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. 19-010  USA AMS 5687
 LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
 (Ref. 20-31-00)

 1EFF : ALL 1 32-22-13Page 406 1 1 May 01/05 1 1 1CES 1

 C. Expendable Parts
 -------------------------------------------------------------------------------
FIG.ITEM |DESIGNATION |IPC-CSN
 -------------------------------------------------------------------------------
8 cotter pin 32-22-01 03A-030 8 cotter pin 32-22-01 03C-030 8 cotter pin 32-22-01 03D-030 9 cotter pin 32-22-01 03A-030 9 cotter pin 32-22-01 03C-030 9 cotter pin 32-22-01 03D-030 19 cotter pin 32-22-01 03A-090 19 cotter pin 32-22-01 03C-090 19 cotter pin 32-22-01 03D-090 22 cotter pin 32-22-01 03A-140 22 cotter pin 32-22-01 03C-140 22 cotter pin 32-22-01 03D-140 23 cotter pin 32-22-01 03A-090 23 cotter pin 32-22-01 03C-090 23 cotter pin 32-22-01 03D-090 26 cotter pin 32-22-01 03A-140 26 cotter pin 32-22-01 03C-140 26 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 32-22-00-220-001 Check of the Nose-Gear Doors Gaps and Mismatches 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
R **ON A/C 001-049, 051-099, 101-105, 151-156, 201-209,
 32-22-13-991-001 Fig. 401
 1EFF : ALL 1 32-22-13Page 407 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------

R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
 32-22-13-991-001-A Fig. 401A
 **ON A/C ALL

 3. Job Set-up
__________
 Subtask 32-22-13-860-050

 A. Aircraft Maintenance Configuration
 (1)
 In the cockpit, on the panel 400VU, make sure that the warning notice(s) is (are) in position to tell persons not to operate the landing gear control lever.

 (2)
 Make sure that the access platform is in position.

 (3)
 Make sure that the safety barriers are in position.

 (4)
 Make sure that the aircraft is on jacks at the forward jacking point (Ref. TASK 07-11-00-581-003).

 4. Procedure
_________
 **ON A/C 001-049, 051-099, 101-105, 151-156, 201-209,

 (Ref. Fig. 401/TASK 32-22-13-991-001) R **ON A/C 106-149, 157-199, 210-299, 301-399, 401-499,
 (Ref. Fig. 401A/TASK 32-22-13-991-001-A)
 1EFF : ALL 1 32-22-13Page 408 1 1 Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105, 151-156, 201-209,

 Subtask 32-22-13-420-053
 A. Installation of the Aft Door
 (1)
 Install the bush (11) on the door assembly (25). NOTE : Make sure that the bush (11) is in the correct position.

____

 (2)
 Install the bushes (18) and (10) on the fittings and keep the door

 (25) in position.

 (3)
 Lubricate the bolts (13) and (16) with COMMON GREASE (Material No. 04-004) or COMMON GREASE (Material No. 04-022).

 NOTE : Do not mix Material No. 04-004 with Material No. 04-022. You
____ can use Material No. 04-022 as an alternative to Material No. 04-004. Clean and degrease the parts before you use Material No. 04-022.
 (4)
 Install the bolts (13) and (16) and the washers (12) and (17).
　
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