1. Reason for the Job
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R Do this procedure when you adjust a gearbox P/N C24763000 with the adjusting tool F26630200 using the Nose Wheel Alignment Tool. R
2. Job Set-up Information
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A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific warning placard
No specific AC voltmeter
No specific square steel plates 1.2 m (3 ft. 11 in.)
F26630200 1 ADJUSTING TOOL - NWS GEARBOX
F26792000 1 SENSOR-VOLTAGE TEST
F26792000-1 1 SENSOR - VOLTAGE TEST
JT2000AIRBUS 1 NOSE WHEEL ALIGNMENT TOOL
98A09003000001 1 BAR - STEERING NOSE WHEEL
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B. Consumable Materials
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Material No. 04-004 USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 04-015 USA BAC 5001 DACO-5073 GREASE (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
29-10-00-864-001 Depressurize the Green Hydraulic System
32-46-00-740-001 BITE Test of the BSCU
32-51-19-000-001 Removal of the Nose Wheel Steering Feedback Sensor
(3GC, 4GC) P/N C24763000
32-51-19-400-001 Installation of the Nose Wheel Steering Feedback
Sensor (3GC, 4GC) P/N C24763000
53-15-11-010-001 Opening of the Radome 110AL
32-51-00-991-018 Fig. 515
32-51-00-991-037 Fig. 516
32-51-00-991-038 Fig. 517
32-51-00-991-020 Fig. 518
32-51-00-991-021 Fig. 519
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3. Job Set-up
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Subtask 32-51-00-941-058
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.
Subtask 32-51-00-860-075
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
(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
(d)
Move the aircraft and position the nose wheels on the greased steel plates (Ref. TASK 09-10-00-584-002)
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(2) Installation of the NOSE WHEEL ALIGNMENT TOOL (JT2000AIRBUS) (Ref. Fig. 515/TASK 32-51-00-991-018, 516/TASK 32-51-00-991-037, 517/TASK 32-51-00-991-038)
WARNING : BE CAREFUL WHEN YOU USE THIS TOOL, BECAUSE IT CONTAINS
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CLASS 2 LASER EQUIPMENT.
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DO NOT LOOK DIRECTLY INTO THE BEAM
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DO NOT POINT THE BEAM AT OTHER PERSONS. THE LASER CAN CAUSE INJURY IF YOU DO NOT OBEY THESE PRECAUTIONS.
(a)
Open the radome to get access to the reference point (first point) (Ref. TASK 53-15-11-010-001)
(b)
Do a mark on the NLG doors (second point)
