(d)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the joints of the pipes (12) and (20), then install the pressure pipe (20) and the return pipe (12).
(e)
At the pipe brackets near to the inboard and outboard sides of the ASC (21):
1 Assemble the clamp blocks (27) and the tubes (26).
_
R 1EFF : 001-003, 051-052, 1 27-14-51Page 429 1 1 May 01/05 1 1 1CES 1 2 Install the washers (25) and the bolts (24).
_
3 Install the nuts (28).
_
(f)
Attach the clamp blocks (7) to the ASC (21) with the bolts (10) and the washers (9).
(g)
TORQUE the bolts (10) to between 0.16 and 0.20 m.daN (14.15 and
17.69 lbf.in).
(h)
Safety the bolts (10) with MISCELLANEOUS (Material No. 19-010).
(i)
Remove the blanking caps from the electrical connections and connect the electrical connector (11) to the ASC (21).
(j)
Clean the electrical connector (11) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(k)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the electrical connector (11).
(l)
Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the bolt (1), the washer (2) and the nut (3)
-
the STA-LOK washers (4) and (13) and the STA-LOK nuts (5) and
(14)
-
the washers (9) and the bolts (10)
-
the nut (15), the washer (16) and the bolt (17)
-
the head of the pins (19) and (23)
-
the bolts (24), the washers (25) and the nuts (28). NOTE : Do not get Material 15-007 on the Servocontrol Spherical
____
Bearings.
(3) For 33CE3(33CE4), do the steps that follow:
(a) At the rear-spar jack-bracket:
(Ref. Fig. 402/TASK 27-14-51-991-002)
1 Put the locking plate (17) on the pin (18).
_
2 Align and attach the locking plate (17) to the stud (15).
_
3 Install the nut (16).
_
R 1EFF : 001-003, 051-052, 1 27-14-51Page 430 1 1 May 01/05 1 1 1CES 1
(b) At the aileron jack-bracket:
1_ Put the locking plate (21) on the pin (22).
2_ Align the bolt hole in the locking plate (21) 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._______
(c)
Remove the blanking plugs from the disconnected hydraulic connections.
(d)
Apply HYDRAULIC FLUIDS (Material No. 02-003) to the joints of the pipes (12) and (19), then install the pressure pipe (19) and the return pipe (12).
(e)
At the pipe brackets near to the inboard and outboard sides of the ASC (20):
1 Assemble the clamp blocks (25).
_
2 Install the washers (24) and the bolts (23).
_
3 Install the nuts (26).
_
(f)
Attach the clamp blocks (7) to the ASC (20) with the bolts (10) and the washers (9).
(g)
TORQUE the bolts (10) to between 0.16 and 0.20 m.daN (14.15 and
17.69 lbf.in).
(h)
Safety the bolts (10) with MISCELLANEOUS (Material No. 19-010).
(i)
Remove the blanking caps from the electrical connections and connect the electrical connector (11) to the ASC (20).
(j)
Clean the electrical connector (11) with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(k)
Apply a continuous layer of STORAGE PRESERVATION (Material No. 15-008) to the electrical connector (11).
R 1EFF : 001-003, 051-052, 1 27-14-51Page 431 1 1 May 01/05 1 1 1CES 1
(l) Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to:
-
the bolt (1), the washer (2) and the nut (3)
-
the STA-LOK washers (4) and (13) and the STA-LOK nuts (5) and
(14)
-
the washers (9) and the bolts (10)
-
the stud (15) and the nut (16)
-
the head of the pins (18) and (22)
-
the bolts (23), the washers (24) and the nuts (26).
NOTE : Do not get Material 15-007 on the Servocontrol Spherical
____ Bearings.
If the aileron servo control is safetied with ABS 0738 nuts, do the steps that follow:
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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(112)
