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 (4)  S 865-125Make sure the mach trim actuator is in the null position (AMM 27-31-00/201).
 (5)  S 865-126Make sure the hydraulic systems A and B are on (AMM 29-00-00/201).
 (6)  S 735-367Do this test of the position signals from the elevator: (a) Set the portable tester to the SUBFRAMES and WORDS shown in the table. (b) Put the elevators in the positions shown in the table. (c) Make sure the portable tester displays agree with the values in the table.
 ~............................................................. | WORD | S/F | ELEVATOR | POSITION (INCHES) | TESTER DISPLAY | ............................................................... | 5  |  0  | LEFT | AT INDEX MARK | 7733 to 0044 | | | | | 10.00 ABOVE INDEX | 7224 to 7332 | | | | | 10.00 BELOW INDEX | 0502 to 0626 | ............................................................... |  37  |  0  | RIGHT | AT INDEX MARK | 7734 to 0045 | | | | | 10.00 ABOVE INDEX | 0446 to 0554 | | | | | 10.00 BELOW INDEX | 7152 to 7276 | 2......….....…..........…....................…................1
 (7)  S 825-129Adjust the elevator position sensors if it is necessary (AMM 31-24-51/401).
 (8)  S 865-704Remove the hydraulic power if it is not necessary (AMM 29-00-00/201).
 (9)  S 865-131If you will do no more tests, then do this task: "Put the Airplane to its Usual Condition."

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 BEJ 101-112, 114-999; ú 31-24-02
 ú ú 12 Page 521 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 TASK 31-24-02-735-473
 12. Rudder Pedal Position Signals Test__________________________________
 A. References
 (1)  AMM 27-21-00/501, Rudder and Rudder Trim Control System
 B. Access
 (1)  Location Zones
 101 Control Cabin - Left
 102 Control Cabin - Right

 C. Procedure
 S 865-720
 (1)
Make sure you did the Prepare For Input Parameter Test task.

 S 735-188

 (2)
Do this test of the position signals from the rudder pedals:

 (a)  
Set the portable tester to SUBFRAME 0, WORD 49.

 (b)  
Use the rudder pedal crank to move the captain's rudder pedal to the zero position.

 (c)  
Install a rig pin in the captain's rudder pedal.

 (d)  
Make sure the portable tester display is 7764 to 0013 (nominal 0000).

 (e)  
Remove the rig pin from the captain's rudder pedal.

 (f)  
Move the rudder pedals smoothly to the positions shown in the table.

 (g)  
Make sure the portable tester display agrees with the values in the table.

 

 ~..................................................... | RUDDER PEDAL POSITION | PORTABLE TESTER DISPLAY | ....................................................... |Captain's right rudder | 1354 to 2014 (nominal 1574) | |pedal fully forward | | |against the stop | | ....................................................... |Captain's left rudder | 5763 to 6423 (nominal 6203) | |pedal fully forward | | |against the stop | | 2.......................….............................1
 S 865-721
 (3)  If you will do no more tests, then do this task:
 "Put the Airplane to its Usual Condition."

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 BEJ 101-112, 114-999; ú  31-24-02
 ú ú 13 Page 522 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 TASK 31-24-02-735-141
 13. Rudder Position Signals Test____________________________
 A. References
 (1)  
AMM 27-21-00/201, Rudder and Rudder Trim Control System

 (2)  
AMM 31-24-41/401, Rudder Position Transmitter

 B. Access
 (1)  Location Zones
 101 Control Cabin - Left
 102 Control Cabin - Right

 C. Procedure
 S 865-142
 (1) Make sure you did the Prepare For Input Parameter Test task.
 S 865-143
　
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