曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

 (1) Install the ground locks in all landing gear (AMM 09-11-00/201).
 S 842-040
 WARNING: YOU MUST CAREFULLY DO THE TASK 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: "The Installation of the Door Locks on the Wing Landing Gear" (AMM 32-00-30/201).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-09
 ALL  ú ú 01 Page 201 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 S 842-036
 (3)  
Do this task: "The Installation of the Door Locks on the Body Landing Gear" (AMM 32-00-30/201).

 S 842-044

 (4)  
Lift the airplane on jacks until the wheels are off the ground (AMM 07-11-01/201).

 S 842-006

 (5)  
Decrease the pressure on the hydraulic system No. 1
 (AMM 29-11-00/201).

 

 S 492-007
 WARNING: YOU MUST HOLD THE BUNGEE WITH SPRING BEFORE YOU REMOVE THE
_______ PINS. THIS CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
 (6)  
Install the bungee restraining tool.

 E.
Remove the Jury Strut Spindle (Fig. 201)

 S 032-008
 (1)  
Remove the conduit from the upper jury strut and the support structure.

 S 032-009

 (2)  
Remove the cotter pin and loosen the spindle nut (8).

 S 032-010

 (3)  
Remove the ground lock.

 S 032-011

 (4)  
Remove the spindle bolt (1), the upper conduit bracket (2), the washers, the end caps (4) and the pin (3).

 (5)  
Pull the jury strut back from the spindle (6).

 S 032-045

 (6)  
Tighten the bungee clamp until you get sufficient clearance to remove the spindle.

 S 032-012
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-09
 ALL  ú ú 01 Page 202 ú Oct 18/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

SEE  A 
A 
A 
1.  SPINDLE 
BOLT 
FWD 
STRUCTURE 
8.  SPINDLE  CONDUIT 
NUT  BRACKET 
7.  SPLINED 
WASHER 
6.  SPINDLE 
CONDUIT2. 
JURY  BRACKET 
STRUT 
FWD 
3.  PIN 
4.  END CAP 
(2 LOCATIONS) 
5.  NUT 
A 
Body Gear Jury Strut Spindle Installation 
Figure 201 (Sheet 1) 

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-13-09
 ALL  ú ú 01 Page 203 ú Feb 10/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL

10. BUSHING/SPINDLE
A-A
NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  WORN PART REPLACE  PART WORN REPAIR  INSTR. REPAIR 
DIAMETER  WEAR MITTED PER-DIM. 3  ANCE MAX CLEAR-DIAM 
MIN  MAX 
9  BUSHING  ID  1.8760  1.8770  1.8815  0.0077  X  2 
SPINDLE  OD  1.8720  1.8740  1.8690  X  1 
10  BUSHING  ID  2.1260  2.1270  2.1320  0.0080  X  2 
SPINDLE  OD  2.1220  2.1240  2.1190  X  1 
11  SHOULDER/WASHER  5.5100  5.5270  5.5400  0.0700  X  1 
BUSHINGS  5.4800  5.5100  5.4600  X  2 

 PART IS REPAIRABLE.  REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION. 
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 起落架 LANDING GEAR 3(17)