(b)
On the panel 11VU, push the WHEEL pushbutton switch in.
(c)
On ECAM, make sure that the applicable green door-uplock symbol is in-line.
(d) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
Subtask 32-12-00-862-050
B. De-energize the Electrical Circuits
(1) De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 32-12-00Page 207 1 1 May 01/98 1 1 1CES 1 Subtask 32-12-00-942-052
C. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 32-12-00Page 208 1 1 Feb 01/98 1 1 1CES 1 MAIN GEAR DOORS - DEACTIVATION/REACTIVATION
___________________________________________
TASK 32-12-00-040-001
Preparation of the Aircraft for 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
_______ 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
_______ GEAR.
1. Reason for the Job
__________________
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 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)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B CORROSION INHIBITING FILLET CONSISTENCY (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 32-12-00Page 401 1 1 Feb 01/05R 1 1 1CES 1
C. Expendable Parts -------------------------------------------------------------------------------
FIG.ITEM --------- |DESIGNATION ------------------------------------ |IPC-CSN----------------------------------
51 cotter pin 32-11-11 80 -090
51 cotter pin 32-11-11 80C-090
51 cotter pin 32-11-11 80D-090
D. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 32-12-00-010-001 32-12-11-000-001 32-12-13-000-001 32-12-14-000-001 32-12-14-400-001
32-31-35-000-001
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 PowerOpen the Main Gear Doors for AccessRemoval of the Door Assembly - Main.Removal of the Secondary Hinged FairingRemoval of the MLG Fixed Fairing AssemblyInstallation of the MLG Fixed Fairing Assembly (That was Removed For Access Only)Removal of the MLG Door Actuating-Cylinder 2523GM (2522GM)
1EFF : ALL 1 32-12-00Page 402 1 1 Feb 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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