• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 16:51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.  Use the procedures in paragraphs 2 and 3 to replace the aft parts of control cables A and B.
 TASK 32-31-41-024-002
 2.  Landing Gear Control Cable Removal (Fig. 401)__________________________________
 A.  References
 (1)  
25-22-00/201, Passenger Seats

 (2)  
29-15-00/201, Hydraulic Systems A, B, and Standby

 (3)  
32-00-01/201, Ground Lock Assemblies

 B.  
Access

 (1)  
Location Zone
 108 Aft Half of Cabin
 202 Lower Nose Compartment


 (2)  
Access Panels
 1103 Forward Access Door


 C.  
Removal


 S 494-001
 (1)  
Install the ground lock assemblies in the nose and main landing gear (Ref 32-00-01/201).

 (2)
Release the hydraulic pressure from system A (Ref 29-15-00/201).

 (3)  
Remove the passenger seats (Ref 25-22-00/201).

 S 014-015

 (4)  
Remove the left inboard panel on the floor which is between stations 663 and 685.


 S 864-003
 S 014-004
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-41
 ALL  ú ú 02 Page 401 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 034-005
 (5)  Disconnect the turnbuckles.
 NOTE: You can find the turnbuckles behind access door 1103.
____ Access door 1103 is forward of the nose wheel well.
 S 034-006
 (6)  
Remove the cotter pins which hold the cables and remove the cables from the control quadrant assembly.

 S 494-007

 (7)  
Attach cords to the cable terminals to help install the new cables.

 S 024-008

 (8)  
Pull the cables off the pulleys and floor beams.


 NOTE: Do not pull the cords out fully.
____
 TASK 32-31-41-424-009
 3. Landing Gear Control Cable Installation (Fig. 401)
_______________________________________
 A. References
 (1)  
25-22-00/201, Passenger Seats

 (2)  
32-31-00/501, Landing Gear Control System

 B.
Access

 (1)  
Location Zone
 108 Aft Half of Cabin
 202 Lower Nose Compartment


 (2)  
Access Panels
 1103 Forward Access Door


 C.
Installation

 (1)
Put the new cables through the floor beams and on the pulleys.


 S 834-010
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-41
 ALL  ú ú 02 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE  A 
CABLE D (LGVB) 
CABLE A (LGVA) 
CABLE C (LGVA) 
CABLE B (LGVB) 
ANTISKID SWITCH  TURNBUCKLES 
(ON LGVA) 
COTTER PIN  CONTROL 
QUADRANT 
ASSEMBLY 
WHEEL WELL CEILING  CONTROL CABLE 

SELECTOR VALVE
INBD
FWD
A
Landing Gear Control Cable Installation Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-41
 ALL  ú ú 02 Page 403 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
1C2  3


1 A B D


CABLE REF  FUNCTION VA-UP VB-DN  NO. REQ  LENGTH (INCHES) L1 L2  CABLE SIZE  FITTINGS 
1  2  3 
A1  LGVA  1  556.1  1/8 7 x 19  MS21260L4RH  BACT14A4 
B1  LGVB  1  568.8  1/8 7 x 19  MS21260L4RH  BACT14A4 
A2  LGVA  1  628.1  1/8 7 x 19  MS21260L4RH  BACT14A4 
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 2(54)