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 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF ALL CONTROL
_______ SURFACES BEFORE YOU SUPPLY HYDRAULIC POWER. AILERONS, RUDDERS, ELEVATORS, FLAPS, SPOILERS, LANDING GEAR, AND THRUST REVERSERS CAN MOVE QUICKLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
 (2)  
Make sure the rudder control system is serviceable (AMM 27-21-00/201).

 S 735-369

 (3)  
Do this test of the position signals from the rudder:

 (a)  
Set the portable tester to the SUBFRAMEs and WORDs shown in the table.

 (b)  
Set the rudder to the applicable condition.

 (c)  
Make sure the portable tester displays agree with the values in the table.

 

 ~........................................................ | WORD | S/F | RUDDER | POSITION | TESTER DISPLAY | .......................................................... |  17  |  0  | | Rudder at index | 7745 to 0034 | | | | | mark | | | | | | 16" left of | 7274 to 7365 | | | | | index mark | | | | | | 16" right of | 0421 to 0511 | | | | | index mark | | 2......….....…........….................…................1
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 BEJ 101-112, 114-999; ú  31-24-02
 ú ú 11 Page 523 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 825-147
 (4)  
Adjust the rudder position sensor if it is necessary (AMM 31-24-41/401).

 S 865-148

 (5)  
Remove the power from the rudder control system if it is not necessary (AMM 27-21-00/201).

 S 865-149

 (6)  
If you will do no more tests, then do this task:
 "Put the Airplane to its Usual Condition."

 

 TASK 31-24-02-735-105
 14. Speed Brake Handle Position Signals Test________________________________________
 A. Reference
 (1)  AMM 27-62-00/501, Speed Brake Control System
 B. Access
 (1)  Location Zones
 101 Control Cabin - Left
 102 Control Cabin - Right

 C. Procedure
 S 865-107
 (1)
Make sure you did the Prepare For Input Parameter Test task.

 S 735-361

 (2)
Do this test of the position signals from the speed brake:

 (a)  
Set the portable tester to SUBFRAME 0, WORD 25.

 (b)  
Set the speed brake handle to the positions shown in the table (AMM 27-62-00/501).

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

 

 ~................................................................ | SPEED BRAKE | HANDLE ANGLE | PORTABLE TESTER DISPLAY | | HANDLE POSITION | (reference) | | .................................................................. | DOWN | 0° | 7763 to 0015 (nominal 0000) | .................................................................. | ARMED | 4.0° | 7723 to 7757 (nominal 7741) | .................................................................. | INFLIGHT | 40.5° | 7074 to 7127 (nominal 7112) | 2...................…..............….............................1
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
 BEJ 101-112, 114-999; ú  31-24-02
 ú ú 14 Page 524 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 865-110
 (3)  
Put the speed brake handle in its usual position.

 S 865-111

 (4)  
If you will do no more tests, then do this task:
 "Put the Airplane to its Usual Condition."

 

 TASK 31-24-02-735-112
 15. Stabilizer Position Signals Test________________________________
 A. References
 (1)  
AMM 27-41-00/501, Horizontal Stabilizer Trim Control System

 (2)  
AMM 29-00-00/201, Hydraulic Power

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