(13)
Disconnect the electrical connector (37) from the connector on the take off light 7LRA (41).
(14)
Remove the nut (42), the washer (43), the screw (38), the washer (39) and the clamp (44) from the support (40).
(15)
Remove the screw (49), the washer (50) and the clamp (51) from the bracket (52).
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NLG - Electrical Harness 1M Figure 402/TASK 32-21-43-991-002- 13 (SHEET 1)
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NLG - Electrical Harness 1M Figure 402/TASK 32-21-43-991-002- 23 (SHEET 2)
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NLG - Electrical Harness 1M Figure 402/TASK 32-21-43-991-002- 33 (SHEET 3)
R 1EFF : 1 1 1CES ALL 1 111 32-21-43 Page 420 May 01/05
(16)
Remove the screw (45), the washer (46), the strut (47) and the clamp
(48) from the bracket (52).
(17)
Disconnect the electrical connector (53) from the proximity sensors 18GAA on the bracket (54).
(18)
Remove the screw (58), the washer (57) and the clamp (56) from the bracket (55).
(19)
Disconnect the electrical connector (65) from the connector on the A/C interface 1300VCA.
(20)
Remove the nuts (60), the washers (61), the screws (64) and the washers (63) to release the clamp (62) on the bracket (59).
(21)
Cut, remove and discard the braid (66) from the grommet (67).
(22)
Remove the upper harness 1M(28).
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TASK 32-21-43-400-002 Installation of the NLG Electrical Harness 1M WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adjustable access platform No specific blanking caps No specific warning notice(s)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-047 C Z-11.904 ANTI COR. COMPOUND(HIGH TEMP.SILICONE SEALANT) (Ref. 20-31-00)
1EFF : ALL 1 32-21-43Page 422 1 1 May 01/05R 1 1 1CES 1
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R R 4 4 66 66 braid braid braid braid
D. Referenced Information
32-21-43 02 -09032-21-43 02A-090 32-21-43 01 -17032-21-43 01B-170
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-862-002
32-00-00-481-001
32-00-00-481-002
R 32-00-00-860-001
R
R 32-00-00-860-002
R
32-22-00-010-001
32-22-00-410-001
R 32-49-00-710-001
R
32-51-00-710-001
R 32-69-00-740-001
R
R
33-43-00-710-001
33-46-00-710-001
32-21-43-991-002
De-energize the Aircraft Electrical Circuits Supplied from the External PowerInstallation of the Safety Devices on the Landing GearsInstallation of the Safety Devices on the Landing Gear Doors Flight Configuration Precautions with Electrical Power Ground Configuration after Flight Configuration with Electrical PowerNose Gear Doors - Ground Doors OpeningNose Gear Doors - Ground Doors Closing Operational Test of the Tire Pressure Indicating System (TPIS)Operational Test of the Nose Wheel Steering with the CFDS. BITE Check Landing Gear Control Interface Unit (LGCIU) using MCDU to Ensure that Continuous BITE is OperativeOperational Test of the Runway Turnoff LightsOperational Test of the Taxi and Take Off LightsFig. 402 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3(123)
