_

 3 Install the nuts (30).
_
 (j)
 Attach the clamp blocks (9) to the ASC (24) 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 (24).

 (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 stud (19) and the nut (20)

 -
the head of the pins (22) and (26)

 -
the bolts (27), the washers (28) and the nuts (30).

 NOTE : Do not get Material 15-007 on the Servocontrol Spherical
____
 Bearings.

R **ON A/C 004-049, 053-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 27-14-51-420-059-A
 A. Preparation for Installation
 (1)
 Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026):

 -
for 33CE1(33CE2), the pins (23) and (27)

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

 -
the flanged bushes (8) and (10)

 -
the interfaces of the aileron and rear-spar jack-brackets.

 (2)
 Make sure that the parts retained from the removed component are clean and in the correct condition.

 (3)
 Do an inspection of the component interface and/or the adjacent area.

 (4)
 Make sure that the hydraulic line end-fittings are serviceable.

 (5)
 Lubricate these parts with SPECIAL MATERIALS (Material No. 05-002):

 -
for 33CE1(33CE2), the pins (23) and (27)

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

 -
the flanged bushes (8) and (10)

 -
the installed bushes in the outboard-flanges of the aileron and rear-spar jack-brackets.

 Subtask 27-14-51-420-050-A
 B. Installation of the Aileron Servo Control (ASC)
 (1)
 Install the flanged bushes (8) and (10) into the inboard-flanges of the aileron and rear-spar jack-brackets.

 (2)
 Apply a layer of STORAGE PRESERVATION (Material No. 15-007) to the eye-ends of the piston rods on the rounded sides only.

 NOTE : Do not get Material 15-007 on the Servocontrol Spherical
____
 Bearings.

 (3) For 33CE1(33CE2), install the ASC (25):
 (a)
 Hold the ASC (7.4 kg (16.3142 lb)) in a horizontal position.

 (b)
 Align the body eye-end with the bushes in the flanges of the rear-spar jack-bracket.

 (c)
 Install the pin (23).

 (d)
 Manually move the aileron to the down position. Do this until the piston-rod eye-end and the bushes of the aileron jack-bracket are aligned.

 (e)
 Install the pin (27).

R 1EFF : 004-049, 053-099, 101-149, 151-199, 1 27-14-51Page 436 1201-299, 301-399, 401-499, 1Aug 01/05 1 1 1CES 1

 (4)
 For 33CE3(33CE4), install the ASC (24):

 (a)
 Hold the ASC (7.4 kg (16.3142 lb)) in a horizontal position.

 (b)
 Align the body eye-end with the bushes in the flanges of the rear-spar jack-bracket.

 (c)
 Install the pin (22).

 (d)
 Manually move the aileron to the down position. Do this until the piston-rod eye-end and the bushes of the aileron jack-bracket are aligned.

 (e)
 Install the pin (26).

 (5)
 For easier access to the installed ASC manually, put and hold the aileron in the fully-up position.

 (6)
 Apply COMMON GREASE (Material No. 04-022) to the threads of the pins:

 -
for 33CE1(33CE2), the pins (23) and (27)
　
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