-
the toothplate (108).
(b)
Remove the eccentric bush (107). If necessary, carefully lift the flap with the hoist and the sling to release the weight from the eccentric bush (107).
(c)
Discard the tabwasher (112) and the lockwasher (109).
(2) Remove the flap from the wing:
CAUTION : MAKE SURE THAT THE SUPPORT STRUCTURE IS CLEAN AND DOES NOT
_______
HAVE ANY SHARP POINTS.
CAUTION : MAKE SURE THAT THE FLAP DOES NOT HIT THE AIRCRAFT
_______
STRUCTURE.
(a)
Lift the flap with the hoist until it is clear of the flap track carriage at the track 2 position.
(b)
Move the outboard end of the flap, aft, until it is clear of the wing.
(c)
Pull the flap outboard until the flap drive trunnion is clear of the flap track carriage of the track 1 position.
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(d) Move the flap with the hoist to a flat support structure and lower it onto the support.
(3) Put covers, where necessary, over the disconnected items of the flap. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-61-080-050
E. Removal of Equipment
(1) Remove the hoisting sling (Ref. TASK 27-50-00-000-002).
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Installation of the Inboard Flap
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific adhesive tape No specific pneumatic wrench No specific safety barriers No specific warning notice No specific warning notice(s) No specific access platform 3.0 m (9 ft. 10 in.) No specific Torque Wrench : range 0.00 to 1.20 m.daN
(0.00 to 9.00 lbf.ft) No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) No specific Torque Wrench : range 1.00 to 10.00 m.daN
(8.00 to 75.00 lbf.ft) No specific Torque Wrench : range 2.00 to 20.00 m.daN
(15.00 to 150.00 lbf.ft) 98D27504035000 1 TORQUE ADAPTOR-TRUNNION NUT 98D27504084000 1 EXTRACTOR - PIN 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-022 USA MIL-PRF-81322 GRADE 2
SYNTHE.HYDROCARBON GREASE HIGH PRESSURE
(Ref. 20-31-00) Material No. 08-004A USA MIL-A-46106 TYPE I
ADHESIVE SEALANT (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 15-007 AIB TN 10138 TYPE II GRADE 1
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
(Ref. 20-31-00) Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00) Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Expendable Parts
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
77 cotter pin 27-54-05 33F-150 77 cotter pin 27-54-05 33U-150 82 cotter pin 27-54-05 33F-035 83 cotter pin 27-54-05 33F-030 83 cotter pin 27-54-05 33U-030 83 cotter pin 27-54-05 33U-030A 89 cotter pin 27-54-05 33F-025 175 cotter pin 27-54-46 04B-035 176 crushable spacer 27-54-46 04B-080
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 428 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 D. Referenced Information
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱6(22)
