Control Cable
 Figure 404/TASK 38-32-42-991-010- 12 (SHEET 1)

R 1EFF : 001-003, 051-052, 1 38-32-42Page 424 1 1 May 01/05 1 1 1CES 1

 Control Cable
 Figure 404/TASK 38-32-42-991-010- 22 (SHEET 2)

R 1EFF : 001-003, 051-052, 1 38-32-42Page 425 1 1 May 01/05 1 1 1CES 1

 TASK 38-32-42-400-003 Installation of the Drain Valve Control-Cable
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific container(s) 5.0 l
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 25-45-13-400-001 Installation of the Lavatory Mirror 38-32-43-400-002 Installation of the Wash Basin Assembly 38-32-42-991-005-B Fig. 401 38-32-42-991-010 Fig. 404
 3. Job Set-up
__________ Subtask 38-32-42-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the ground service network is energized (Ref. TASK 24-41-00-861-002).

 (2)
 Make sure that the water shutoff valve is in the closed position.

R 1EFF : 001-003, 051-052, 1 38-32-42Page 426 1 1 May 01/05 1 1 1CES 1

 4. Procedure
_________
 (Ref. Fig. 404/TASK 38-32-42-991-010) Subtask 38-32-42-420-052
 A. Installation of the control cable.
 (1)
 Put the control cable (52) in position.

 (2)
 Insert the barrel end of the cable into the actuating link (51).

 (3)
 Install the actuating link (51) on the operating handle assembly (58) together with the cable (52) in the angle plate.

 (4)
 Make sure that the ball unit (59) is in the correct position.

 (5)
 Tighten the grub screw (50).

 (6)
 Install the crescent rings (53).

 (7)
 Install the treaded end of the control cable in the drain valve and tighten the grub screw (57).

 (8)
 Install the nut (56).

 (9) Put the lever (55) in position and install the nut (54). Subtask 38-32-42-820-051
 B. Adjustment of the Control Cable
 (Ref. Fig. 404/TASK 38-32-42-991-010)

 (1) Adjust the close position.
 (a)
 Put the operating handle (66) in the close position.

 (b)
 Make sure that the lever (65) contacts the close stop.

 (c)
 Make sure that the plug (60) is closed.

 (d)
 Loosen but do not remove the nut (63).

 (e)
 Adjust the nut (61) and make sure that the distance between the lever (62) and the plug assembly rod (64) is between 0.5 mm (0.0196 in.) and 1.0 mm (0.0393 in.).

R 1EFF : 001-003, 051-052, 1 38-32-42Page 427 1 1 May 01/05 1 1 1CES 1 (f) Tighten the nut (63).

 (2) Operate the operating handle (66) and make sure that the system operates smoothly.
 Subtask 38-32-42-410-054-A
 C. Installation.
 (1)
 Install the wash basin assembly (Ref. TASK 38-32-43-400-002).

 (2)
 Install of the lavatory mirror (Ref. TASK 25-45-13-400-001).

 (a)
 Remove the container.

 (b)
 Open the shutoff valve (1).
 (Ref. Fig. 401/TASK 38-32-42-991-005-B)

 Subtask 38-32-42-790-050
 D. Leal check of the wash basin drain.
 (1)
 Close the wash basin drain valve

 (2)
 Put a container(s) 5.0 l drain mast 4DU and 14DU.

 (3)
 Put approximately 2.0 l (0.5283 USgal) of water into the wash basin.

 (4)
 Make sure that the water does not flow from the wash basin.

 (5)
 Examine the wash basin drain for leaks.
 NOTE : Leaks are not permitted.

____

 (6)
 Open the wash basin drain.

 (7)
 Make sure that the water flows from the wash basin.

 (8)
 Remove the container(s).

R 1EFF : 001-003, 051-052, 1 38-32-42Page 428 1 1 May 01/05 1 1 1CES 1
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM WATER/WASTE 2(130)