-
for 33CE3(33CE4), the pins (22) and (26).

 Subtask 27-14-51-420-058-A R C. Complete the Installation of the Aileron Servo Control (ASC)
 (1) For 33CE1(33CE2), do the steps that follow:
 (Ref. Fig. 401A/TASK 27-14-51-991-001-A)

 (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 (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: 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.
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 3 Install the bolt (21), the washer (20) and the nut (19).
_
 (f)
 At the aileron jack-bracket:

 (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):

 1_ Put the locking plate (26) on the pin (27).
 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).

 1 Assemble the clamp blocks (31) and the tubes (30).
_
 2 Install the washers (29), the bolts (28) and the nuts (32).

_

 (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

 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).

 NOTE : In the step that follows, make sure that you do not get
____ Material No. 15-007 on the servocontrol spherical bearings.
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 (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).

 (2) For 33CE3(33CE4), do the steps that follow:
 (Ref. Fig. 402A/TASK 27-14-51-991-002-A)

 (a)
 Install the washers (7) and (18) and the nuts (6) and (17).

 (b)
 TORQUE the nuts (6) and (17) to 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.
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