(d)  
Remove the bolt, nut, and three washers which attach the electrical ground to the rudder aft quadrant.

 (e)  
Remove the nut, washer and bolt that attach the transmitter rod to the rudder aft quadrant.

 (f)  
Remove the nut, washer and bolt that attach the transmitter rod to the rudder feel and centering unit.

 (g)  
Remove the transmitter rod from the airplane.

 TASK 31-24-43-424-008
 3.  Rudder Pedal Force Transmitter Rod Installation (Fig. 401)_______________________________________________
 A. Standard Tools and Equipment
 (1)  F70207-107 Rig Pin Kit
 (a)  
Rig Pin R-3

 (b)  
Rig Pin R-4

 B. References
 (1)  AMM 27-21-00/201, Rudder and Rudder Trim Control System
 C. Access
 (1)  
Location Zone
 706 Vertical Fin

 (2)  
Access Panels
 9509L TE Access Panel
 9513L Access Door - Rudder
 9525L Access Door on Fin
 9530L Access Door on Fin

 D. Transmitter Rod Installation
 S 424-009
 (1)  Install the transmitter rod:
 (a)  
Put the transmitter rod in its position.

 (b)  
Install the bolt, washer and nut that attach the transmitter rod to the rudder feel and centering unit.

 (c)  
Install the bolt, washer and nut that attach the transmitter rod to the rudder aft quadrant.

 (d)  
Install the bolt, nut and three washers which attach the electrical ground to the rudder aft quadrant.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES POST-SB 31-3112;  ú 31-24-43
 AIRPLANES WITH RUDDER PEDAL FORCE  ú
 TRANSMITTER ROD INSTALLED  ú 01 Page 406 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (e) Connect the electrical connector to the transmitter rod.
 E. Put the Airplane Back to Its Usual Condition
 S 414-010
 (1)
Install access panel 1103.

 S 834-011

 (2)
Remove rigging pins R-3 and R-4 from the forward quadrants.

 S 414-012

 (3)
Install access panels 9509, 9525, 9530 and close access door 9513.

 S 444-013

 (4)
Do this task: Pressurize the hydraulic systems (AMM 27-21-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 AIRPLANES POST-SB 31-3112;  ú 31-24-43
 AIRPLANES WITH RUDDER PEDAL FORCE  ú
 TRANSMITTER ROD INSTALLED  ú 01 Page 407 ú Mar 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ELEVATOR POSITION TRANSMITTER - REMOVAL/INSTALLATION
____________________________________________________
 1.  General_______
 A.  This procedure has two tasks, one for the removal and one for the installation of the elevator position transmitter (which is referred to as the transmitter). The procedure has these parts:
 (1)  
The removal of the transmitter.

 (2)  
The installation of the transmitter.

 (3)  
An adjustment of the transmitter.

 B.  There is a transmitter on the left and right elevator. The procedure is the same for each transmitter.
 TASK 31-24-51-004-018
 2.  Elevator Position Transmitter Removal (Fig. 401)_____________________________________
 A.  References
 (1)  AMM 27-31-00/201, Elevator and Tab Control System
 B.  Access
 (1)  
Location Zone
 711, 712 Elevator and Tab

 (2)  
Access Panels
 3801/3802 Tail Cone Access Door
 9105/9205 Access Panel Trailing Edge

 C.  Procedure
 S 864-019
 (1)  
Remove the hydraulic power (AMM 27-31-00/201).

 S 864-020

 (2)
Open this circuit breaker and attach a DO-NOT-CLOSE tags:
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：737-300 400 500 AMM 飛機(jī)維護(hù)手冊(cè) 儀表 INSTRUMENTS(107)