(2)
Put a warning notice in position in the cockpit to tell persons not to operate the flight controls.
(3)
Put a warning notice on panel 400VU to tell persons not to operate the landing gear.
Subtask 27-54-61-860-055
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 that the flaps are in the fully retracted position (Ref. TASK 27-50-00-866-009).
(2)
Make sure that the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) is on the slat/flap control lever.
(3)
Disconnect the applicable torque shaft from the right angle gearbox (Ref. TASK 27-54-41-000-001).
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(4) Make sure that the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) is on the applicable torque shaft.
Subtask 27-54-61-865-054
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 27-54-61-010-053
D. Get Access
(1)
Put the access platform in position below the applicable inboard flap tab.
(2)
Remove the fairings from the tab hinges at the 1A and 1B positions (Ref. TASK 57-55-11-000-005).
(3)
Lower the flap track No. 2 movable fairing (Ref. TASK 57-55-11-010-001).
4. Procedure
_________
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.
Subtask 27-54-61-020-057
A. Removal of the Inboard Flap Tab
(Ref. Fig. 413/TASK 27-54-61-991-028)
(1) Install the DISTANCE GAUGES (98D27504114000) on the flap and tab hinges at the hinge 1A and the track 2 positions (Ref. TASK 27-54-61-000-003).
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Inboard Tab Hinge at the 1B Position - Location and Detail
Figure 413/TASK 27-54-61-991-028
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(2)
Disconnect the tab at the hinge 1B position:
(a) Disconnect the rear strut (5):
(3)
Disconnect the forward strut (18):
(a)
Remove and discard the cotter pin (15).
(b)
Remove the nut (14) and the washer (13).
(c)
Remove the bolt (10), the washer (11) and disconnect the forward strut (18).
(d)
Remove the sliding bush (12).
(4)
Disconnect the tab at the hinge 1A position: (Ref. Fig. 414/TASK 27-54-61-991-027)
1_ Remove and discard the cotter pin (8).
2_ Remove the nut (9) and the washer (7).
3_ Remove the bolt (1), the washer (2) and disconnect the rear
strut (5).
4_ Remove the sliding bush (6).
(a) Disconnect the tab drive control-rod (45): 1 Remove and discard the cotter pin (46).
_
2 Remove the nut (47) and the washer (48).
_
3 Remove the bolt (42), the washer (43) and disconnect the tab
_ drive control-rod (45).
4 Remove the sliding bush (44).
_
(5) Disconnect the forward strut (39):
(a)
Remove and discard the cotter pin (34).
(b)
Remove the nut (35) and the washer (36).
(c)
Remove the bolt (40), the washer (41) and disconnect the forward strut (39).
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Inboard Tab Hinge at the 1A Position - Location and Detail
Figure 414/TASK 27-54-61-991-027
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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(36)
