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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 424-071

 (16)
 Use the swaging die and portable swager to swage the ball to the cable.


 NOTE: Swage ball to conform to MS20664C3 contour.
____
 S 864-000
 (17)
 Cut off the unwanted part of the cable.

 S 424-072

 (18)
 Install the cable assembly at the cable quick-disconnect.

 S 714-073

 (19)
 With the drain valve in the closed position, make sure the cable moves 1/2 inch, with cable load of 5 pounds, before the valve starts to open.

 S 834-074

 (20)
 If it is necessary, adjust the locknuts at the mounting bracket to get the 1/2 inch movement.


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 38-32-41
 ALL  ú ú 09 Page 417 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 424-080
 (21)
 Install the lockwire on the two locknuts on the mounting bracket.

 S 714-075

 (22)
 Operate the tee handle to make sure the drain valve operates correctly.

 S 414-076

 (23)
 Install the access panel on the aft bulkhead in the aft cargo compartment.

 S 414-079

 (24)
 Install the cabin pressurization outflow valve (AMM 21-31-11/401).


 TASK 38-32-41-404-141
 7.  TOILET SYSTEMS WITH THE BALL VALVE; Cable with Casing Installation______________________________
 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 - AT520J, ATI Industries (V00784)

 (3)  
Swaging Die - AT520CSB-3-332, Ball type, ATI Industries (V00784)


 B.  References
 (1)  
AMM 12-31-11/201, Body Section 41 Access Doors and Panels

 (2)  
AMM 25-21-39/401, Sidewall and Ceiling Insulation

 (3)  
AMM 25-52-91/401, Cargo Compartment Insulation


 C.  Access
 (1)  Location Zone
 103 Forward Lavatory

 D.  Procedure to Install the Lower Cable Assembly
 S 864-074
 (1)  
Make sure that the clevis, clevis nut, rubber boot and one locknut and washer are removed from the clevis end of the cable assembly.

 S 824-075

 (2)  
Make sure that one locknut and one washer are installed at approximately the center of the threaded section.


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 38-32-41
 ALL  ú ú 17 Page 418 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 (3)  S 424-076Put the lower cable assembly in its approximate position.
 (4)  S 424-078Move the clevis end of the cable assembly through the lower side of the lower mounting bracket (towards the ball valve).
 (5)  S 424-079Install the washer and locknut on the clevis end and move them to the lower mounting bracket.
 (6)  S 424-150Install the rubber boot.
 (7)  S 424-149Install the clevis nut and the clevis.
 (8)  S 824-082Turn the clevis nut and clevis until there is 15 inches between the center of hole in the clevis and the near end of the threaded section.
 (9)  S 424-083Put the service panel end of the cable assembly through the hole in the service panel.
 S 424-084

 (10)
 On the external side of the service panel, install the tabwasher, locknut and lockwire.

 S 424-085

 (11)
 Install the T-handle.

 S 824-086

 (12)
 Adjust the clevis to connect with the actuator lever when the ball valve is fully closed and the T-handle is almost fully up.

 S 224-087

 (13)
 Make sure that you can see the end of threaded rod come thru the clevis.

 S 824-088

 (14)
 If it is necessary, turn the locknuts in the lower mounting bracket to give the necessary extnetion.
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 WATER AND WASTE(76)