(8)
Disconnect the rear strut (15):
(a)
Remove and discard the cotter pin (17).
(b)
Remove the nut (18) and the washer (16).
(c)
Remove the bolt (24), the washer (23) and disconnect the rear strut (15).
(9)
Remove the eccentric bolt (9):
(a)
Remove and discard the cotter pin (12).
(b)
Remove the nut (11) and the washer (10).
(c)
Remove and discard the lockwire from the bolt (7). NOTE : Write down the position of the punch marks so that the
____ eccentric bolt (9) can be installed in the same position.
(d)
Remove the bolt (7) and the washer (6).
(e)
Remove the toothplate (8) and the eccentric bolt (9).
(10) Removal of the tab from the flap: CAUTION : HOLD THE TAB ALONG THE FULL LENGTH OF THE TRAILING EDGE.
_______ THIS WILL PREVENT DAMAGE TO THE TAB WHEN YOU MOVE IT.
CAUTION : MAKE SURE THAT THE DISCONNECTED PARTS DO NOT TOUCH AND/OR
_______ CATCH THE ADJACENT STRUCTURE WHEN YOU MOVE THE TAB. THIS WILL PREVENT DAMAGE TO THE FLAP.
CAUTION : MAKE SURE THAT THE SUPPORT STRUCTURE IS CLEAN AND DOES NOT
_______
HAVE ANY SHARP POINTS.
NOTE : The weight of the outboard flap tab is 80kgs (176lbs).
____
1EFF : 301-399, 1 27-54-62Page 496 1 1 May 01/05R 1 1 1CES 1
(a)
Remove the DISTANCE GAUGES from the hinges at the track 3 and the track 4 positions.
(b)
Carefully and slowly lift the tab from the flap.
(c) Move the tab and put it onto the support structure. Subtask 27-54-62-020-061
B. If a replacement tab is to be installed, remove:
-
the tab drive control-rod (13) from the tab at the track 3 position (Ref. Fig. 424/TASK 27-54-62-991-036)
-
the tab drive control-rod (23) from the tab at the track 4 position. (Ref. Fig. 425/TASK 27-54-62-991-037)
(1)
At the track 3 position:
(a)
Remove and discard the cotter pin (4).
(b)
Remove the nut (5) and the washer (3).
(c)
Remove the bolt (1), the washer (2) and remove the tab drive control-rod (13).
(2)
At the track 4 position:
(a)
Remove and discard the cotter pin (24).
(b)
Remove the nut (25) and the washer (26).
(c)
Remove the bolt (21), the washer (22) and remove the tab drive control-rod (23).
1EFF : 301-399, 1 27-54-62Page 497 1 1 May 01/05R 1 1 1CES 1
TASK 27-54-62-400-006
Installation of the Outboard Flap Tab
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 distance gauges No specific pneumatic wrench No specific safety barriers No specific warning notice No specific access platform 3.0 m (9 ft. 10 in.) 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) 98D27504115000 2 DISTANCE GAUGES 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP)
1EFF : 301-399, 1 27-54-62Page 498 1 1 May 01/05R 1 1 1CES 1
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (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)
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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(82)
