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(6)
Remove the nut (28), the washer (29), the bonding strap (30), the washers (31) and (32) and the bolt (33).
(7)
Disconnect the rear strut (24):
(a)
Remove and discard the cotter pin (19).
(b)
Remove the nut (20) and the washer (21).
(c)
Remove the bolt (26), the washer (25) and disconnect the rear strut (24).
(d)
Remove the sliding bush (27).
(8)
Disconnect the tab at the track 2 position:
(Ref. Fig. 415/TASK 27-54-61-991-029)
(a)
Remove the nut (58), the washer (59), the bolt (61) and disconnect the bonding strap (60).
(b)
Disconnect the tab drive control-rod (73) from the flap track carriage (Ref. TASK 27-54-61-000-003).
(9)
Disconnect the rear strut (53):
(a)
Remove and discard the cotter pin (56).
(b)
Remove the nut (57) and the washer (55).
(c)
Remove the bolt (49), the washer (50) and disconnect the rear strut (53).
(d)
Remove the sliding bush (54).
(10) Remove the eccentric bolt (69): NOTE : Write down the position of the punch marks so that the
____ eccentric bolt (69) can be installed in the same position.
(a)
Remove the nut (67), the washer (66) and the screw (65).
(b)
Remove and discard the cotter pin (62).
(c)
Remove the nut (63) and the washer (64).
(d)
Remove the toothplate (68) and the eccentric bolt (69).
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Inboard Tab Hinge at the Track 2 Position - Location and Detail Figure 415/TASK 27-54-61-991-029
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(11) Remove 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.
NOTE : The weight of the inboard tab is 80kgs (176lbs).
____
(a) Remove the DISTANCE GAUGES from the hinges at the 1A and track 2 positions.
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.
(b) Carefully and slowly lift the tab from the flap. CAUTION : MAKE SURE THAT THE SUPPORT STRUCTURE IS CLEAN AND DOES
_______
NOT HAVE ANY SHARP POINTS.
(12) Move the tab and put it onto the support structure. Subtask 27-54-61-020-062
B. If a replacement tab is to be installed, remove:
-the tab drive control-rod (73) from the tab at the track 2 position. (Ref. Fig. 415/TASK 27-54-61-991-029)
(1) At the track 2 position:
(a)
Remove and discard the cotter pin (70).
(b)
Remove the nut (71) and the washer (72).
(c)
Remove the bolt (74), the washer (75) and remove the tab drive control-rod (73).
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TASK 27-54-61-400-004
Installation of the Inboard 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 pneumatic wrench No specific safety barriers No specific warning notice 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) 98D27504030001 1 LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT 98D27504114000 2 DISTANCE GAUGES 98D27804001000 1 ADAPTOR-DRIVE, SLAT (AND FLAP)
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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(37)
