(1)
 Remove the cotter pin (6) and discard it, remove the nut (7) and the washer (8).

 (2)
 Remove the bolt (9) and disconnect the rotating rod from the aft door of the nose landing gear.

 (3)
 Remove the access platform(s).

 (4)
 Retract the nose landing gear (Ref. TASK 32-30-00-867-001).

 (5)
 Remove the cotter pin (15) and discard it, remove the nut (14) and the washer (13).

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 Rotating Rod
 Figure 401/TASK 32-22-16-991-001
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1  1  Feb 01/98
 1  1
 1CES  1

 (6) Remove the bolt (10) and the bushes (11) and (12).
 (7) Remove the rotating rod. Subtask 32-22-16-020-052
 B. Removal of the Universal Joint (1) from the Rod Assy (5)
 (1)
 Disengage the tab of the lockwasher (3) from the nut (2).

 (2)
 Loosen the nut (2).

 (3)
 Remove the universal joint (1) from the rod assy (5) and discard the lockwasher (3).

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 Installation of the Rotating Rod
 1. Reason for the Job
__________________
 Self Explanatory
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
REFERENCE  QTY DESIGNATION
 -------------------------------------------------------------------------------
No specific safety barriers
 No specific warning notice(s)
 No specific access platform 1.7 m (5 ft. 7 in.)

R No specific  Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
 (2.00 to 26.00 lbf.ft) 98AMS172321000 1 ADAPTOR - WRENCH
 B. Consumable Materials
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
Material No. 04-004  USA MIL-PRF-23827 TYPE I
 SYNTH.ESTER BASED GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 04-022  USA MIL-PRF-81322 GRADE 2
 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
 (Ref. 20-31-00)

 Material No. 11-002  USA MIL-PRF-680
 DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
 (Ref. 20-31-00)

 Material No. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

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 C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ---------------------------------------- |IPC-CSN------------------------------
3  lockwasher  32-22-01 03A-184
 3  lockwasher  32-22-01 03C-184
 3  lockwasher  32-22-01 03D-184
 6  cotter pin  32-22-01 03A-140
 6  cotter pin  32-22-01 03C-140
 6  cotter pin  32-22-01 03D-140
 15  cotter pin  32-22-01 03A-140
 15  cotter pin  32-22-01 03C-140
 15  cotter pin  32-22-01 03D-140
 D. Referenced Information
 ------------------REFERENCE  -------------------------------DESIGNATION ------------------------------

-------------------------------------------------------------------------------
07-11-00-581-003 Lifting of the Aircraft at Forward Jacking Point, MLG Wheels on the Ground 07-11-00-586-001 Lowering of the Aircraft at Forward Jacking Point,
 MLG Wheels on the Ground 12-22-32-640-002 Lubrication of the NLG and Doors 32-22-00-010-001 Nose Gear Doors - Ground Doors Opening 32-22-00-410-001 Nose Gear Doors - Ground Doors Closing 32-30-00-867-001 Retraction of the Landing Gear for Maintenance 32-30-00-867-002 Extension of the Landing Gear after Maintenance 32-31-00-720-003 Functional Test of the Normal Extension and
 Retraction of the Nose Landing Gear 32-22-16-991-001 Fig. 401
 3. Job Set-up
__________
 Subtask 32-22-16-860-051
 A. Aircraft Maintenance Configuration
 (1)
　
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