E = C +/- 20mV

 (b)
 If the value E is more than the value C plus or minus 20 mV, adjust the gearbox again and move the gearbox plate (11) counterclockwise to get :

 E = C +/- 20mV
 (12)
 Remove the SENSOR-VOLTAGE TEST (F26792000) or SENSOR - VOLTAGE TEST (2).

 (13)
 Install the RVDT 4GC (1) (Ref. TASK 32-51-19-400-001).

 (14)
 Connect the electrical connector (3) to the RVDT 4GC (1).

 Subtask 32-51-00-865-076
 F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3GG, 4GG, 2EN1, 2EN2
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 5. Close-up
________ Subtask 32-51-00-860-066
 A. Aircraft Maintenance Configuration
 (1)
 If the front of the aircraft is lifted off the ground, lower the aircraft to the ground (Ref. TASK 07-11-00-586-001).

 (2)
 If the nosewheels are on grease plates, move the aircraft to remove the grease plates (Ref. TASK 09-10-00-584-002).

 Subtask 32-51-00-740-052
 B. Bite Test
 (1) Do the Bite test of the BSCU (Ref. TASK 32-46-00-740-001). Subtask 32-51-00-942-059
 C. Remove the Equipment
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Remove the access platform(s).

 (3)
 Remove the warning notice(s).

 (4)
 Remove the ground support and maintenance equipment, the special and standard tools and all other items.

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 TASK 32-51-00-820-001-A
 Adjustment of the NWS "Zero" position for A/C with NWS Sensor Box (3GC,4GC) P/N E21336000, Rudder Trim Angle as Reference
 CAUTION : IF THE SENSOR BOX HAS P/N E21336000, NEVER REMOVE THE SENSOR FROM THE
_______ GEARBOX. THE SENSOR AND THE GEARBOX ARE AN ASSEMBLY THAT YOU MUST NOT DISASSEMBLE ON THE AIRCRAFT. IF YOU REMOVE THE SENSOR FROM THE GEARBOX:
 -YOU WILL CAUSE DAMAGE TO THE SENSOR BOX
 -THE ADJUSTMENT OF THE SENSOR BOX WILL NO LONGER BE CORRECT.
 WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
 START A TASK ON OR NEAR:

 -
THE FLIGHT CONTROLS

 -
THE FLIGHT CONTROL SURFACES

 -
THE LANDING GEAR AND THE RELATED DOORS

 -COMPONENTS THAT MOVE.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1. Reason for the Job
__________________
 Do this procedure when you have a Sensor Box P/N E2133600 installed on the NLG and when you use the Rudder Trim Angle as reference for the adjustment. R
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 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific nosewheel jack No specific spatula No specific warning placard No specific AC voltmeter (minimum range: 0-20V, accuracy: 1 mV,
 frequency: 50-2000 Hz) No specific 1.2m (4ft.) square steel plates No specific Torque Wrench : range 0.00 to 1.20 m.daN
 (0.00 to 9.00 lbf.ft) F26792000 1 SENSOR-VOLTAGE TEST F26792000-1 1 SENSOR - VOLTAGE TEST
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
 Material No. 09-008E  USA AMS 3277 EARLY QUICK REPAIR FUEL TANK SEALANT (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-003 Lifting of the Aircraft at Forward Jacking Point, MLG Wheels on the Ground 07-11-00-586-001 Lowering of the Aircraft at Forward Jacking Point,
 MLG Wheels on the Ground 07-12-00-582-001 Jacking for Nose Gear Wheel Change 09-10-00-584-002 Towing with the Nose Gear from the Front 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the
　
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