(3)
 Remove the hubcap (1).

 1EFF : ALL 1 32-41-00Page 403 1 1 Aug 01/05 1 1 1CES 1

 Nose Wheel Hubcap Deactivation/Reactivation
 Figure 401/TASK 32-41-00-991-010

R 1EFF : 001-049, 101-149, 151-199, 201-299, 1 32-41-00Page 404 1301-399, 401-499, 1Aug 01/05 1 1 1CES 1R Nose Wheel Hubcap Deactivation/Reactivation R Figure 401A/TASK 32-41-00-991-010-A

R 1EFF : 051-099, 1 32-41-00Page 405 1 1 May 01/05 1 1 1CES 1

R  **ON A/C 051-099, 
R  Subtask 32-41-00-040-051-A 
R  A. Deactivation of the Nose Wheel Hubcap: 
R  (1) Cut and remove the corrosion resistant steel lockwire. 
R  (2) Remove the screws (11) and the washers (12). 
R  (3) Release the grommet (13) and remove the hubcap (9). 
R  (4) Disconnect the electrical connector (14) from the connector (15) and 
R  install the blanking cap. 
R  WARNING : MAKE SURE THAT THE TIRE IS FULLY DEFLATED._______ 
R  (5) Remove and discard the cotter pin (4). Remove the nut (5). 
R  (6) Remove the pressure transducer (3). 
R  (7) Apply a thin layer of COMMON GREASE (Material No. 04-004) to the 
R  shaft (1). 
R  (8) Install a seal plug (6) on the shaft (1). 
R  (9) Install a nut (7) and tighten it. 
R  (10) Safety the nut (7) with the cotter pin (8). 
R  (11) Remove the rotating mechanism (Ref. TASK 32-49-17-000-001). 
R  (12) Inflate the tire on the related NLG wheel (Ref. TASK 12-14-32-614-
R  001). 
R  (13) Put a temporary placard in the cockpit to warn the crew that the tire 
R  pressure indication is not available on the applicable wheel. 

R 1EFF : 051-099, 1 32-41-00Page 406 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 32-41-00Page 407 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 32-41-00Page 408 1 1 May 01/05 1 1 1CES 1

R  **ON A/C ALL
 5. Close-up________ Subtask 32-41-00-942-052
R  A. Remove the safety devices: (1) Remove the warning notice from the cockpit. (2) Remove the wheel chocks at the main landing gear. (3) Make an entry in the log book. **ON A/C 051-099, 
R  Subtask 32-41-00-865-055 
R R R  B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1GV

R  **ON A/C ALL
 TASK 32-41-00-440-001
 Nose Wheel Hubcap Reactivation
 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 -------------------------------------------------------------------------------
R  No specific No specific No specific  circuit breaker(s) safety clip(s)warning noticewheel chocks
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R R R R R  No specific Material No. 04-004 Material No. 11-002  lockwire-corrosion resistant steel dia. 0.8 mm (0.032 in.) USA MIL-PRF-23827 TYPE I SYNTH.ESTER BASED GREASE HIGH PRESSURE (Ref. 20-31-00) USA MIL-PRF-680 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT) (Ref. 20-31-00) 
R  C. Expendable Parts 
R R R  -------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R R  2 4  seals cotter pin  32-49-15 01 -050 32-49-15 01 -010

 D. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE DESIGNATION
 -------------------------------------------------------------------------------
12-14-32-614-001 Nitrogen Filling of the Tires
 32-49-00-720-001 Crosscheck TPIS Reading and Tire Pressure Gauge
 32-49-17-400-001 Installation of the NLG TPIS Rotating Mechanism

R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 32-41-00-991-010 Fig. 401
 **ON A/C 051-099,
 32-41-00-991-010-A Fig. 401A
 **ON A/C ALL
 3. Job Set-up
__________ R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 32-41-00-941-053
 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.
　
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