(3)
Open the access panels on the vertical fin (Ref 12-31-51/201).

 S 024-005

 (4)  
Remove the rudder position sensor:

 (a)  
Disconnect the electrical connector from the rudder position transmitter.

 (b)  
Loosen the screws on the support bracket and crank.

 (c)  
Remove the rudder position transmitter from the airplane.

 S 014-004
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-41
 ú ú 13 Page 401 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE  A  MOUNTING BRACKET 
RUDDER POSITION TRANSMITTER (T469) 

10.59 INCHES(NOMINAL)
A B
THUMBNUT
A  ADJUSTABLE
CONTROL ROD
B
CLAMPING SCREWS
CRANK
FWD
A
TRANSMITTER
SUPPORT BRACKET

CRANKCLAMPING CENTERLINESCREW CRANK
E
Z
TRANSMITTER SUPPORT BRACKET ADJUSTABLE CONTROL ROD
TRANSMITTER  ALIGN EZ MARK ON TRANSMITTER BODY WITH INDEX MARK ON
CLAMPING
SUPPORT BRACKET.
SCREW
ALIGN ZERO REFERENCE INDEX MARK ON
A-A
TRANSMITTER SHAFT WITH
TRANSMITTER  CENTERLINE OF CRANK.
SHAFT
TRANSMITTER
B-B
Rudder Position Transmitter Installation
Figure 401

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-41
 ú ú 12 Page 402 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 31-24-41-404-006
 3.  Rudder Position Transmitter Installation (Fig. 401)________________________________________
 A. Access
 (1)  
Location Zone
 706 Vertical Stabilizer
 708 Rudder

 (2)  
Access Panel
 9507 Access Panel, LH
 9509 Access Panel, LH
 9508 Access Panel, RH
 9511 Access Panel, RH

 B. Procedure
 S 424-007
 (1)  Install the rudder position transmitter:
 (a)  
Make sure the adjustable control rod is set to 10.59 inches.

 (b)  
Install the rudder position transmitter in the support bracket and crank.

 (c)  
Align the rudder position transmitter in the support bracket as shown in views A-A and B-B.

 (d)  
Tighten the screws.

 (e)  
Install the electrical connector on the rudder position transmitter.

 C. Put the Airplane Back to Its Usual Condition
 S 864-025
 (1)  
Do this task: "Rudder Hydraulic System A and B Depressurization (Ref 27-21-00/201).

 (2)  
Close the access panels.

 (3)  
Do this task: Rudder Position Transmitter Test (AMM 31-24-41/501).

 S 014-026
 S 734-029
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-41
 ú ú 13 Page 403 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 RUDDER POSITION TRANSMITTER - ADJUSTMENT/TEST
_________________________________________________
 1.  General_______
 A.  This procedure has one task. The task is a test of the rudder position transmitter.
 TASK 31-24-41-705-065
 2.  Rudder Position Transmitter Adjustment Test____________________________________________
 A.  Special Tools and Equipment
 (1)  
One of these portable testers which can select SUBFRAMES and WORDS to show the data for the flight data recorder. The Teledyne tester 2222786 or the AlliedSignal tester 981-6301-002 can be used on airplanes installed with FDR that records up to ]4 wps. Use the Teledyne tester 2229738-1 on airplanes installed with FDRs that record up to 128 wps. Use the Teledyne tester 2229738-1 Mod E on airplanes installed with FRD that records up to 256 wps.
　
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