(2) For the slat-track can 12:
-disconnect the drain pipe (71) from the slat-track can (70).
-remove the bolts (72)
-carefully remove the slat-track can (70).
NOTE : You must keep the bolts (72) in their related positions.
____
1EFF : ALL 1 57-24-11Page 412 1 1 May 01/04R 1 1 1CES 1
TASK 57-24-11-400-002
Installation of the Slat-track Cans 1 thru 12
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
__________________
Self explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific plastic spatula
No specific safety barriers
No specific warning notices
No specific access platform 4 m (13 ft. 1 in.)
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) R Material No. 11-003 USA ASTM D 740 METHYL-ETHYL-KETONE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
12-11-28-650-003 24-41-00-861-002
24-41-00-862-002
27-80-00-866-004 27-80-00-866-005 28-10-00-910-001 28-10-00-910-002 28-11-00-790-002
R 28-11-00-790-008 28-12-46-000-001 28-12-46-400-001 28-25-00-650-001 28-25-00-869-001 57-27-11-000-001
57-27-11-000-002
57-27-11-400-001
57-27-11-400-002
57-24-11-991-001-A 57-24-11-991-002-A 57-24-11-991-003 57-24-11-991-004 57-24-11-991-005 57-24-11-991-006 Pressure Refuel with Automatic ControlEnergize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerExtending the Slats on the GroundRetracting the Slats on the GroundSafety Procedures When You Do Work in a Fuel TankAccess to the Fuel Tanks and the Work AreasLeak Test with Fuel of the Wing-Tank Outer and Inner Cells Leak Test with Fuel of the Wing TankRemoval of the Overpressure-Protector OutletInstallation of the Overpressure-Protector OutletPressure DefuelFuel TransferRemoval of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)Removal of the Access Panel (540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, 640KB, ....)Installation of the Access Panel (540AB, 540BB, 540CB, 540DB, 540EB, 540FB, 540GB, 640AB, 640BB, 640CB, 640DB, 640EB, 640FB, 640GB)Installation of the Access Panel (540HB, 540JB, 540KB, 540LB, 540MB, 540NB, 540PB, 540QB, 540RB, 550AB, 550BB, 550CB, 550DB, 560AB, 640HB, 640JB, ....)Fig. 401Fig. 402Fig. 403Fig. 404Fig. 405Fig. 406
3. Job Set-up
__________
Subtask 57-24-11-941-053
A. Safety Precautions WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN A FUEL TANK.
_______
(1)
Obey the fuel safety procedures (Ref. TASK 28-10-00-910-001) when you do work in the fuel tanks.
(2)
Make sure the warning notices are in position in the cockpit to tell persons not to operate the flap/slat system or the fuel system.
(3)
Make sure the safety barriers are in position.
(4)
Make sure the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is installed on the flap/slat control lever.
Subtask 57-24-11-860-051
B. Aircraft Maintenance Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1) Make sure the slats are in the fully extended position (Ref. TASK 27-80-00-866-004).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 57-24-11-010-054-A
C. Get Access
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本文鏈接地址：A320飛機維護手冊 AMM WINGS 機翼2(11)
