(a)
Make sure the force is not more than 12 pounds.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-00
 ALL  ú ú 01 Page 503 ú Mar 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-021
 (7) Put the control handle to the DN position.
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-00
 ALL  ú ú 01 Page 504 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LANDING GEAR CONTROL LEVER ASSEMBLY - REMOVAL/INSTALLATION
__________________________________________________________
 TASK 32-31-11-024-001
 1.  Remove the Control Lever Assembly for the Landing Gear (Fig. 401)______________________________________________________
 A. References
 (1)  
AMM 32-00-01/201, Ground Lock Assemblies

 B.
Access

 (1)  
Access Panel
 1103 Forward Access Door

 C.
Remove the Control Lever Assembly for the Landing gear

 S 864-002
 (1)  
Install the ground lock assemblies for the landing gear (AMM 32-00-01).

 S 864-003

 (2)  
Remove the pressure from the hydraulic system.

 S 034-004

 (3)  
Disconnect the turnbuckles on control cables for the landing gear.

 S 034-005

 (4)
Remove the antiskid switch cam from the landing gear up cable.

 NOTE: This is forward of the turnbuckles.
____
 S 864-006
 (5)  Attach ropes to the cable terminals.
 NOTE: This will make the replacement of the cables easier.
____
 S 014-007
 (6)  
Remove the right part of the P9 panel that is below the control lever.

 (7)  
Release and lower the P2 and the P3 panels.

 (8)  
Remove the screws that attach the base plate assembly.

 (9)  
Disconnect the electrical connector for the base plate assembly.

 S 014-008
 S 034-009
 S 034-010
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-11
 ALL  ú ú 01 Page 401 ú Mar 15/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TURNBUCKLES
CABLE D
(LGVB)
CABLE C (LGVA)
ANTISKID SWITCH (ON LGVA)
A 737-300/400/500MAINTENANCE MANUAL
SPRING PINS (TYPICAL)
FWD
LANDING GEAR
CONTROL CABLE
ANTISKID SWITCH CAM INSTALLATION
SCREW
WIRE BUNDLE 
CLAMP 
FWD 
MOUNTING 
BASEPLATE  SCREWS 
ASSEMBLY 
ELECTRICAL 
CONNECTOR 
SPACER  FWD 
MOUNTING 
SCREWS 

CONTROL
LEVER
ASSEMBLY
CONTROL CABLE TURNBUCKLE TERMINALS
CONTROL LEVER ASSEMBLY ELECTRICAL CONNECTOR
FWD
LOWER BASEPLATE MOUNTING ASSEMBLY SCREWS
Landing Gear Control Lever Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-31-11
 ALL  ú ú 01 Page 402 ú Feb 20/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 034-011
 (10)
 Remove the base plate assembly.

 S 034-012

 (11)
 Disconnect the electrical connector for the control lever assembly.

 S 034-013

 (12)
 Remove the lower attachment screws.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機維護手冊 起落架 LANDING GEAR 2(50)