• 热门标签

当前位置: 主页 > 航空资料 > 机务资料 >

时间:2011-04-02 16:53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


 TASK 32-51-81-004-001
 2.  Rudder Pedal Steering Actuator Removal (Fig. 401)______________________________________
 A. Standard Tools and Equipment
 (1)
Rigging Pin - MS20392, 5/16-inch diameter (2 is necessary)

 B.
References

 (1)  
32-00-01/201, Ground Lock Assemblies

 C.
Procedure


 S 494-002
 (1)  
Install the ground locks in the nose landing gear
 (Ref 32-00-01/201).


 S 014-003

 (2)  
Open the steering circuit breaker of the nose landing gear (C1027) on the P6 panel.

 S 494-004

 (3)
Install the rigging pin in the cable drum and the cable quadrant.

 S 014-005

 (4)  
Remove the forward access panel from the left bulkhead of the nose wheel well.


 NOTE: The removal of this panel will access you to the turnbuckles
____ of NGPPA and NGPPB cables. You can also access to the rotary actuator of the rudder pedal steering.
 S 034-006
 (5)  
Loosen the position cables (NGPPA and NGPPB) at their turnbuckles.

 S 034-007

 (6)  
Disconnect the position cables NGPPA and NGPPB on the nose landing gear from the rotary actuator pulley.

 (a)  
Remove the cotter pins at the ends of the cable terminals on each side of the rotary actuator pulley.

 (7)
Disconnect the electrical connection at the rotary actuator.

 (8)  
Remove the four mounting bolts from the rotary actuator.


 S 034-008
 S 034-009
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-81
 ALL  ú ú 01 Page 401 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.

737-300/400/500MAINTENANCE MANUAL 
SEE  A 
NGPPA 
NGPPB 
NGPPB 
STEERING 
WHEEL 
ROTARY 
ACTUATOR 
PULLEY 
ROTARY 
ACTUATOR 
FWD 
NGPPA 
MOUNTING BOLT 
NGPPB  (TYP 4)  1  CAUTION:_______ 


ROTARY ACTUATOR 
SEE  B 
CABLE 
NGPPA 
QUADRANT 
RIG 
PULLEY  PIN HOLE 
SEE  C 
CABLE 
NGPPB 
CABLE DRUM 

Rudder Pedal Steering Rotary Actuator 
Figure 401 

NGPPA
NGPPA CABLE TERMINAL 1
NGPPB CABLE TERMINAL 1
ENDS OF COTTER PIN MUST NOT CONTACT HOUSING OF ACTUATOR AFTER INSTALLATION.
FWD
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 32-51-81
 ALL  ú ú 01 Page 402 ú Oct 25/85
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 024-010
 (9)  Remove the rotary actuator.
 TASK 32-51-81-404-011
 3. Rudder Pedal Steering Actuator Installation (Fig. 401)
___________________________________________
 A. References
 (1)  
32-51-00/501, Nose Wheel Steering System

 B.
Procedure


 S 434-012
 (1)  
Put the rotary actuator on the support bracket and install the four mounting bolts.

 S 434-013

 (2)  
Connect the electrical supply to the actuator.


 S 434-019
 CAUTION: MAKE SURE THE ENDS OF THE COTTER PINS WILL NOT TOUCH THE
_______ HOUSING OF THE ACTUATOR AFTER YOU INSTALL. IF YOU INSTALL THE
 PINS INCORRECTLY, A POSSIBLE DAMAGE TO THE EQUIPMENT CAN OCCUR.
 (3)  
Connect the position cables NGPPA and NGPPB to the rotary actuator pulley.

 S 824-015

 (4)  
Adjust the position cables (Ref 32-51-00/501).

 (5)
Remove the rigging pins from the cable drum and the quadrant.

 S 414-017

 (6)  
Install the forward access panel to the leftside of the wheel well bulkhead on the nose landing gear.


 
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 3(145)