-
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
__________________
R Do this procedure when you have a Sensor Box P/N E21336000 installed on the R NLG and when you use the Nose Wheel Alignment Tool for the adjustment R
 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 spatula
 No specific warning placard
 No specific AC voltmeter
 No specific square steel plates 1.2 m (3 ft. 11 in.)
 No specific Torque Wrench : range 0.00 to 1.20 m.daN

 (0.00 to 9.00 lbf.ft)
 F26792000 1 SENSOR-VOLTAGE TEST

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 -------------------------------------------------------------------------------
R
R

R

REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
F26792000-1 1 SENSOR - VOLTAGE TEST JT2000AIRBUS 1 NOSE WHEEL ALIGNMENT TOOL 98A09003000001 1 BAR - STEERING NOSE WHEEL
 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 -------------------------------------------------------------------------------
07-12-00-582-001 Jacking for Nose Gear Wheel Change 08-22-00-200-001 Precise Leveling 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
 External Power 29-10-00-863-001 Pressurize the Green Hydraulic System 29-10-00-863-002 Pressurize the Yellow Hydraulic System 29-10-00-864-001 Depressurize the Green Hydraulic System 29-10-00-864-002 Depressurize the Yellow Hydraulic System 32-46-00-740-001 BITE Test of the BSCU 53-15-11-010-001 Opening of the Radome 110AL 32-51-00-991-027 Fig. 526 32-51-00-991-035 Fig. 527
**ON A/C 005-049, 055-099, 101-149, 151-199, 201-299, 401-499,
 32-51-00-991-036  Fig. 528
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REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
**ON A/C 301-399,
 32-51-00-991-036-A Fig. 528A R **ON A/C 005-049, 055-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-51-00-991-029 Fig. 529
 3. Job Set-up
__________
 Subtask 32-51-00-941-059

 A. General
 (1)
 Put a warning placard in the cockpit to tell persons not to operate R the landing gear or the N/WS.

 (2)
 On the panel 400VU, make sure that the L/G normal control lever is in the DOWN position and the A/SKID & N/W STRG switch is ON.

 (3)
 On the nose gear leg, on the nose wheel steering deactivation electrical box, make sure that the towing lever is in the normal position (engaged position).

 (4)
 Make sure that the N/WS handwheels and the rudder pedals are in the neutral position.

 (5)
 Make sure that RUD TRIM indicator shows 0. R **ON A/C 005-049, 055-099, 101-149, 151-199, 201-299, 301-399,

 Subtask 32-51-00-860-077
 B. Aircraft Maintenance Configuration
 (1) Move the aircraft and position the nosewheels on the square steel plates
 (a) Position a steel plate in front of the wheels
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 (b)
 Apply a thick layer of COMMON GREASE (Material No. 04-004) to the upper surface of the steel plate

 (c)
 Put the other steel plate on the top of the greased steel plate
　
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