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时间:2011-04-13 08:07来源:蓝天飞行翻译 作者:航空
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 S 434-006

 (2)  
Remove the protective caps or the plugs from the open lines, fittings, or ports.

 S 424-007

 (3)  
Install the pressure regulator:

 (a)  
Put the pressure regulator in the position on the dripshield on the aft right sidewall.

 (b)  
Loosely connect the inlet and the outlet lines.

 (c)  
Install the fasteners

 (d)  
Tighten the inlet and outlet lines.

 


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 35-11-05
 ALL  ú ú 01 Page 403 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 434-010
 (4)  Install the closure assembly in the right coat closet (Fig. 401).
 (a)  Move the RESET lever (sliding control) on the demand regulator to N (normal).
 S 864-018
 WARNING:_______OPEN THE SHUTOFF VALVE ON THE CREW OXYGEN CYLINDER SLOWLY. IF NOT, HIGH TEMPERATURES CAN OCCUR WHICH CAN START AN IGNITION WITH THE OXYGEN. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE AIRPLANE AND EQUIPMENT.
 CAUTION: DO NOT TIGHTEN THE SHUTOFF VALVE ON THE CREW OXYGEN CYLINDER
_______ MORE THAN 25 POUND-INCHES. THIS CAN CAUSE DAMAGE TO THE SHUTOFF VALVE.
 (5)  Open the shutoff valve on each crew oxygen cylinder:
 NOTE: Some airplanes have an optional second oxygen cylinder.
____
 (a)  Slowly turn the shutoff valve until it is fully open.
 NOTE: The shutoff valve can be closed by hand which is
____
 equivalent to 25 pound-inches.

 (b)  
Close the shutoff valve one-fourth of a turn.

 (c)  
Install a lockwire on the shutoff valve.


 NOTE: Use the 0.020 inch diameter coppper lockwire
____
 (AMM 20-11-28/401).

 S 794-009
 (6)  
Do a check of the inlet and outlet line connections for leaks with the leak detection compound for the oxygen system.

 (7)  
Rub off the leak detection compound after you have done the check.


 S 144-020
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 35-11-05
 ALL  ú ú 01 Page 404 ú Oct 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 414-023
 (8) Close the cylinder access door.
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 35-11-05
 ALL  ú ú 01 Page 405 ú Jun 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 OVERBOARD DISCHARGE INDICATOR - REMOVAL/INSTALLATION
____________________________________________________
 1.  General_______
 A.  These tasks are included in this procedure:
 (1)  
Removal of the overboard discharge indicator.

 (2)  
Installation of the overboard discharge indicator.


 B.  The overboard discharge indicator is a plastic disc. Dirt, grease, and most other contaminants will not normally enter the overboard discharge line with the overboard discharge indicator installed. The overboard discharge indicator will blow out if the safety valve on the cylinder opens. This permits pressure in the overboard discharge line to increase to 500 psi.
 C.  The overboard discharge indicator is installed aft of the forward cargo door in the airplane skin (Fig. 401). Access is from outside of the airplane.
 TASK 35-11-10-004-001
 2.  Overboard Discharge Indicator Removal (Fig. 401)_____________________________________
 A.  References
 (1)  
AMM 35-00-00/201, Oxygen

 (2)  
IPC 35-11-10


 B.  Access
 (1)  Location Zone 124 Forward Cargo Container Compartment, Aft Half Right
 C.  Procedure
 
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本文链接地址:747-400 AMM 飞机维护手册 氧气 OXYGEN(34)