(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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