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 -YOU WILL CAUSE DAMAGE TO THE SENSOR BOX
 -THE ADJUSTMENT OF THE SENSOR BOX WILL NO LONGER BE CORRECT.
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
 WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific spatula No specific warning notices No specific AC voltmeter (minimum range:0-20V, accuracy: 1 mV,
 frequency: 50-2000 Hz) 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
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 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004A INFORMATION TRANSFERRED TO 04-022 (Ref. 20-31-00) Material No. 09-008E USA AMS 3277 EARLY QUICK REPAIR FUEL TANK SEALANT (Ref. 20-31-00)
 Material No. 11-002  USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00)
 Material No. 19-010  USA AMS 5687 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-11-00-581-001 Lifting for Aircraft Maintenance Operations 07-11-00-581-003 Lifting of the Aircraft at Forward Jacking Point, MLG Wheels on the Ground 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 32-51-00-720-003 Functional Test of the Nose Wheel Steering with the
 Handwheel. 32-51-19-991-002 Fig. 402 32-51-19-991-003 Fig. 403
 3. Job Set-up
__________
 Subtask 32-51-19-860-056
 A. Aircraft Maintenance Configuration
 (1) In the cockpit, on the panel 400VU, make sure that the warning notice is in position to tell persons not to operate the landing gear control lever.
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 (2)
 On the CAPT and F/O NWS handwheels and on the brake pedals, make sure that the warning notices are in position to tell persons not to operate them.

 (3)
 Make sure that the safety barriers are in position.

 (4)
 Make sure that the aircraft is lifted at the forward jacking point (Ref. TASK 07-11-00-581-003).

 (5) On the panel 402VU, set the A/SKID & N/W STRG switch to OFF. Subtask 32-51-19-865-060
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33
 Subtask 32-51-19-865-062
 C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35
 4. Procedure
_________
 (Ref. Fig. 402/TASK 32-51-19-991-002, 403/TASK 32-51-19-991-003) Subtask 32-51-19-560-051
 A. Preparation of the Replacement Component
 (1)
 Clean the component interface and/or the adjacent area.

 (2)
 Clean the attachment hardware with CLEANING AGENTS (Material No. 11-002) and dry with filtered compressed air.

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 Sensor Box P/N E21336000 - Adjustment
 Figure 403/TASK 32-51-19-991-003

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