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.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 WATER AND WASTE(76)