• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-13 07:52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

B
A
1 FOR TORSION LINK INSPECTION/CHECK REFER TO 32-21-03/601
Nose Gear Steering Collar Wear Limits Figure 601 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-06
 ALL  ú ú 01 Page 602 ú Feb 10/89
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL


A-A
7. BUSHING/PIN 2. BUSHING/PIN

STEERING STEERING PIN COLLAR PIN CYLINDER ROD END RETAINER
STEERING COLLAR-FORWARD
B-B

Nose Gear Steering Collar Wear LimitsFigure 601 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-06
 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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  WEAR DIM. 7  DIAM CLEAR-ANCE MAX 
MIN  MAX 
1  BUSHING  ID  1.7500  1.7510  1.7545  0.0056  X  3 
PIN  OD  1.7480  1.7490  1.7455  X  X  1 
2  BUSHING  ID  1.7500  1.7510  1.7545  0.0056  X  2 
PIN  OD  1.7480  1.7490  1.7555  X  X  2 
3  BEARING  ID  1.7490  1.7500  1.7510  0.0056  X  4 
PIN  OD  1.7480  1.7490  1.7454  X  X  1 
4  BUSHING  ID  10.800  10.803  10.818  0.018 5  X 
STRUT  OD  10.797  10.800  10.785  X  X  6 
5  STRUT  8.580  8.586  8.593  0.018  X 
BUSHING  8.575  8.578  8.568  X  X  6 
6  BUSHING  7.675  7.678  7.669  0.026  X  X  6 
COLLAR  7.671  7.673  7.651  X  X  6 
7  BUSHING  ID  2.1250  2.1260  2.130  0.0059  X  2 
PIN  OD  2.1225  2.1235  2.120  X  X  1 
8  BUSHING  ID  2.1250  2.1260  2.130  0.0059  X  3 
PIN  OD  2.1225  2.1235  2.120  X  X  1 

Nose Gear Steering Collar Wear Limits
Figure 601 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-06
 ALL  ú ú 01 Page 604 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

WORN PART (OR ASSEMBLY) IS REPAIRABLE. REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION

PROCURE REPLACEMENT BUSHING. INSTALL BUSHING IN FORWARD COLLAR ASSEMBLY PER 20-11-01/401
PROCURE REPLACEMENT BUSHING. INSTALL BUSHING IN AFT COLLAR ASSEMBLY PER 20-11-01/401 INSTALL NEW ACTUATOR OR INSTALL NEW BEARING IN ACTUATOR ROD END PER 20-11-01/401INCLUDES CLEARANCE BETWEEN STEERING COLLAR AND BUSHING
INSTALL REPLACEMENT OR REPAIR PER OVERHAUL MANUAL LIMITS SHOWN MAY BE EXCEEDED PROVIDED MAXIMUM CLEARANCE IS NOT EXCEEDED
Nose Gear Steering Collar Wear Limits
Figure 601 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-06
 ALL  ú ú 01 Page 605 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 NOSE GEAR RUDDER PEDAL STEERING INTERCONNECT
___________________________________________ ACTUATOR - REMOVAL/INSTALLATION
_______________________________
 1.  General_______
 A.  This procedure removes and installs the nose gear rudder pedal steering interconnect actuator.
 
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 8(37)