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 B. Referenced Information
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REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action 32-00-00-481-001 Installation of the Safety Devices on the Landing Gears 32-00-00-860-001 Flight Configuration Precautions with Electrical Power 32-00-00-860-002 Ground Configuration after Flight Configuration with Electrical Power 32-41-11-000-006 Removal of the MLG Wheel (2649GM,2650GM,2651GM,2652GM) 32-41-11-400-006 Installation of the MLG Wheel
 (2649GM,2650GM,2651GM,2652GM) 32-42-27-000-001 Removal of the Brake (2641GM,2642GM,2643GM,2644GM) 32-42-27-400-001 Installation of the Brake
 (2641GM,2642GM,2643GM,2644GM)
 32-42-71-000-001 Removal of the MLG Axle Adaptor-Sleeves
 32-42-71-400-001 Installation of the MLG Axle Adaptor-Sleeves
R  32-48-51-000-005 Removal of the Fan Assy (7GS,8GS,9GS,10GS) 
R  32-48-51-400-005 Installation of the Fan Assy (7GS,8GS,9GS,10GS) 32-11-00-991-022-A Fig. 606
 3. Job Set-up
__________
 Subtask 32-11-00-941-075
 A. Safety Precautions
 (1)
 Make sure that the ground safety locks are installed on the landing gear (Ref. TASK 32-00-00-481-001).
 (2)
 On the panel 400VU:
 -make sure that the landing-gear control-lever 6GA is in the DOWN position
 -put a warning notice in position to tell persons not to operate the landing gear.
 (3)
 Make sure that the Green and Yellow hydraulic systems are depressurized (Ref. TASK 29-00-00-864-001).
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 (4) Put warning notices in position to tell persons not to operate the landing gear doors.
 (5) Put the safety barriers in position.
 Subtask 32-11-00-869-057
 B. Flight Configuration Precautions
 (1)
 If the electrical power is not necessary for other maintenance tasks, de-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 (2)
 If the electrical power is necessary, do the precautions for flight configuration (Ref. TASK 32-00-00-860-001) before you lift the aircraft.
 **ON A/C 001-049, 101-149, 151-199, 201-299,
 Subtask 32-11-00-010-065
 C. Get Access
 (1)
 Remove the MLG wheels (Ref. TASK 32-41-11-000-006).
 (2)
 Remove the MLG brakes (Ref. TASK 32-42-27-000-001).
 (3) Remove the MLG axle adaptor sleeves (Ref. TASK 32-42-71-000-001). R **ON A/C 051-099, 301-399, 401-499,
 Subtask 32-11-00-010-065-A
 C. Get Access
 (1)
 Remove the MLG brake fans (Ref. TASK 32-48-51-000-005).
 (2)
 Remove the MLG wheels (Ref. TASK 32-41-11-000-006).
 (3)
 Remove the MLG brakes (Ref. TASK 32-42-27-000-001).
 (4)
 Remove the MLG axle adaptor sleeves (Ref. TASK 32-42-71-000-001).
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 4. Procedure
_________
 (Ref. Fig. 606/TASK 32-11-00-991-022-A)
 Subtask 32-11-00-210-072-A
 A. Visual Inspection of the MLG Axle Lands
 (1)
 Examine the MLG axles for overheating.
 (2)
 Examine the axle lands for discoloration and/or deterioration of the chrome finish.
 (3)
 Examine the axle adaptor sleeves for:
 -scoring of the internal surface
 - overheating/discoloration.
 Subtask 32-11-00-220-064
 B. Detailed Inspection of the MLG Axle Lands
 (1)
 Measure the out-of-roundness of the axle lands T. The axle lands T must be round within 40 microns (1600 micro-inches).
 (2)
 Measure the out-of-roundness of the axle lands S. The axle lands S must be round within 63 microns (2500 micro-inches).
 5. Close-up
________ R **ON A/C 001-049, 101-149, 151-199, 201-299,
 
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