31-24-31
 ú ú 11 Page 401 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SEE

TRANSMITTER SHAFT

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-31
 ú ú 10 Page 402 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 TASK 31-24-31-404-029
 3.  Aileron Position Transmitter Installation (Fig. 401)_________________________________________
 A. Access
 (1)  
Location Zone 306 Wing Trailing Edge, Aileron and Control Tab, LH 406 Wing Trailing Edge, Aileron and Control Tab, RH

 (2)  
Access Panel
 7218 Access Panel, LH
 7418 Access Panel, RH

 B. Procedure
 S 424-030
 (1)  Install the aileron position transmitter:
 (a)  
Make sure that the adjustable control rod is set at 13.35 inches.

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

 (c)  
Align the EZ marks on the transmitter body and the index mark on the transmitter shaft with the centerline of the crank.

 (d)  
Tighten the screws.

 (e)  
Install the electrical connector on the transmitter.

 C. Put the Airplane Back to Its Usual Condition
 S 864-046
 (1)  
Do this task: "Aileron Hydraulic Systems A and B Depressurization" (Ref 27-11-00/201).

 (2)  
Close the access panel.

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

 S 414-047
 S 734-050
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú

 31-24-31
 ú ú 11 Page 403 ú Mar 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AILERON POSITION SENSOR - ADJUSTMENT/TEST
_________________________________________
 1.  General_______
 A.  This procedure has one task. The task is a test of the aileron position transmitter.
 TASK 31-24-31-705-045
 2.  Aileron Position Sensor Adjustment Test________________________________________
 A.  Special Tools and Equipment
 (1)  
Use one of these portable testers to select SUBFRAMES and WORDS to show the data for the flight data recorder. The Teledyne tester 2222786 or the Allied Signal tester 980-6301-002 can be used on airplanes installed with a flight data recorder (FDR) that records up to 64 wps. Use the Teledyne tester 2229738-1 on airplanes installed with FDRs that record up to 128 wps. Use the Teledyne tester 2229838-1 Mod E on airplanes installed with FDRs that record up to 256 wps.

 (a)  
Flight Line Tester, Teledyne P/N 2222786, 2229738-1, or 2229738-1 Mod E Data rate: 256 wps Teledyne Controls, 12333 W. Olympic Blvd., West Los Angeles, CA 90064

 (b)  
Digital Signal Display unit, Allied Signal P/N 981-6301-002, Allied Signal Aviation Division, PO Box 7002 4747 Harrison Ave. Rockford, IL 61101

 (2)
Adapter Cable - Tester, Flight Data Recorder System P/N A31007

 NOTE: The tester cable consists of a cable assembly that is
____ approximately 60 inches long with a connector and a dust cap on each end. Use the -2 cable of the -1 kit when using the Teledyne testers 2222786. Use the -32 cable of the -30 kit (on airplanes with FDEP) or -35 cable of the -49 kit (on airplanes without FDEP) when using the Allied Signal tester 981-6301-002. Use the -60 cable of the -59 kit when using the Teledyne tester 2229738-X.
 B.  References
 (1)  
AMM 27-11-00/201, Aileron and Aileron Trim Control System

 (2)  
AMM 31-24-31/401, Aileron Position Transmitter

 C.  Access
 (1)  Location Zone
 101 Control Cabin - LH
 102 Control Cabin - RH

 D.  Prepare to Test
 S 865-002
 (1)  Supply electrical power (AMM 24-22-00/201).
　
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