S 495-029

 (13)
 Install the rigging pins 1 thru 4.

 S 835-030

 (14)
 Adjust the tension of all the segments of cables NWSA and NWSB (per Table I) until the rigging pins 1 thru 4 will install correctly.

 S 435-031

 (15)
 If you remove the lock clips, install the clips to lock the turnbuckles of the cables NWSA and NWSB.

 S 825-083
 CAUTION: MAKE SURE THE END OF THE ROD WILL COVER AT LEAST ONE HALF OF
_______ INSPECTION HOLE IN THE CONTROL ROD ASSEMBLY. A MINIMUM OF THREE THREADS MUST BE OPEN OUTSIDE THE LOCKNUT ON THE CONTROL ROD AT THE CRANK END. AN INTERFERENCE AND A POSSIBLE ROD FAILURE CAN OCCUR.
 (16)
 If the steering control rod of the rudder pedal is disconnected, do the steps that follow:

 (a)  
Adjust the steering control rod of the rudder pedal.

 (b)  
Make sure the attach bolt will install correctly through the control rod and the input rod.

 (c)  
Install the attach bolt.

 (17)
 Remove all the rigging pins.

 S 095-033
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 705-081
 (18)
 Make sure that the position to center the nose landing gear is zero (with the possibilities given on the shock strut of the nose landing gear).

 (a)  
If it is necessary, adjust the input rod of the steering metering valve.

 NOTE: The shoulder bolt must install correctly without the
____ movement of the metering valve (spring loaded) from its neutral position.
 S 735-034
 (19) Do a test on the steering system of the nose wheel (refer to paragraph 2).
 TASK 32-51-00-705-061
 4. Nose Wheel Steering System Test
________________________________
 A. General
 (1)  
You do a test on the steering system of the nose wheel to find if the steering rate, the steering wheel centering, and the angle of travel are in the necessary limits and the system is free of malfunctions and leaks. You must adjust the steering systems of the nose wheel and the rudder control system before you do the tests.

 (2)  
Service the hydraulic system before you do the test
 (AMM 12-12-00/301).

 NOTE: If it is necessary to adjust or replace the proximity sensor
____ of the nose wheel or the target refer to AMM 32-09-02.
 (3)  
You must adjust the steering system of the nose wheel well correctly before you do the test.

 (4)  
It is important that you bleed the hydraulic system of the nose gear steering completely everytime you open it for servicing. You do this task is to make sure of an effective shimmy damping. To bleed the system you must pressurize the hydraulic system A (AMM 29-15-00/201) and try the steering system through at least 15 complete cycles from full left to full right without the torsion link apex pin.

 B.
Special Tools and Equipment

 (1)  
Spring Scale - calibrated from 0 to 25 pounds

 (2)  
3TE65-73762, Jacking Adapter

 C.
Standard Tools and Equipment

 (1)  
Stop Watch

 (2)  
Greased turning plates to allow nose wheels to steer

 D.
References

 (1)  
AMM 07-11-21/201, Jack Airplane

 (2)  
AMM 29-15-00/201, Hydraulic Systems A and B

 (3)  
AMM 32-00-01/201, Ground Lock Assemblies

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
 E. Prepare to Test the Steering System of the Nose Wheel
 S 495-035
 (1)  
Install the ground locks in the nose landing gear
 (AMM 32-00-01/201).

 S 865-036

 (2)  
Remove the pressure from the hydraulic system A (AMM 29-15-00/201).
　
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