(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).
1EFF : ALL 1 32-22-16Page 402 1 1 Feb 01/98 1 1 1CES 1
Rotating Rod
Figure 401/TASK 32-22-16-991-001
1EFF : ALL 1 32-22-16 Page 403
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).
1EFF : ALL 1 32-22-16Page 404 1 1 Feb 01/98 1 1 1CES 1 TASK 32-22-16-400-001
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)
1EFF : ALL 1 32-22-16Page 405 1 1 May 01/05 1 1 1CES 1
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)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM LANDING GEAR 起落架4(22)