(3) To lock the lifting frame assembly: CAUTION : DO NOT TIGHTEN THE ADJUSTER ASSEMBLIES ON THE LIFTING FRAME
_______ TOO MUCH OR YOU WILL DAMAGE THE AILERON.
 (a) Tighten the adjuster assemblies on the LIFTING FRAME ASSEMBLY (AILERON) to lock the aileron in position.
R **ON A/C 001-003, 051-052,
 Subtask 27-14-41-420-052-B
 D. Installation of the Aileron If the aileron is safetied with STA-LOK nuts, do the steps that follow:
 (1)
 Use the crane to put the aileron in position.

 (2)
 For hinge No.s 1, 2 and 3, do the steps that follow:

 (a)
 Install the GUIDE CONE - AILERON (98D27104000001) on the hinge pin (19). Install the hinge pin (19) with the head outboard. Remove the GUIDE CONE - AILERON.

 (b)
 Make sure that the head of the hinge pin (19) is correctly aligned so that the locking plate (20) can be installed.

 (c)
 Install the STA-LOK nut (27) and the STA-LOK washer (28) as follows:

 (d)
 Install the locking plate (20), the bolt (21) and the nut (22).

 (e)
 Install the bonding strap (25), the washers (24) and (29), the bolt (30) and the nut (23) (Ref. TASK 20-28-00-912-004).

 (3)
 For hinge No.s 4 and 5, do the steps that follow:

 (a)
 Install the GUIDE CONE - AILERON (98D27104000001) on the hinge pin (42). Install the hinge pin (42) with the head outboard. Remove the GUIDE CONE - AILERON.

 (b)
 Make sure that the hinge pin (42) is correctly aligned, so that the locking plate (43) can be installed.

 (c)
 Install the STA-LOK nut (51) and the STA-LOK washer (52) as follows:

 1_ Install the STA-LOK nut (27) with the WRENCHES - NOTCHED,
 TIGHTENING OF NUTS NSA5454 (SL90-315-5625), (Ref. TASK 20-22-
00-400-001).
 2_ TORQUE the nut (27) to between 4.7 and 5.2 m.daN (34.66 and
 38.34 lbf.ft).
 3_ Install the STA-LOK washer (28) with the TOOL - INSTALLATION,
 TAB WASHERS STA-LOK NSA5454 (SL90-313-5625), (Ref. TASK 20-22-
00-400-001).

 1 Install the STA-LOK nut (51) with the WRENCHES - NOTCHED,
_ TIGHTENING OF NUTS NSA5454, (Ref. TASK 20-22-00-400-001).
 2 TORQUE the nut (51) to between 4.7 and 5.2 m.daN (34.66 and
_
 38.34 lbf.ft). 3 Install the STA-LOK washer (52) with the TOOL - INSTALLATION,
_ TAB WASHERS STA-LOK NSA5454, (Ref. TASK 20-22-00-400-001).
 (d)
 Install the locking plate (43) and the bolt (44).

 (e)
 Install the bonding strap (40), the washers (46) and (56), the bolt (45) and the nut (55) (Ref. TASK 20-28-00-912-004).

R 1EFF : 001-003, 051-052, 1 27-14-41Page 426 1 1 May 01/05 1 1 1CES 1

 (4)
 For hinge No. 5, install the bonding strap (49), the washers (48) and (54), the bolt (47) and the nut (53) (Ref. TASK 20-28-00-912-004).

 (5)
 Hold the aileron, loosen the adjuster assemblies and remove the
 LIFTING FRAME ASSEMBLY (AILERON) from the aileron.

 (6)
 Install the flanged bushes (14) in the actuator attachment brackets.

 (7)
 Apply COMMON GREASE (Material No. 04-022) to the threads of the pins (15).

 NOTE : In the step that follows, make sure that you do not get
____ Material No. 15-007 on the servocontrol spherical bearings.
 (8)
 Apply STORAGE PRESERVATION (Material No. 15-007) to the eye-ends of the piston rods on the rounded side only.

 (9)
 Align the eye-ends of the actuators No. 1 and No. 2 with the holes in the actuator attachment brackets. Install the pins (15) with the heads outboard.

 (10)
 Make sure that the heads of the pins (15) are correctly aligned, so that the locking plates (16) can be installed.

 (11)
 Install the STA-LOK nuts (12) and the STA-LOK washers (13) as follows:

 (a)
 Install the STA-LOK nuts (12) with the WRENCHES - NOTCHED, TIGHTENING OF NUTS NSA5454 (SL90-315-7500), (Ref. TASK 20-22-00-400-001).

 (b)
 TORQUE the nuts (12) to between 7.0 and 8.0 m.daN (51.62 and

 58.99 lbf.ft).
 (c) Install the STA-LOK washers (13) with the TOOL - INSTALLATION, TAB WASHERS STA-LOK NSA5454 (SL90-313-7500), (Ref. TASK 20-22-00-400-001).

 (12)
 Install the locking plates (16), the washers (10), the bolts (17) and the nuts (11).

 NOTE : In the steps that follow, make sure that you do not get
____ Material No. 15-007 on the servocontrol spherical bearings.
R 1EFF : 001-003, 051-052, 1 27-14-41Page 427 1 1 May 01/05 1 1 1CES 1
　
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