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时间:2011-04-02 16:51来源:蓝天飞行翻译 作者:航空
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SEE A
CONNECTOR ELECTRICAL 
ASSEMBLY LEVER CONTROL 
LEVER CONTROL OVERRIDE TRIGGER LOCK 
LOCK SLUG SOLENOID COIL  LEADS ELECTRICAL 
(2 LOCATIONS) SCREW  SCREWS  FWD 
ASSEMBLY BASEPLATE 

Figure 401 Landing Gear Control Lever Lock Solenoid Installation 

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 32-31-31
 ALL  ú ú 01 Page 402 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 034-010
 (8)
Disconnect the electrical leads from the lock solenoid coil.

 S 034-011

 (9)  
Remove the screws for the lock solenoid coil.

 S 034-029

 (10)
 Remove the slug from the lock solenoid coil.


 TASK 32-31-31-424-034
 3.  Lock Solenoid Installation (Fig. 401)__________________________
 A. Access
 (1)  
Location Zone
 101,102 Control Cabin


 B.
Installation


 S 434-013
 (1)  
Put the lock solenoid coil around the slug and install the screws.

 S 434-014

 (2)  
Connect the electrical leads to the lock solenoid coil.

 S 434-015

 (3)  
Put the baseplate assembly in the correct position and connect the electrical connector to the baseplate assembly.

 S 434-017

 (4)  
Install the screws for the baseplate assembly.

 (5)  
Connect external electrical power to the airplane.

 S 864-035

 (6)
Remove the DO-NOT-CLOSE tags and close these circuit breakers:

 (a)  
P6 Main Power Distribution Panel
 1) LEVER LATCH & PRESS WARN

 

 S 864-019
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 32-31-31
 ALL  ú ú 03 Page 403 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 864-020
 (7)  Release the pressure from the hydraulic system.
 S 714-021
 (8)  Try to move the control lever for the landing gear to UP.
 NOTE:____ Make sure you cannot move the control lever to UP.

 S 714-022
 (9)  
Pull the lock override trigger and make sure you can move the control lever for the landing gear to UP.

 S 864-031

 (10)
 Move the control lever for the landing gear to OFF.

 S 034-023

 (11)
 Disconnect the teleflex cable on the torsion link of the right main landing gear.

 S 864-024

 (12)
 Move the actuator of the air safety sensor for the landing gear in front of the sensor.


 NOTE: This energizes the air safety sensor.
____
 S 714-025
 (13)
 Make sure you can move the control lever for the landing gear to all three positions.

 S 864-032

 (14)
 Move the control lever for the landing gear to DN.

 S 414-026

 (15)
 Close and lock the P2 and P3 panels.

 S 434-027

 (16)
 Connect the teleflex cable to the torsion link of the right main landing gear.


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 32-31-31
 ALL  ú ú 01 Page 404 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 LANDING GEAR CONTROL CABLES - REMOVAL/INSTALLATION
__________________________________________________
 1.  General_______
 A.  You must remove the control lever assembly to remove the forward parts of the control cables. You must remove the antiskid switch cam from cable C before you can remove the cables (Ref 32-31-11/401).
 
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本文链接地址:737-300 400 500 AMM 飞机维护手册 起落架 LANDING GEAR 2(53)