(e)
Move the rotary actuator drive-lever from the flap drive arm and remove the packers (84).
(f)
Remove the bushes (85) from the rotary actuator drive-lever.
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Flap to Rotary Actuator Drive-Lever Connection Figure 403/TASK 27-54-61-991-005- 12 (SHEET 1)
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Flap to Rotary Actuator Drive-Lever Connection Figure 403/TASK 27-54-61-991-005- 22 (SHEET 2)
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(10) Hold the trailing edge of the flap by hand and disconnect the rotary
actuator drive-lever at track 2 as follows:
(a)
Remove and discard the cotter pin (89).
(b)
Remove the nut (88) and the washer (87).
(c)
Remove the bolt (86).
(11) Hold the trailing edge and manually extend the inboard flap until the flap carriages rest on the end stops.
(12) Hold the flap on supports at an angle of 20 degrees. R **ON A/C 106-149, 159-199, 211-299, 401-499,
Subtask 27-54-61-020-059-A
B. Preparation for Removal of the Inboard Flap
WARNING : THE INBOARD FLAP WEIGHS 114kgs (251lbs).
_______
CAUTION : OPERATE THE HOIST SLOWLY, WHEN YOU PUT THE SLING IN TENSION. DO
_______ NOT TRY TO REMOVE THE FLAP BECAUSE THIS WILL CAUSE DAMAGE.
(1)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the applicable torque shaft.
(2)
Manually extend the flaps to position 3 (Ref. TASK 27-50-00-866-011).
(3)
Install the LOCK-TORQUE SHAFT LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on the shaft 6220CM (6270CM) (Ref. TASK 27-50-00-400-003).
(4)
Remove the FWD rubbing pad from the fixed shroud adjacent to the outboard cruise roller of the inboard flap.
(5)
Manually extend and lock the spoilers 1 and 2 (Ref. TASK 27-60-00-866-002).
(6)
Install the hoisting sling (Ref. TASK 27-50-00-400-002).
(a) Carefully lift the sling with the hoist until the hoist holds the weight of the flap.
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(7)
Disconnect the inner flap from the rotary actuator drive-levers as follows: (Ref. Fig. 403A/TASK 27-54-61-991-005-B)
(a) Remove the nut (70), the bolt (72) and disconnect the bonding strap (71).
(8)
Remove the nut (73), the bolt (75) and disconnect the bonding strap (74).
(9)
Hold the trailing edge of the flap by hand and disconnect the rotary actuator drive-lever at track 1 as follows:
(a)
Remove and discard the cotter pin (77).
(b)
Remove the nut (76) and washer (78).
(c)
Remove the bolt (79).
(10)
Hold the trailing edge of the flap by hand and disconnect the rotary actuator drive-lever at track 2 as follows:
(a)
Remove and discard the cotter pin (83).
(b)
Remove the nut (82) and the washer (81).
(c)
Remove the bolt (80).
(11)
Hold the trailing edge and manually extend the inboard flap until the flap carriages rest on the end stops.
(12) Hold the flap on supports at an angle of 20 degrees. R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-61-020-050
C. Removal of the Inboard Flap
(Ref. Fig. 404/TASK 27-54-61-991-006)
(1) Disconnect the inboard flap from the track 2 flap track carriage:
(a) Loosen the nuts (184) sufficiently to let the failsafe hook assembly (185) move.
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Flap to Rotary Actuator Drive-Lever Connection
Figure 403A/TASK 27-54-61-991-005-B12 (SHEET 1)
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Flap to Rotary Actuator Drive-Lever Connection
Figure 403A/TASK 27-54-61-991-005-B22 (SHEET 2)
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Flap to Flap Carriage Connection (Track 2)
Figure 404/TASK 27-54-61-991-006
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 418 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵6(20)
