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时间:2011-04-12 10:37来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 (1)  
Do this task: "Removal of the Door Locks on the Wing Landing Gear" (AMM 32-00-30/201).

 S 096-061

 (2)  
Do this task: "Removal of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).


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 32-41-15
 ALL  ú ú 01 Page 607 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

MAIN GEAR TRUCK BEAM
A
ASSEMBLY
A
BB
____ THE LEFT WING GEAR IS SHOWN, THE GEAR AT ALLNOTE: BRAKE ROD BRAKE TORQUE ARM
OTHER LOCATIONS ARE EQUIVALENT.
THE TIRES, WHEELS, BRAKE UNITS AND BRAKE RODS
ON THE NEAR SIDE OF THE TRUCK ARE NOT SHOWN.

AXLE SLEEVE
BRAKE TORQUE
ARM
3.  BUSHING/BOLT
BRAKE
2.  BUSHING/
ROD
BRAKE OUTER
BEARING

6.  BUSHING/ 5. BOLT/ BUSHING BUSHING
1.  BUSHING/ BRAKE INNER BEARING
4.  BUSHING/BOLT 3. BUSHING/BOLT
MAIN GEAR
TRUCK BEAM (EXAMPLE, 4 LOCATIONS)

ASSEMBLY
B-B
(EXAMPLE, 4 LOCATIONS)
(THE BRAKE HOUSING IS NOT SHOWN)
A-A

Wear Limits for the Landing Gear Brake Unit
Figure 602 (Sheet 1)

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 32-41-15
 ALL  ú ú 01 Page 608 ú Oct 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  PART WORN REPLACE  PART WORN REPAIR  INSTR REPAIR 
DIAMETER  PER-MITTED WEAR DIM. 6  ANCE CLEAR-MAX DIA 
MIN  MAX 
1  BEARING BRAKE INNER  ID  6.2050  6.2070  6.2100  TBD  1 
BUSHING  OD  6.1970  6.1990  6.1920  X 
2  BEARING BRAKE OUTER  ID  6.2050  6.2070  6.2100  TBD  1 
BUSHING  OD  6.1970  6.1990  6.1920  X 
3  BUSHING  ID  1.2510  1.2530  1.2552  0.0072  1 
BOLT  OD  1.2480  1.2490  1.2458  1 
4  BUSHING  ID  1.2500  1.2510  1.2532  0.0052  X 
BOLT  OD  1.2480  1.2490  1.2458  1 
5  BOLT  2  3.5150  3.5340  3.5440  0.0900  1 
BUSHING  3  3.4540  3.5060  3.4440  1 
6  BUSHING  4  1.7500  1.7700  1.8040  0.0680  1 
BUSHING  5  1.7360  1.7480  1.7020  X 


YOU CAN REPAIR THE WORN PART. REFER TO THE OVERHAUL MANUAL FOR THE REPAIR INFORMATION.
DISTANCE BETWEEN THE HEAD AND THE NUT (BOLT GRIP LENGTH).
____ TIGHTEN THE NUT ON THE BOLT BEFORE YOU MEASURE THE DISTANCE. YOU CAN TURN THE NUT BACK

NOTE:

A MAXIMUM OF 1/6 TURN TO GET THE CORRECT DIMENSION.
WIDTH OVER THE BRAKE TORQUE ARM BUSHINGS.
WIDTH BETWEEN THE FLANGES OF THE BRAKE TORQUE ARM BUSHINGS.
WIDTH OVER THE FLANGES OF THE BRAKE ROD BUSHINGS.
THE MAXIMUM DIMENSION CAN BE MORE THAN THE LIMITS SHOWN IF THE MAXIMUM CLEARANCE IS SATISFACTORY.
Wear Limits for the Landing Gear Brake Unit
Figure 602 (Sheet 2)

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 32-41-15
 ALL  ú ú 01 Page 609 ú Oct 10/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 HYDRAULIC BRAKE DISCONNECT - REMOVAL/INSTALLATION
_________________________________________________
 1.  General_______
 A.  This procedure contains these tasks:
 (1)  
The removal of the hydraulic brake disconnect assembly.

 (2)  
The installation of the hydraulic brake disconnect assembly.
 
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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(104)