-
the fuel load is symmetrical or the wing tanks are empty
-
the flaps are fully retracted (Ref. TASK 27-50-00-866-012).
(1)
Install the sharks fin flap rigging kit and do a check of the inboard flap rigged position (Ref. TASK 27-51-00-820-003).
(2)
If necessary, adjust the inboard flap rigged position (Ref. TASK 27-51-00-820-008).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 438 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
Subtask 27-54-61-420-052-A
G. Continue to Connect the Flap Drive Arms
(1)
At the track 1 position:
(Ref. Fig. 403/TASK 27-54-61-991-005)
(a) Safety the flap drive arm to the rotary actuator drive-lever as follows:
(2)
At the track 2 position:
1_ Make sure that the bushes (85), the packers (84), the shear
bolt (80), the washer (81) and the nut (83) are correctly
installed.
2_ TORQUE the nut (83) to between 1.6 and 1.8 m.daN (11.79 and
13.27 lbf.ft).
3_ Safety the nut (83) with a new cotter pin (82).
4_ Install the indicator pin (79), the indicator plate (78), the
washers (77) and the bolts (76).
5_ TORQUE the bolts (76) to between 0.15 and 0.17 m.daN (13.27
and 15.04 lbf.in).
WARNING : CUT, REMOVE AND DISCARD THE LOCKWIRE AS YOU DO THE_______
TASK. LOOSE LOCKWIRE CAN CUT OR BLIND YOU.
6_ Safety the bolts (76) together with MISCELLANEOUS (Material
No. 19-010).
(a) Safety the flap drive arm to the rotary actuator drive-lever as follows:
1 Make sure that the bolt (86), the washer (87) and the nut (88)
_ are correctly installed.
2 TORQUE the nut (88) to between 7.6 and 8.5 m.daN (56.04 and
_
62.68 lbf.ft). 3 Safety the nut (88) with a new cotter pin (89).
_
R 1EFF : 001-049, 051-099, 101-105, 151-158, 1 27-54-61Page 439 1201-210, 1May 01/05 1 1 1CES 1
R **ON A/C 106-149, 213-299, 401-499,
R Subtask 27-54-61-420-052-D
R G. Continue to Connect the Flap Drive Arms
R (1) At the track 1 position:
R (Ref. Fig. 403A/TASK 27-54-61-991-005-B)
R (a) Safety the flap drive arm to the rotary actuator drive-lever as
R follows:
R 1_ Make sure that the bolt (79), the washer (78) and the nut (76)
R are correctly installed.
R 2_ TORQUE the nut (76) to between 7.6 and 8.5 m.daN (56.04 and
R 62.68 lbf.ft).
R 3_ Safety the nut (76) with a new cotter pin (77).
R (2) At the track 2 position:
R (a) Safety the flap drive arm to the rotary actuator drive-lever as
R follows:
R 1_ Make sure that the bolt (80), the washer (81) and the nut (82)
R are correctly installed.
R 2_ TORQUE the nut (82) to between 1.8 and 2.2 m.daN (13.27 and
R 16.22 lbf.ft).
R 3_ Safety the nut (82) with a new cotter pin (83).
R 1EFF : 106-149, 213-299, 401-499, 1 27-54-61Page 440 1 1 Aug 01/05 1 1 1CES 1
R **ON A/C 159-199, 211-212,
Subtask 27-54-61-420-052-C R G. Continue to Connect the Flap Drive Arms
(1) At the track 1 position:
(Ref. Fig. 403A/TASK 27-54-61-991-005-B)
(a) Safety the flap drive arm to the rotary actuator drive-lever as follows:
1 Make sure that the bolt (79), the washer (78) and the nut (76)
_
are correctly installed.
2 TORQUE the nut (76) to between 7.6 and 8.5 m.daN (56.04 and
_
62.68 lbf.ft). 3 Safety the nut (76) with a new cotter pin (77).
_
(2) At the track 2 position:
(a) Safety the flap drive arm to the rotary actuator drive-lever as follows:
1 Make sure that the bolt (80), the washer (81) and the nut (82)
_
are correctly installed.
R 2_TORQUE the nut (82) to between 7.6 and 8.5 m.daN (56.04 and
62.68 lbf.ft). 3 Safety the nut (82) with a new cotter pin (83).
_ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-61-420-073
H. Safety the Inboard Flap Connections
(Ref. Fig. 404/TASK 27-54-61-991-006)
(1) At the track 2 position:
(a)
Make sure that the failsafe hook nuts (184) are hand tight only.
(b)
Remove the nut (174).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 441 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
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