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 2)  Hydraulic pump switch B
 3)  Flight control hydraulic switch A
 4)  Flight control hydraulic switch B.
 (b)  Open the forward access panel, 1103.
 (c)  Loosen the two sensor clamp screws.
 (d)  Hold the cable drum and turn the sensor until the mark on the
 shaft aligns with the mark on the sensor.
 NOTE:____ No special position of the aligned marks is necessary.
 (e)  Turn the sensor to get a display of 0000.
 (f)  Tighten the clamp screws to 30-35 pound-inches.
 S 865-020

 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.
 (6)  
Supply pressure to hydraulic systems A and B (Ref 29-15-00/201).

 S 865-021

 (7)  
Move the rudder pedals smoothly to the positions shown in the table (Ref 27-21-00/201).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. B-2535 AND ON ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 S 215-022
 (8)  For each position, 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
 F. Put the Airplane in its Usual Condition
 S 865-023
 (1)  
Put the TEST--NORMAL switch to the NORMAL position.

 S 865-024

 (2)
Put the POWER switch on the portable tester to the OFF position.

 S 085-025

 (3)  
Disconnect the portable tester from the flight data recorder system.

 S 415-027

 (4)  
Close the forward access door, 1103.

 S 865-028

 (5)  
Remove the hydraulic power (Ref 29-15-00/201).

 S 865-029

 (6)  
Remove the electrical power if it is not necessary
 (Ref 24-22-00/201).

 

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. B-2535 AND ON ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 RUDDER PEDAL FORCE TRANSMITTER ROD - REMOVAL/INSTALLATION
_________________________________________________________
 1.  General
_______
 A.  This procedure has two tasks:
 (1)  
Rudder Pedal Force Transmitter Rod Removal

 (2)  
Rudder Pedal Force Transmitter Rod Installation.

 B.  The rudder pedal force transmitter rod is referred to as the "transmitter rod" in this procedure.
 TASK 31-24-43-014-001
 2.  Rudder Pedal Force Transmitter Rod Removal (Fig. 401)
__________________________________________
 A.  References
 (1)  AMM 27-21-00/201, Rudder and Rudder Trim Control System
 B.  Standard Tools and Equipment
 (1)  
F70207-107 Rig Pin Kit

 (2)  
Rig Pin R-3

 (3)  
Rig Pin R-4

 C.  Access
 (1)  
Location Zone
 706 Vertical Fin

 (2)  
Access Panels
 9509L TE Access Panel
 9513L Access Door - Rudder
 9525L Access Door on Fin
 9530L Access Door on Fin

 

 D.  Prepare for Removal
 S 044-002
 (1)  
Do this task: Remove pressure from the rudder hydraulic system (AMM 27-21-00/201).
　
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