 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú
 ú  01  Page 507
 ú  Mar 20/90 

BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757 MAINTENANCE MANUAL
 
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