(2)
 Remove the hubcap (4). NOTE : Remove the hubcap along the centerline of the wheel axle to

____ prevent damage to the tachometer drive shaft.
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 Main Wheel Hubcap
 Figure 402/TASK 32-41-00-991-035

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 5. Close-up
________ Subtask 32-41-00-942-058
 A. Remove the Safety Devices:
 (1)
 Remove the warning notice.

 (2)
 Remove the wheel chocks at the main landing gear.

 (3)
 Make an entry in the log book.

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 Reactivation of the Main Wheel hubcap
 1. Reason for the Job
__________________
 Refer to the CDL TASK: 32-2
 Main Wheel Hubcap
 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 warning notice No specific wheel chocks
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-003 USA MIL-T-5544
 GRAPHITED PETROLATUM THREAD COMPOUND (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1
 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819
 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
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 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
07-12-00-582-002 Jacking for Main Gear Wheel Change 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) 29-24-00-863-001 Pressurize the Yellow Hydraulic System with the
 Electric Pump 32-42-00-720-002 Functional test of the tachometers 32-41-00-991-035 Fig. 402
 3. Job Set-up
__________
 Subtask 32-41-00-941-059
 A. Safety Precautions
 (1)
 On the panel 400VU:

 -put a warning notice in position to tell persons not to operate the landing gear control lever.

 (2)
 Make sure that the wheel chocks are in position.

 Subtask 32-41-00-865-059
 B. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU HYDRAULIC/BRAKING AND STEERING/SYS2/SPLY 4GG M36 121VU HYDRAULIC/BRAKING AND STEERING/SYS2/CTL 3GG M35 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/CTL 1GG M34 121VU HYDRAULIC/BRAKING AND STEERING/SYS1/IND AND/SPLY 2GG M33
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 C. Aircraft Maintenance Configuration
 (1)
 On the panel 110VU:

 -Make sure that the PARK BRK control switch is set to ON.

 (2)
 On the panel 400VU:

 -make sure that the brake pressure indication on the Yellow brake-pressure triple indicator is correct.
 -If necessary pressurize the brake accumulator with the yellow pump (Ref. TASK 29-24-00-863-001).

 (3)
 Lift the related axle with a jack (Ref. TASK 07-12-00-582-002).

 (4) Fully deflate the tire. Subtask 32-41-00-420-050
 D. Preparation for Installation
 (1)
 Clean the component interface and/or the adjacent area with MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).

 (2)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (3)
 Do an inspection of the component interface and/or the adjacent area.
　
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