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时间:2011-04-03 11:21来源:蓝天飞行翻译 作者:航空
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 S 834-097

 (18)
 If it is necessary, adjust the locknuts at the sleeve subassembly to get the 1/2 inch movement.

 S 424-098

 (19)
 Install the lockwire on the two locknuts on the sleeve subassembly.

 S 714-099

 (20)
 Operate the tee handle to make sure the drain valve operates correctly.

 S 414-100

 (21)
 If removed, install the access panels in the nose wheel well (AMM 12-31-11/201).

 S 414-101

 (22)
 If removed, install the access panel on the aft bulkhead in the aft cargo compartment.

 S 414-102

 (23)
 If removed, install the cabin pressurization outflow valve (AMM 21-31-11/401).

 S 824-092

 (24)
 Pull the cable end to meet with the cable quick-disconnect and make a mark to indicate where the ball will join the quick-disconnect.


 TASK 38-32-41-404-026
 6. Cable with Casing Installation (Auxiliary Waste Tank) (Fig. 401)
______________________________
 A. Equipment and Materials
 (1)
The Ball End of the Cable (use either of the following):

 (a)
Part No. 24835, Teleflex Inc. (V78710)

 (b)
MS20664C3

 

 (2)
The Portable Swager - AT5202J, ATI Industries (V00784)

 (3)
Swaging Die - AT520C58-3-332, Ball Type, ATI Industries (V00784)


 B. Reference
 (1) AMM 21-31-11/401, Cabin Pressurization Outflow Valve
 C. Access
 (1)  Location Zone
 220 Aft Cargo Equipment Bay

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 38-32-41
 ALL  ú ú 09 Page 415 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 D. Procedure
 S 864-055
 (1)  Make sure the external locknut, washer and shim are removed from the service panel end of the cable assembly.
 NOTE:____Some cable assemblies do not have the shims. Ignore the steps and parts of steps for shims if they are not applicable.
 S 824-056
 (2)  
Make sure the internal locknut is adjusted to a position that allows the shim and washer to be just inboard of the center of the threaded section.

 S 424-057

 (3)  
From inside of the airplane, put the service panel end of the cable assembly into the service panel.

 S 424-058

 (4)  
Loosely install the external shim, washer, and locknut.

 S 824-059

 (5)  
Adjust the two shims to align the cable assembly in the correct direction.

 S 824-060

 (6)  
Turn the slider housing to align the flatted surfaces of the threaded section with the shorter sides of the placard for the tee handle.


 NOTE: The flatted surfaces of the threaded section will be
____ perpendicular to the tee handle when the tee handle is in the closed position.
 S 424-061
 (7)  
Tighten the external locknut and install the lockwire.

 (8)  
Install the tee handle and the pin.

 (9)  
Install the clamps.

 S 864-064

 (10)
 Remove the top locknut and washer from the ball end of the cable assembly.


 S 424-062
 S 424-063
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 38-32-41
 ALL  ú ú 09 Page 416 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 824-065
 (11)
 Make sure the bottom locknut and washer are just below the center of the threaded section.

 S 424-066

 (12)
 Install the cable assembly in the mounting bracket on the right side of the tank.

 S 424-067

 (13)
 Install the top washer and locknut.

 S 424-068

 (14)
 Put the ball end of the cable through the pulley.

 S 824-069

 (15)
 Move the ball end of the cable to align with the cable quick-disconnect.
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 WATER AND WASTE(75)