Restoration of the Aircraft after Flight with One MLG Door Assembly Missing or One MLG Fixed Fairing Assembly Missing or One Secondary Hinged Fairing Missing
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
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START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
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GEAR.
1. Reason for the Job
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Refer to the CDL TASK: 52-13
MAIN LANDING GEAR DOORS (732, 733, 742,
743, 744) (Flight with gear down)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking plugs
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
R No specific access platform 1.6 m (5 ft. 3 in.) No specific access platform 3 m (9 ft. 10 in.) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 460005833 1 GROUND LOCK SLEEVE
1EFF : ALL 1 32-12-00Page 431 1 1 Nov 01/03 1 1 1CES 1 B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R Material No. 02-003 F NSA 307110 TYPE 4
R Material No. 02-003A HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307110 TYPE 4
R Material No. 02-003B HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 TYPE 4
Material No. 02-003C HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)F NSA 307-110 TYPE IV
R Material No. 02-003D HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00) F NSA 307-110 TYPE IV
Material No. 07-010 HYDRAULIC FLUID (PHOSPHATE ESTER BASE) (Ref. 20-31-00)D DA-4-653-91
Material No. 09-016 LACQUER OBSOLETE USE 16-047 (Ref. 20-31-00)USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
Material No. 19-010 (Ref. 20-31-00)USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
1 cotter pin 32-12-03 01D-130
51 cotter pin 32-11-11 80 -090
51 cotter pin 32-11-11 80C-090
51 cotter pin 32-11-11 80D-090
69 cotter pin 57-26-05 36 -030
1EFF : ALL 1 32-12-00Page 432 1 1 Feb 01/05 1 1 1CES 1 D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-22-32-640-001 20-28-00-912-004
24-41-00-861-002
24-41-00-862-002
29-00-00-910-002 29-10-00-864-001 32-00-00-481-001
R R R R 32-00-00-860-001 32-00-00-860-002 32-12-11-400-001 32-12-13-400-001
32-12-14-000-001 32-12-14-400-002
32-31-00-710-002 32-31-35-400-001
32-31-38-400-001
51-75-13-916-002 57-26-21-400-001
32-12-00-991-011 32-12-00-991-015 32-12-00-991-009 32-12-00-991-010
Lubrication of the MLG and DoorsElectrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerSafety Procedures of the Hydraulic SystemDepressurize the Green Hydraulic SystemInstallation of the Safety Devices on the Landing Gears Flight Configuration Precautions with Electrical Power Ground Configuration after Flight Configuration with Electrical PowerInstallation of the Door Assembly - Main.Installation of a Replacement Secondary Hinged FairingRemoval of the MLG Fixed Fairing AssemblyInstallation of a Replacement MLG Fixed Fairing AssemblyOperational Test of the Landing Gear DoorsInstallation of the MLG Door Actuating-Cylinder 2523GM (2522GM)Installation of the MLG Door Swivel-Joint Assembly 2763GM (2764GM)Repair to a layer of Corrosion Preventive CompoundInstallation of the Secondary-Hinged-Fairing AttachmentFig. 401Fig. 402Fig. 403Fig. 404 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM LANDING GEAR 起落架3(13)
