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时间:2011-04-12 10:27来源:蓝天飞行翻译 作者:航空
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_______ GEAR. AN ACCIDENTAL RETRACTION OF THE LANDING GEAR CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (1) Install the ground locks in all landing gear (Ref 09-11-00/201).
 S 494-003
 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: "Wing Landing Gear Door Lock Installation" (Ref 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-29
 ALL  ú ú 01 Page 401 ú Feb 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 494-013
 (3)  
Do this task: "Body Landing Gear Door Lock Installation" (Ref 32-00-30/201).

 S 864-004

 (4)  
Remove the hydraulic pressure from system No. 4 (Ref 29-11-00/201).

 D.
Removal


 S 024-005
 (1)  
Remove the door safety valve (Fig. 401):

 (a)  
Disconnect the hydraulic lines from the valve and install plugs.

 (b)  
Disconnect the four bolts that attach the valve to the differential assembly.

 (c)  
Remove the clamping bolt from the lever.

 (d)  
Remove the lever from the shaft with splines.

 (e)  
Remove the safety valve.

 (f)  
Remove the hydraulic fittings from the valve and install plugs in the ports.


 TASK 32-32-29-404-006
 3.  Wing Landing Gear Door Safety Valve Installation________________________________________________
 A. Consumable Materials
 (1)  
D00288 Lubricant - MCS 352 (Skydrol Assembly Lube)

 B.
References

 (1)  
29-11-00/201, Main Hydraulic Supply System

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

 (3)  
IPC 32-36-08 Fig. 10

 C.
Access

 (1)  
Location Zone
 135 Wing Landing Gear Wheel Well, LH
 136 Wing Landing Gear Wheel Well, RH


 D.
Installation


 S 434-015
 (1)  
Install the hydraulic fittings in the valve:

 (a)  
Lubricate the new O-rings and the backup rings with Skydrol Assembly Lube.

 (b)  
Install the new O-rings, the backup rings and the fittings in the safety valve.


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 32-32-29
 ALL  ú ú 01 Page 402 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

SEE B
SEE A
SAFETY VALVE  A 
SAFETY VALVE LEVER 
A  DIFFERENTIAL ASSEMBLY 
CLAMPING BOLT 

RELEASE LINKAGE FOR THE DOOR ACTUATOR  VALVE ATTACH BOLT (4 LOCATIONS) 

MISSING TOOTH
A-A
B

Wing Landing Gear Safety Valve Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-32-29
 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 424-014
 (2)  
Install the door safety valve (Fig. 401):

 (a)  
Put the valve in the position above the differential assembly housing. 1) Install the shaft with splines in the hole in the safety


 valve lever.
 NOTE: The splines on the shaft must align with the splines
____ in the hole in the safety valve lever (Section A-A, Fig. 401).
 (b)  
Install the four valve attach bolts in the nutplates on the differential housing.

 (c)  
Tighten the four valve attach bolts.
 
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本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 4(108)