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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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 S 222-060
 (6)  
Move the control wheel to its neutral position and do this check:

 (a)  
Make sure the inboard trailing edge of the aileron is aligned with the outboard trailing edge of the main flap (use a tolerance of | 0.06 inch (1.5 mm)).

 (7)  
Examine the PCA hydraulic connections for leaks.


 S 212-061
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 ALL  ú ú 01 Page 216 ú Jan 28/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 F. Put the Airplane Back to Its Usual Condition
 S 862-062
 (1)  
Remove the power from the left, right, and center hydraulic systems (Ref 29-11-00).

 S 862-063

 (2)
Remove electrical power if it is not necessary (Ref 24-22-00).

 S 412-066

 (3)  
Close access panel 561CB (left wing) or 661CB (right wing)
 (Ref 06-44-00).

 

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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757 MAINTENANCE MANUAL
 AILERON POWER CONTROL ACTUATOR (PCA) AND REACTION LINK-
_______________________________________________________ INSPECTION/CHECK
________________
 1.  General_______
 A.  This procedure supplies the data that is necessary to examine the aileron PCA and the Aileron-PCA Reaction-Link assembly for wear. It does not supply the data that is necessary to access, remove, or install the aileron PCA. Refer to the aileron PCA Removal/Installation procedure for this data.
 TASK 27-11-20-206-001
 2.  Examine The Aileron PCA For Wear________________________________
 A.  Access
 (1)  
Location Zones
 568 Aileron (Left)
 668 Aileron (Right)


 B.  
Procedure


 S 226-002
 (1)  Use the supplied data (Fig. 601) to examine the aileron PCA for too much wear.
 TASK 27-11-20-206-003
 3.  Examine The Aileron-PCA Reaction-Link Assembly For Wear_______________________________________________________
 A.  Access
 (1)  
Location Zones
 568 Aileron (Left)
 668 Aileron (Right)


 B.  
Procedure


 S 226-004
 (1)  Use the supplied data (Fig. 602) to examine the Aileron-PCA Reaction-Link assembly for too much wear.
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A

757
MAINTENANCE MANUAL

AILERON INBOARD PCA
SEE A
IDLER LEVER
REACTION-LINK-ASSEMBLY (SEE FIG. 602)
F
PCA
F
AILERON INBOARD PCA
SEE A
B
B

INPUT CONTROL LINKAGE
A C
E
C D
E D
AILERON PCA A
AILERON INBOARD PCA (LEFT SIDE SHOWN, RIGHT SIDE OPPOSITE)
A
AILERON INBOARD PCA A-A
Aileron-PCA Wear Limits
Figure 601 (Sheet 1)

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757
MAINTENANCE MANUAL

1. IDLER LEVER
ASSEMBLY/BUSHING


4. BUSHING/BOLT

3. BRACKET ASSEMBLY/BUSHING
2. BUSHING/BOLT UP 3. BRACKET

B-B
4. BUSHING/BOLT
ASSEMBLY/BUSHING
C-C


PCA ROD END
 
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