-
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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