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时间:2011-04-12 10:20来源:蓝天飞行翻译 作者:航空
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 C.  
This procedure introduces an optional split scraper ring which can be used to replace the damaged scraper ring on the gear without the removal of the gear or disassembly of the gear. This procedure also has two quick checks to examine the scraper ring without the removal of the gear or disassembly of the gear.


 TASK 32-13-02-002-001
 2.  Body Landing Gear Shock Strut Pressure Gage Removal (Fig. 201)
___________________________________________________
 A.  References
 (1)  
09-11-00/201, Towing

 (2)  
32-00-30/201, Landing Gear Door Locks

 (3)  
IPC 32-13-01 Fig. 5, IPC 32-21-01 Fig. 4

 B.  
Access

 (1)  
Location Zone
 755 Body Landing Gear, LH
 765 Body Landing Gear, RH


 C.  
Prepare for the Procedure


 S 492-036
 WARNING: YOU MUST CAREFULLY INSTALL THE GROUND LOCKS IN ALL LANDING
_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
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 32-13-02
 ALL  ú ú 01 Page 201 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (1) Install the ground locks in all landing gear (Ref 09-11-00/201).
 S 492-037
 WARNING: YOU MUST CAREFULLY DO THE STEPS IN THE TASKS BELOW TO INSTALL
_______ THE DOOR LOCKS ON THE LANDING GEAR DOORS. THE DOORS CAN CLOSE QUICKLY IF YOU DO NOT INSTALL THE DOOR LOCKS CORRECTLY. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (2)  
Do this task: "Installation of the Door Locks on the Wing Landing Gear" (Ref 32-00-30/201).

 S 492-038

 (3)  
Do this task: "Installation of the Door Locks on the Body Landing Gear" (Ref 32-00-30/201).

 D.
Procedure


 S 862-004
 (1)  
Close the shutoff valve for the pressure gage (9) with a 3/16-inch hex wrench.

 S 872-059

 (2)
Use the oil fill valve (4) to bleed the pressure from the tube between the pressure gage (3) and the shutoff valve (9).


 NOTE: Use a small container to catch all fluid when it comes
____
 through the oil fill valve.

 S 032-058
 (3)  
Disconnect the tube from the pressure gage assembly (3).

 S 022-060

 (4)  
Remove the four nuts (2) and washers (1) which hold the pressure gage assembly (3) to the clamps on the shock strut.


 NOTE: The bolts must stay in the clamps after you remove the nuts
____
 and washers.

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 32-13-02
 ALL  ú ú 01 Page 202 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

7.  FLOW FUSE
OUTER
9.  SHUTOFF CYLINDER
VALVE
SEE  B 
GAGE ASSEMBLY STRUT CLAMP  3.  PRESSURE GAGE ASSEMBLY 

EXTENSION INDICATOR
4.  OIL FILL CHARGINGSEE A CHECK VALVE
SHOCK STRUT OUTER CYLINDER
1.  
WASHER (4 LOCATIONS)

2.  
NUT (4 LOCATIONS)

3.  
PRESSURE GAGE ASSEMBLY

4.
OIL FILL CHARGING (O-RING) CHECK VALVE


6.  PACKING
5.  CAP
A
Body Gear Shock Strut Details Figure 201 (Sheet 1)
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 32-13-02
 ALL  ú ú 01 Page 203 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


B

Body Gear Shock Strut Details
Figure 201 (Sheet 2)

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