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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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 (5)  Push the STATUS button on the pilot's select-display panel, P9, to show the aileron position indicator on the bottom EICAS display.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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MAINTENANCE MANUAL

 S 215-007
 (6)  
Move the EICAS computer-select switch on the P9 panel to L and do the check that follows:

 (a)  
Make sure that the aileron position pointers are aligned with the mid-scale mark on the aileron position indicator.


 NOTE: use a tolerance of +/- one-half an arrow width.
____
 S 215-008
 (7)  
Turn the control wheel clockwise and do the check that follows:

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


 S 215-009
 (8)  
Turn the control wheel counterclockwise and do the check that follows:

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


 S 215-010
 (9)  
Move the EICAS computer-select switch on the P9 panel to R and do the check that follows:

 (a)  
Make sure that the aileron position pointers are aligned with the mid-scale mark on the aileron position indicator.


 NOTE: Use a tolerance of +/- one-half an arriw width.
____
 S 215-011
 (10)
 Turn the control wheel clockwise and do the check that follows:

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


 S 215-012
 (11)
 Turn the control wheel counterclockwise and do the check that follows:

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


 S 865-013
 (12)
 Open this circuit breaker on the P11 panel and attach a DO-NOT-CLOSE tag:

 (a)  
11J14, AILERON POS LEFT


 S 215-014
 (13)
 Turn the control wheel clockwise and do the check that follows:

 (a)  
Make sure that the left aileron position pointer shows no movement and the right position pointer moves up.


 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 01 Page 502 ú Dec 20/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757
MAINTENANCE MANUAL

AILERON POSITION TRANSMITTER
SEE A
FWDAILERON QUADRANT AND OVERRIDE MECHANISM
SEE B
SCREW, BUSHING,
WASHER, NUT
TRANSMITTER
POSITION CONTROL ROD
TRANSMITTER
CRANK

TRANSMITTER
BRACKET

A
AILERON
POSITION TRANSMITTER
SCREW, WASHER,
ELECTRICAL
NUT
CONNECTOR
FINEMOUNTING RIG PIN HOLE
ADJUSTMENT
BRACKET A3 (LEFT AILERON)NUT A A4 (RIGHT AILERON)
FWD INBD
AILERON POSITION TRANSMITTER
A
POSITION TRANSMITTER
SCREW
TRANSMITTER
BRACKET
AILERON QUADRANT AND OVERRIDE MECHANISM
B
A-A Aileron Position-Indicating System Adjustment Figure 501 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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 ALL  ú ú 01 Page 503 ú Dec 20/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

757
MAINTENANCE MANUAL

LATERAL CONTROL-OVERRIDE MECHANISM LATERAL FEEL,
RIG PINSEE D
CENTERING, AND
HOLES A1 TRIM MECHANISM
SEE C
FWD INBD
LATERAL FEEL, CENTERING, AND TRIM MECHANISM C
RIG PIN HOLES A2
INBD FWD
LATERAL CONTROL-OVERRIDE MECHANISM D
Aileron Position-Indicating System Adjustment
Figure 501 (Sheet 2)
 
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