(b)
TORQUE the nuts (6) and (17) to between 7.5 and 8.0 m.daN (55.30 and 58.99 lbf.ft).
(c)
Install the locking caps (5) and (16) on the pins (27) and (23).
(d)
Safety the items that follow:
-
the locking cap (5) with the new cotter pin (4)
-
the locking cap (16) with the new cotter pin (15).
(e)
At the rear-spar jack-bracket:
(f)
At the aileron jack-bracket: 1 Put the locking plate (26) on the pin (27).
1_ Put the locking plate (22) on the pin (23).
2_ Align the bolt hole in the locking plate (22) with the holes
in the flanges of the rear-spar jack-bracket.
3_ Install the bolt (21), the washer (20) and the nut (19).
_ 2 Align the bolt hole in the locking plate (26) with the hole in
_
the flange of the aileron jack-bracket. 3 Install the bolt (1), the washer (2) and the nut (3).
_
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(g)
Remove the blanking plugs from the disconnected hydraulic connections.
(h)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the joints of the pipes (14) and (24), then install the pressure pipe (24) and the return pipe (14).
(i)
At the pipe brackets near to the inboard and outboard sides of the ASC (25):
(j)
Attach the clamp blocks (9) to the ASC (25) with the bolts (12) and the washers (11).
(k)
TORQUE the bolts (12) to between 0.16 and 0.20 m.daN (14.15 and
1_ Assemble the clamp blocks (31) and the tubes (30).
2_ Install the washers (29) and the bolts (28).
3_ Install the nuts (32).
17.69 lbf.in).
(l)
Safety the bolts (12) with MISCELLANEOUS (Material No. 19-010).
(m)
Remove the blanking caps from the electrical connections and connect the electrical connector (13) to the ASC (25).
(n)
Clean the electrical connector (13) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(o)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the electrical connector (13).
(p)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the bolt (1), the washer (2) and the nut (3)
-
the cotter pin (4), the locking cap (5), the nut (6) and the washer (7)
-
the washers (11) and the bolts (12)
-
the cotter pin (15), the locking cap (16), the nut (17) and the washer (18)
-
the nut (19), the washer (20) and the bolt (21)
-
the head of the pins (23) and (27)
-
the bolts (28), the washers (29) and the nuts (32).
NOTE : Do not get Material 15-007 on the Servocontrol Spherical
____ Bearings.
R 1EFF : 001-003, 051-052, 1 27-14-51Page 433 1 1 May 01/05 1 1 1CES 1
(5) For 33CE3(33CE4), do the steps that follow:
(Ref. Fig. 402/TASK 27-14-51-991-002)
(a)
Install the washers (7) and (18) and the nuts (6) and (17).
(b)
TORQUE the nuts (6) and (17) to between 7.5 and 8.0 m.daN (55.30 and 58.99 lbf.ft).
(c)
Install the locking caps (5) and (16) on the pins (26) and (22).
(d) Safety the items that follow: R - the locking cap (5) with the new cotter pin (4) R - the locking cap (16) with the new cotter pin (15).
(e) At the rear-spar jack-bracket: 1 Put the locking plate (21) on the pin (22).
_
2 Align and attach the locking plate (21) to the stud (19).
_
3 Install the nut (20).
_
(f) At the aileron jack-bracket: 1 Put the locking plate (25) on the pin (26).
_ 2 Align the bolt hole in the locking plate (25) with the hole in
_ the flange of the aileron jack-bracket.
3 Install the bolt (1), the washer (2) and the nut (3).
_ WARNING : OBEY THE HYDRAULIC SAFETY PROCEDURES.
_______
(g)
Remove the blanking plugs from the disconnected hydraulic connections.
(h)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the joints of the pipes (14) and (23), then install the pressure pipe (23) and the return pipe (14).
(i)
At the pipe brackets near to the inboard and outboard sides of the ASC (24):
1 Assemble the clamp blocks (29).
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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(113)
