S 024-003
 (2)  Remove the FDAU (Ref 20-10-07/201).
 TASK 31-24-22-404-005Flight Data Acquisition Unit Installation
_________________________________________
 A.  References
 (1)  
AMM 20-10-07/201, Electrical and Electronic Black Box

(2)  
AMM 31-24-00/501, Flight Data Recorder System

 (3)  
AMM 31-24-01/501, Flight Data Recorder System

 (4)  
AMM 31-24-02/501, Flight Data Recorder System

 B.  Access
 (1)  Location Zone
 205 Electronics Compartment

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 31-24-22
 ú ú 10.1 Page 401 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 
737-300/400/500MAINTENANCE MANUAL
 C.  Procedure
 S 864-006
 (1) Make sure these circuit breakers are open:
 (a) P18 Panel
 1) FLIGHT RECORDER AC
 2) FLIGHT RECORDER DC
 S 424-007
 CAUTION: DO NOT TOUCH THE CONNECTOR PINS OR OTHER CONDUCTORS ON THE_______
 FDAU. IF YOU TOUCH THESE CONDUCTORS, ELECTROSTATIC DISCHARGE
 CAN CAUSE DAMAGE TO THE FDAU.
 (2) Install the FDAU (AMM 20-10-07/201).
 S 864-017
 (3) Close these circuit breakers:
 (a) P18 Panel
 1) FLIGHT RECORDER AC
 2) FLIGHT RECORDER DC
 S 744-023
 (4) Do the BITE test part of the Operation Test - Flight Data Recorder
 ú  System Task (AMM 31-24-00/501 or 31-24-01/501 or 31-24-02/501 or
 ú  31-24-03/501 or 31-24-04/501).
 ú  NOTE: Some of these references may not be applicable to your____
 ú  airplanes.
 ú

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. B-2535 AND ON ú

 31-24-22
 ú ú 09.1 Page 402 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 AILERON POSITION TRANSMITTER - REMOVAL/INSTALLATION
___________________________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the aileron position transmitter.
 TASK 31-24-31-004-024
 2.  Aileron Position Transmitter Removal (Fig. 401)____________________________________
 A.  References
 (1)  
27-11-00/201, Aileron and Aileron Trim Control System

 (2)  
12-31-61/201, Wing Lower Surface Access Doors and Panels

 B.  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

 C.  Remove the Aileron Position Transmitter
 S 864-025
 (1)  
Do this task: "Aileron Hydraulic Systems A and B Depressurization" (Ref 27-11-00/201).

 S 864-026

 (2)  
Open these circuit breakers and attach DO-NOT-CLOSE tags:

 (a)  P18-2 Circuit Breaker Panel 1) POSITION INDICATOR AND TRANSMITTER

 (3)  
Open the access panel on the lower wing surface (Ref 12-31-61/201).

 S 024-028

 (4)  
Remove the aileron position transmitter:

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

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

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

 S 014-027
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. BEJ 101-999 ú
　
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