-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
1. Reason for the Job
__________________
Refer to the MMEL TASK: 32-31-02-B)
Normal Extention And Retraction
Proximity detectors
System 2
11GA(10GA), 13GA, 17GA(16GA), 19GA, 23GA(22GA), 25GA, 29GA(28GA), 31GA,
35GA(34GA), 39GA(38GA)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific warning notice No specific access platform 2 m (6 ft. 7 in.)
1EFF : ALL 1 32-31-00Page 401 1 1 Feb 01/98 1 1 1CES 1 B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
21-26-00-710-001
21-27-00-710-001
22-60-00-710-001 27-51-00-740-002
27-81-00-740-002
R 27-93-00-710-001
R 27-94-00-710-001
27-94-00-710-002
27-94-00-710-003
R 27-96-00-740-001 31-60-00-860-001 31-60-00-860-002 32-00-00-481-001
32-00-00-481-002
32-12-00-010-001 32-12-00-410-001 32-22-00-010-001 32-22-00-410-001 32-31-00-720-002
32-31-73-200-001
32-69-00-740-001 34-13-00-740-002 34-13-00-740-003 34-42-00-740-002 Operational Test of the Avionics Equipment Ventilation from the Multipurpose Control and Display Unit (MCDU)Operational Test of the Avionics Equipment Ground Cooling Fault WarningOperational Test of the FAC 2 FunctionsBite Test of the Slat and Flap Control Computers (Flap System)Bite Test of the Slat and Flap Control Computers (Slat System) Operational Test of the Elevator and Aileron Computers (ELACs)Operational Test of the Spoiler Elevator Computer 3 (SEC 3)Operational Test of the Spoiler Elevator Computer 1 (SEC 1)Operational Test of the Spoiler Elevator Computer 2 (SEC 2) BITE Test of the EFCS (Ground Scanning)EIS Start ProcedureEIS Stop ProcedureInstallation of the Safety Devices on the Landing GearsInstallation of the Safety Devices on the Landing Gear DoorsOpen the Main Gear Doors for AccessClose the Main Gear Doors after AccessNose Gear Doors - Ground Doors OpeningNose Gear Doors - Ground Doors ClosingFunctional Test of the Normal Extension and Retraction of the Landing GearInspection of the MLG Proximity Sensor and Target ClearancesBITE Test of the Landing GearINTERFACE TEST of the ADRSYSTEM TEST of the ADRBITE Test of the Radio Altimeter
1EFF : ALL 1 32-31-00Page 402 1 1 Nov 01/01 1 1 1CES 1
3. Job Set-up
__________
Subtask 32-31-00-941-069
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Make sure that the ground safety locks are on the landing gear (Ref. TASK 32-00-00-481-001).
(3)
On the panel 400VU:
-make sure that the landing-gear control-lever 6GA is in the DOWN position
-put a warning notice in position to tell persons not to operate the landing gear/landing gear doors.
Subtask 32-31-00-010-064
B. Get Access
(1)
Open the applicable MLG door (Ref. TASK 32-12-00-010-001) or the applicable NLG door (Ref. TASK 32-22-00-010-001).
(2)
Make sure that the GROUND LOCK SLEEVE (460005835) is installed, if you open the MLG doors, on the applicable MLG door actuating-cylinder (Ref. TASK 32-00-00-481-002).
(3)
Make sure that the SAFETY PIN - NLG DOOR (98D32203502000) is installed, if you open the NLG doors, in the rigging holes of the left and right nose gear doors.
(4)
Put the access platform in position in zone 734/744 for the MLG.
R (5) Put the access platform in position in zone 123 for the NLG. Subtask 32-31-00-869-100
C. Aircraft Maintenance Configuration
(1)
Do the EIS start procedure (upper ECAM DU only) (Ref. TASK 31-60-00-860-001).
(2)
On the panel 50VU, make sure that the ENG FADEC GND PWR 1 and 2 pushbutton switches are released (ON legends come on).
1EFF : ALL 1 32-31-00Page 403 1 1 Aug 01/02 1 1 1CES 1 1EFF : ALL 1 32-31-00Page 404 1 1 Aug 01/02 1 1 1CES 1
Subtask 32-31-00-865-089
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