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时间:2011-04-12 10:37来源:蓝天飞行翻译 作者:航空
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_______ 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: "Nose Landing Gear Door Lock Installation" (AMM 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-36-08
 ALL  ú ú 01 Page 401 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 494-005
 (3)  Do this task: "Body Landing Gear Door Lock Installation"
 (AMM 32-00-30/201).

 S 034-006
 WARNING: MAKE SURE THAT ALL PERSONS AND EQUIPMENT ARE CLEAR OF THE DOOR
_______ OPERATION AREA. FAST MOVEMENT OF THE DOORS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (4)  
Do this task: "Wing Landing Gear Door Operator Rods Disconnection" (AMM 32-00-30/201).

 S 864-005

 (5)
Remove the power from the hydraulic system 1 (AMM 29-11-00/201).

 S 864-006

 (6)  
Pressurize the hydraulic system 4 (AMM 29-11-00/201).

 S 864-007

 (7)  
Move the ground release handle for the doors of the main landing gear to the DOORS CLOSED position.

 S 864-008

 (8)
Remove the power from the hydraulic system 4 (AMM 29-11-00/201).

 S 984-009

 (9)  
Put the door actuator for the wing landing gear in its closed and locked position.


 NOTE: This is the extension of the actuator when the doors for the
____ wing landing gear are in the closed and locked position.
 D. Removal (Fig. 401)
 S 034-007
 (1)
Disconnect the differential output rod from the ground release cam.

 (2)  
Remove the nut, shims, washers, and the ground release cam.

 S 034-009

 (3)  
Disassemble the ground release cam if it is necessary.

 (a)  
Remove the bearings.

 (b)  
Remove the spacer.


 S 034-008
 S 034-010
 (4)  
Remove the lever assembly.

 (a)  
Disassemble the lever assembly if it is necessary.

 (b)  
Remove the bolt.


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 32-36-08
 ALL  ú ú 01 Page 402 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
SEE A
DOOR ACTUATOR
FWD
ACTUATOR BEAM
SEE B
A
DOOR ACTUATOR
B
DOOR ACTUATOR
A
BEARING
GROUND RELEASE CAM
A  0.08 |0.01
DIFFERENTIAL LEVER OUTPUT ROD ASSEMBLY
BOLT WASHER NUT (2 LOCATIONS)
DIFFERENTIAL
LEVER

OUTPUT ROD
ASSEMBLY

GROUND RELEASE CAM
BEARING
A B
NUT
0.19 |0.01
NUT
A
RIGHT SIDE
B  LEFT SIDE
Wing Landing Gear Door Actuator Release Mechanism
Figure 401 (Sheet 1)

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 32-36-08
 ALL  ú ú 01 Page 403 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


DIFFERENTIAL OUTPUT ROD
A-A
DIFFERENTIAL
OUTPUT ROD


FWD GROUND RELEASE CAM
B-B

1
DIMENSIONS EQUAL WITHIN 0.02 INCH

Wing Landing Gear Door Actuator Release Mechanism
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-36-08
 ALL  ú ú 01 Page 404 ú Oct 10/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
 
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本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 6(13)