_
2 Remove the locking plate (26).
_
(e) At the rear-spar jack-bracket: 1 Remove the nut (19), the washer (20) and the bolt (21).
_
2 Remove the locking plate (22).
_
(15) For 33CE3(33CE4), do the steps that follow:
(a) At the pipe brackets near to the inboard and outboard sides of the ASC:
1 Remove the nuts (30), the bolts (27) and the washers (28).
_
R 1EFF : 001-003, 051-052, 1 27-14-51Page 414 1 1 May 01/05 1 1 1CES 1 2 Disassemble and remove the clamp blocks (29).
_
(b)
Disconnect and remove the return pipe (14) and the pressure pipe (23).
(c)
Put blanking plugs or caps on the ASC hydraulic connections and the disconnected line ends.
(d)
At the aileron jack-bracket: 1 Remove the nut (3), the washer (2) and the bolt (1).
_
2 Remove the locking plate (25).
_
(e) At the rear-spar jack-bracket:
1 Remove the nut (20).
_
2 Remove the locking plate (21) from the stud (19).
_
(16)
Remove and discard the cotter pins (4) and (15) from the locking caps
(5) and (16).
(17)
Remove the locking caps (5) and (16), the nuts (6) and (17) and the washers (7) and (18).
Subtask 27-14-51-020-050
B. Complete the Removal of the Aileron Servo-Control (ASC)
If the aileron servo control is safetied with STA-LOK nuts, do the steps that follow:
(1) To decrease the length of the piston rod:
(a)
For 33CE1(33CE2), manually move the aileron to the down position.
(b)
Hold the ASC (21) (7.4 kg (16.3142 lb)) and remove the pin (23).
(c)
Manually move the aileron to the fully up position.
(d)
Safety the aileron in this position if the other ASC is not installed, and remove the pin (19).
(e)
Remove the ASC (21) from the aircraft.
(f)
For 33CE3(33CE4), manually move the aileron to the down position.
R 1EFF : 001-003, 051-052, 1 27-14-51Page 415 1 1 May 01/05 1 1 1CES 1
(g)
Hold the ASC (20) (7.4 kg (16.3142 lb)) and remove the pin (22).
(h)
Manually move the aileron to the fully up position.
(i)
Safety the aileron in this position if the other ASC is not installed, and remove the pin (18).
(j)
Remove the ASC (20) from the aircraft.
(2)
Remove the flanged bushes (6) and (8).
(3)
Install these parts on the removed ASC:
-
the clamp blocks (7)
-
the washers (9)
-
the bolts (10).
NOTE : The clamp blocks (7), the washers (9) and the bolts (10) must
____
stay with the removed ASC.
If the aileron servo control is safetied with ABS 0738 nuts, do the steps that follow:
(4)
To decrease the length of the piston rod:
(a)
For 33CE1(33CE2), manually move the aileron to the down position.
(b)
Hold the ASC (25) (7.4 kg (16.3142 lb)) and remove the pin (27).
(c)
Manually move the aileron to the fully up position.
(d)
Safety the aileron in this position if the other ASC is not installed, and remove the pin (23).
(e)
Remove the ASC (25) from the aircraft.
(f)
For 33CE3(33CE4), manually move the aileron to the down position.
(g)
Hold the ASC (24) (7.4 kg (16.3142 lb)) and remove the pin (26).
(h)
Manually move the aileron to the fully up position.
(i)
Safety the aileron in this position if the other ASC is not installed, and remove the pin (22).
(j)
Remove the ASC (24) from the aircraft.
(5)
Remove the flanged bushes (8) and (10).
R 1EFF : 001-003, 051-052, 1 27-14-51Page 416 1 1 May 01/05 1 1 1CES 1
(6) Install these parts on the removed ASC:
-
the clamp blocks (9)
-
the washers (11)
-
the bolts (12).
NOTE : The clamp blocks (9), the washers (11) and the bolts (12) must
____
stay with the removed ASC.
R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
Subtask 27-14-51-020-062-A
A. Removal of the Aileron Servo Control (ASC)
(1)
Manually put and hold the aileron in the fully-up position.
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱1(107)
