• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-12 10:20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)  
32-11-19/401, Wing Gear Trunnion Fork

 (2)  
IPC 32-11-03 Fig. 1, IPC 32-11-19 Fig. 1

 B.  
Access

 (1)  
Location Zone
 735 Wing Landing Gear, LH
 745 Wing Landing Gear, RH


 C.  
Procedure


 S 026-002
 (1)  
Remove the trunnion fork and the bolt assemblies of the trunnion fork (Ref 32-11-19/401).

 S 226-003

 (2)  
Do a check on the wear limits of the housing of the trunnion fork bearing, the bushings and the bolts.

 (a)  
Measure the parts as it is necessary and compare the measured dimensions to the limit dimensions.

 (b)  
If the part is not in tolerance, repair or replace as it is necessary.


 S 426-004
 (3)  Install the trunnion fork and the bearing and connect the trunnion fork to the wing gear trunnion (Ref 32-11-19/401).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-19
 ALL  ú ú 01 Page 601 ú Oct 10/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


FOR DRAG BRACE-TO-TRUNNION FORK INSPECTION/CHECK REFER TO 32-11-03/601
Wing Gear Trunnion Fork Wear LimitsFigure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-19
 ALL  ú ú 01 Page 602 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

3. RACE/BALL

A-A

Wing Gear Trunnion Fork Wear Limits
Figure 601 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-19
 ALL  ú ú 01 Page 603 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE PART WORN  REPAIR WORN PART  REPAIR INSTR. 
DIAMETER  MITTED PER-WEAR DIM. 16  ANCE DIAM CLEAR-MAX 
MIN  MAX 
1  HOUSING  ID  6.9998  7.0016  7.0043  0.0083  X  1 
RACE  OD  6.9960  6.9980  6.9933  X 
2  HOUSING  2  2.77  2.79  4  X 
RACE  3  2.80  2.83  X  5 
3  RACE  ID  6.2500  6.2520  6.2570  0.0090  X 
BALL  OD  6.2480  6.2490  6.2430  X  5 
4  BUSHING  ID  2.2500  2.2510  2.2570  0.0080  X 
BOLT  OD  2.2480  2.2490  2.2450  X  5 
5  BUSHING  ID  2.2500  2.2515  2.2555  0.0065  X 
BOLT  OD  2.2480  2.2490  2.2450  X  5 
6  BOLT  6  3.143  3.148  3.184  0.044  X  8 
BUSHING  7  3.126  3.140  3.104  11 
7  BUSHING  9  1.255  1.264  1.284  0.036  11 
BUSHING  10  1.246  1.248  1.228  11 
8  BUSHING  12  7.375  7.379  7.404  0.032  11 
BUSHING  13  7.363  7.372  7.347  11 
9  BUSHING  14  9.878  9.886  9.905  0.038  X  11 
BUSHING  15  9.867  9.875  9.848  X  11 

Wing Gear Trunnion Fork Wear Limits
Figure 601 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-11-19
 ALL  ú ú 01 Page 604 ú Jun 10/90
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 起落架 LANDING GEAR 2(35)