38-32-72
 ú ú 01 Page 401 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

WITNESS HOLE
Ball Valve Rod Assembly Installation Figure 401
 C82137
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. FREIGHTERS ú

 38-32-72
 ú ú 01 Page 402 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 864-009
 (8)  Connect the jamnut and clevis to the rod assembly.
 TASK 38-32-72-404-010
 3.  Ball Valve Rod Assembly Installation (Fig. 401)____________________________________
 A. Consumable Materials
 (1)  D00015 - BMS 3-24 Grease, Corrosive Preventative
 B. References
 (1)  
AMM 12-17-61/301, Toilet Tank - Servicing

 (2)  
AMM 24-22-00/201, Manual Control

 C. Access
 (1)  Location Zone 126 Area Below Fwd Cargo Container Compartment
 D. Procedure
 S 864-011
 (1)  
If it is necessary, remove the clevis and jamnut from the input end of the rod assembly.

 S 424-012

 (2)  
Put the input end of the rod assembly through the bearing on the outer side of the toilet service panel.

 S 434-013

 (3)  
Install the clevis and jamnut on the rod assembly.

 S 834-014

 (4)  
Adjust the clevis and jamnut to make sure the distance from the top of the jamnut to the top of the rod is that which was measured during removal (distance "A").

 (5)
Make sure that you can see threads through the witness hole.

 S 864-016

 (6)
Remove the cotter pin, nut, bolt and washers that were loosely installed on the valve arm during the removal procedure.

 S 644-017

 (7)  
Put a thin layer of grease on the surfaces of the bolt and the clevis.

 S 824-015
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. FREIGHTERS ú

 38-32-72
 ú ú 01 Page 403 ú Oct 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-018
 (8)  Connect the rod assembly to the valve arm with the bolt and washers.
 NOTE: The nut and cotter pin will be attached after the adjustment
____
 steps.

 S 864-019
 (9)  
Move the valve arm to the fully closed position.

 S 224-020

 (10)
 Measure the distance from the end of the drain valve handle to the service panel.

 S 834-021

 (11)
 If the distance is not 2.10 inches, do the steps that adjust the clevis.

 E. Adjust the Rod Assembly Clevis
 S 824-034
 (1)  
Do an estimate of the number of turns of the clevis that are necessary to meet the above 2.10 inch dimension.

 S 864-032

 (2)  
Disconnect the valve assembly from the valve arm.

 S 824-035

 (3)  
Turn the clevis the number of turns that you estimated in the above step.

 S 824-022

 (4)  
Make sure that you can see threads through the witness hole.

 (5)
Connect the clevis to the valve arm with the bolt and washers.

 S 864-033

 (6)  
With the valve closed, make sure the distance from the end of the handle to the service panel is 2.10 inches.

 (7)
If it is necessary, do the steps that adjust the clevis again.

 S 864-031
 S 824-036
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. FREIGHTERS ú
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 氣動系統(tǒng) WATER/WASTE(79)