CAUTION:  SHARP EDGES WILL DAMAGE CASING WHEN PULLING CABLE OUT.

(c)  
Carefully cut end of control cable at right angles to cable centerline. Avoid sharp edges.

NOTE:  If cable is broken at this point, it must still be cut to eliminate sharp edges.
(5)  If cable is not broken at control panel, proceed as follows:
CAUTION:  SHARP EDGES WILL DAMAGE CASING WHEN PULLING CABLE OUT.
(a)  
Just above cable ball end, carefully cut through cable at right angles to cable centerline. Avoid sharp edges.

(b)  
Remove cable by pulling handle at control panel.

5.  Install Cable without Casing (Fig. 401)
A.  Equipment and Materials
(1)  
Ball End (use either of the following):

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

(b)
 MS20664C3

(2)
Portable Swager - AT520J, ATI Industries (V00784)

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

(4)
Grease - Dow Corning 33, light consistency

(5)
Grease - MIL-G-23827

532 
38-32-41 Page 402  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Oct 20/85 

532  Toilet Drain Valve Control Cable Installation 
Oct 20/85  Figure 401 BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  38-32-41 Page 403 

B. Install Cable
(1)
Lubricate entire length of cable with a light film of Dow Corning 33 grease.

(2)
Lubricate slider assembly with MIL-G-23827 grease.

(3)
Insert cable and slider assembly into panel. Install handle in locked position.

(4)
Swage ball end to cable using swaging die and portable swager.

NOTE:  Swage ball to conform to MS20664C3 contour.

(5)
Engage cable at quick-disconnect.

NOTE:  With drain valve closed check that there is a 1/2-inch cable movement, with a cable load of approximately 5 pounds, before the valve starts to open.
If necessary, reroute casing and reinstall clamps. Reinstall insulation as necessary (Ref 25-21-51 or 25-52-141).
(6) Check that drain valve operates properly.
C. Install shroud(s) and/or access panels as necessary.
532 
38-32-41 Page 404  BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.  Oct 20/86 

TOILET GROUND FLUSH LINE - REMOVAL/INSTALLATION
1. General
A.  This procedure gives the data to remove and install the ground flush line for the toilet waste tank(s).
B.  The ground flush lines for the modular lavatories have a routing that begins at the service panel and follows the drain line to the area below the lavatory. The ground flush lines go through a hole in the crease beam just outboard of the lavatory and enter the lavatory through the outboard partition.
C.  The toilet flush lines for the non-modular lavatories A, B, and C have two sections, the top and the bottom. The bottom section is connected at the service panel and the connection (union) is under the lavatory. The top section is attached to the bottom section at the connection at the lavatory floor and then is connected to the toilet tank. If only the top or bottom section is damaged, it is not necessary to replace the remaining section.
2.  Toilet ground Flush Line Removal
A.  References
(1)  
AMM 12-17-0, Toilet Servicing

(2)  
AMM 12-31-11, Body Section 41 Access doors and Panels

(3)  
AMM 25-40-01, Modular Lavatory Compartment

B.  Access
(1)  Location Zones
103 Forward Lavatory A
113 Aft Left Lavatory B
114 Aft Right Lavatory C
118 Aft left Lavatory D
109 Aft Right Lavatory E 

NOTE: Not all Lavatories are installed on each airplane.
C.  Procedure
(1)  
Drain the toilet tank (AMM 12-17-0).

(2)  
Remove the fasteners and remove the toilet shroud assembly, using the removal procedure for the lavatory waste tank (AMM 38-32-51).

(3)  
Disconnect the ground flush line from the toilet tank.

(4)  
Remove the clamps that hold the ground flush line in the lavatory compartment.

(5)  
For the modular lavatories, perform these steps to remove the clamp that is just outboard of the lavatory.

(a)  
For lavatories A, C, D, E, or F, move the lavatory module inboard approximately 6 inches (AMM 25-40-01).

(b)  
For lavatory B, remove the fasteners and the attendant’s panel at the lower outboard corner of the forward partition.
　
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