____ same length. Record the position of the screws as you remove them. This will make sure that they are installed correctly when the fairing panel is installed.
(a)
For the fairing panel 193AB(194AB):
(b)
For the fairing panel 193BB(194BB): 1 Hold the fairing panel and remove the attachment screws.
1_ Hold the fairing panel and remove the attachment screws and
washers.
2_ Remove the fairing panel from the aircraft.
_ 2 Hold the sliding panel (3) in position so that it does not
_ move as the fairing panel is removed.
3 Move the fairing panel rearward, away from the sliding panel
_
(3) and off the aircraft. 4 Remove the sliding panel (3) from the flap trunnion.
_
(8)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the applicable torque shaft.
(9)
Manually extend the flaps to position 1 (Ref. TASK 27-50-00-866-011).
(10)
Install the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT is on the applicable torque shaft.
(11)
Remove the flap kink seals (Ref. TASK 27-54-61-000-002).
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R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
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 27-54-61-020-058
A. Disconnect the Interconnecting Strut
(Ref. Fig. 402/TASK 27-54-61-991-012)
(1)
Remove the electrical connectors (18) and (20) from the connectors
(17) and (19).
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Remove and discard the cotter pin (16) from the nut (15).
(4)
Remove the nut (15) and the washer (14).
(5)
Remove the bolt (11), the washer (12) and the bush (13).
(6)
Hold the interconnecting strut (10) with adhesive tape to the outboard flap.
**ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
Subtask 27-54-61-020-059
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).
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Interconnecting Strut - Location and Detail
Figure 402/TASK 27-54-61-991-012
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(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.
(7) Disconnect the inner flap from the rotary actuator drive-levers as follows: R
(Ref. Fig. 403/TASK 27-54-61-991-005) R
(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 (82).
(b)
Remove the nut (83) and washer (81).
(c)
Remove the bolts (76), the washers (77) and the indicator plate (78).
(d)
Remove the indicator pin (79) and the shear bolt (80).
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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(19)
