(b) Install the debris guard (23). Make sure that you engage the shaft of the tachometer (31) in the bushing (24).
 NOTE : The debris guard has holes of different diameters:
____
 -large diameter (two): to permit removal of the guard assy without removal of the shroud assy screws (larger than the screw heads).
 -medium diameter (two): to put the locating pins in the correct position. Same holes on the shroud assy (centering function).
 -small diameter (four): to put the four attachment screws in the correct position.
 NOTE : Use the locating pins (17) to put the debris guard (23) in
____
 the correct position.

 (c)
 Install the bolts (22) and the washers (21).

 (d)
 TORQUE the bolts (22) to between 0.22 and 0.24 m.daN (19.46 and

 21.23 lbf.in)
 5. Close-up
________
 Subtask 32-41-11-860-093
 A. Aircraft Maintenance Configuration
 (1)
 Inflate the tire to the unloaded pressure (Ref. TASK 12-14-32-614-001).

 (2)
 Lower the aircraft on its wheels (Ref. TASK 07-12-00-582-002).

 (3)
 Do a check of the pressure of the tire (Ref. TASK 32-41-00-210-003).

 (4)
 Make sure that the work area is clean and clear of tool(s) and other items.

 Subtask 32-41-11-865-094
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GV, 1GS, 2GS, 3GS
 1EFF : 051-099, 1 32-41-11Page 414 1 1 Config-3 May 01/05 1 1 1CES 1 Subtask 32-41-11-710-060

 C. Test
 (1)
 Do the functional test of the tire-pressure indicating (Ref. TASK 32-49-00-720-001).

 (2)
 Do the functional test of the brake fans (Ref. TASK 32-48-00-720-001).

 1EFF : 051-099, 1 32-41-11Page 415 1 1 Config-3 May 01/05 1 1 1CES 1 WHEEL - NLG (2659GM,2660GM) - REMOVAL/INSTALLATION

__________________________________________________
 TASK 32-41-12-000-001
 Removal of the NLG Wheel (2659GM,2660GM)
 WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
 GEAR.

 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific blanking cap
 No specific circuit breaker(s) safety clip(s)
 No specific warning notice
 J47548 1 PROTECTOR NLG
 J47549 1 ADAPTOR NLG

 B. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
07-12-00-582-001  Jacking for Nose Gear Wheel Change
 32-00-00-481-001  Installation of the Safety Devices on the Landing Gears
 32-41-00-210-003  Inspection/Check of the Pressure of Tires
R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-41-12-991-001 Fig. 401
 **ON A/C 051-099,

 32-41-12-991-001-A  Fig. 401A
 1EFF : ALL 1 32-41-12Page 401 1 1 Aug 01/05 1 1 1CES 1 1EFF : ALL 1 32-41-12Page 402 1 1 May 01/05 1 1 1CES 1

R  **ON A/C ALL
 3. Job Set-up__________ 
R  **ON A/C 051-099, 
R  Subtask 32-41-12-865-050 
R  A. Open, safety and tag this(these) circuit breaker(s): 
R R R R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/TIRE/PRESS 1GV M31 
R  **ON A/C ALL
 Subtask 32-41-12-941-050 
R  B. Safety Precautions
 (1) Put the wheel chocks in position at the main landing gear.
 (2) In the cockpit, put a warning notice on the panel 400VU to tell persons not to operate the landing gear.
 Subtask 32-41-12-860-050 
R  C. Aircraft Maintenance Configuration
 (1) Make sure that the safety devices are installed on the landing gears (Ref. TASK 32-00-00-481-001).
 (2) Lift the nose gear (Ref. TASK 07-12-00-582-001).
　
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