S 014-087
(2)
Remove the access panel from the aft bulkhead in the aft cargo compartment.
S 004-090
(3)
Remove the cabin pressurization outflow valve (AMM 21-31-11/401).
D. Procedure
S 024-091
(1)
Disengage the cable at the cable quick-disconnect.
S 024-092
(2)
Remove the cable pin and the tee handle at the service panel.
S 024-093
(3)
Remove the external locknut and washer from the service panel.
S 024-094
(4)
If a shim is installed adjacent to the washer, remove the shim.
S 024-095
(5)
Remove all the clamps.
S 024-096
(6)
Remove the fasteners from the top side of the sleeve subassembly found on the mounting bracket on the right side of the tank.
(7)
Pull the slider housing inboard to remove it from the service panel.
(8)
Remove the cable and casing assembly from the airplane.
S 024-097
S 024-098
TASK 38-32-41-004-061
4. TOILET SYSTEMS WITH THE BALL VALVE; Cable with Casing Removal (Fig. 401)_________________________
A. References
(1)
AMM 12-17-00/301, Toilet Servicing
(2)
AMM 12-31-11/201, Body Section 41 Access Doors and Panels
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ALL ú ú 10 Page 409 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
B.
C.
D.
A
737-300/400/500MAINTENANCE MANUAL
Access
(1) Location Zone 103 Forward Lavatory
Prepare to Remove the Cable Assembly
NOTE: The cable assembly for the toilet systems with the ball valve has
____ two parts: the lower cable assembly and the top cable assembly. This procedure describes the removal of the two assemblies separately.
S 684-050
(1)
Drain and flush the toilet tank (AMM 12-17-00/301).
S 014-062
(2)
Remove the access panels in the nose wheel well (AMM 12-31-11/201).Remove the Lower Cable Assembly (Cable and Casing).
S 024-054
(1)
Remove the pin that holds the T-handle on the shaft and remove the T-handle.
S 024-055
(2)
Remove the lockwire, locknut and tabwasher from the exterior side of the service panel.
S 024-056
(3)
Remove the cotter pin, straight pin and washer to disconnect the clevis from the actuator lever on the ball valve.
S 024-057
(4)
Turn the clevis and nut until they are disengaged from the cable assembly.
S 024-058
(5)
Move the rubber dust cover past the end that has the clevis removed.
S 024-059
(6)
Remove the lockwire and the locknut from the ball valve side of the lower mounting bracket.
S 024-061
(7)
Hold the slider housing at the inboard side of the service panel and carefully pull the cable assembly away from the service panel.
S 024-062
(8)
Pull the cable assembly away from the ball valve and out of the lower mounting bracket.
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38-32-41
ALL ú ú 11 Page 410 ú Nov 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 024-063
(9) Remove the lower cable assembly from the airplane.
E. Remove the Top Cable Assembly.
S 024-064
(1)
Remove the cotter pin, straight pin and washer to disconnect the clevis from the actuator lever.
S 024-065
(2)
Remove the lockwire, locknut and washer from the ball valve side of the higher mounting bracket.
S 024-067
(3)
Remove the clamps that hold the cable assembly to the drain line.
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