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(i)
Remove the PIN RIGGING FLAPS (which was installed for the removal of the actuator) (Ref. TASK 27-54-49-000-001) from the lever (17).
(j)
Remove the nuts (18) from the bolts (2), (3) and (4).
(k)
Remove the bolts (2), (3) and (4) and the cover shell (1).
(l)
Disconnect the No. 1 flap track beam from the aircraft structure at the forward and the rear mountings (Ref. TASK 57-51-33-000-001).
NOTE : This will give sufficient access to remove the
____ flap-actuator lever from the beam.
(m) Remove the lever (17) from the No.1 flap track beam.
Subtask 27-54-55-020-058-A
R B. Removal of the Flap-Actuator Lever Assembly - Track 2 CAUTION : SUPPORT THE FLAP ALONG THE FULL LENGTH OF THE TRAILING EDGE.
_______
THIS WILL PREVENT DAMAGE TO THE FLAP.
(1)
Use the hoisting sling to hold the weight of the inboard flap.
(2)
At the track 1 position:
(Ref. Fig. 401A/TASK 27-54-55-991-001-A)
(a)
Remove and discard the cotter pin (14).
(b)
Remove the nut (15) and the washer (16).
(c)
Remove the bolts (7), the washers (6) and the indicator plate (8).
(d)
Remove the indicator pin (9) and the shearbolt (10).
(e)
Move the flap link arm (5) from the lever (17) and remove the packers (11) and (13).
(f)
Remove the bushes (12) from the lever (17).
(3)
At the track 2 position:
(Ref. Fig. 402/TASK 27-54-55-991-004)
(a) Remove and discard the cotter pin (30).
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R (b) Remove the nut (31), the washer (29) and the bolt (33).
R R (c) Disconnect the lever (28) from the flap link arm (32).
R (d) Lower the inboard flap onto the stops at tracks 1 and 2.
NOTE : The stops only limit the carriage movement, they do not____ prevent flap movement.
R (e) Hold the trailing edge of the inboard flap with an adjustable strut.
R (f) Remove and discard the cotter pin (38).
R (g) Remove the nut (39), the bolt (27) and the retention plate (35).
R (h) Remove the nut (44) and the bolt (25).
R (i) Use the EXTRACTOR-HOUSING (FLAP TRACK RIBS 2, 3 AND 4 INBOARD) (98D27504025000) to remove the bearing housing (26).
R (j) Remove the PIN RIGGING FLAPS (which was installed for the removal of the actuator) (Ref. TASK 27-54-49-000-002) from the lever (28). Move the lever (28) inboard and remove it from the bearing housing (34).
R (k) Turn the lever (28) through 90 deg. and remove it from the brackets (36) on the rear spar.
R (l) Remove and discard the cotter pin (37). Use the SOCKET WRENCH -RETAINER NUT, TRACK 1 to remove the ring nut (40).
R (m) Use the EXTRACTOR - HOUSING (98D27504097000) to remove the bearing housing (34).
R (n) Remove the nuts (41), the bolts (43) and the anti-rotation plate (42).
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R **ON A/C 106-149, 213-299, 401-499,
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱5(167)
