(b)
Remove the nut (183), the bolt (182) and disconnect the bonding strap from the bracket on the inboard flap.
(c)
Remove and discard the cotter pin (175).
(d)
Remove the nut (174).
(e)
Remove and discard the crushable spacer (176).
(f)
Install the EXTRACTOR - PIN (98D27504084000) onto the carriage bolt (181). (Ref. Fig. 405/TASK 27-54-61-991-013)
NOTE : Make sure that you screw the extractor pin fully onto the
____ threads. This will hold the locking ring in position and let it be compressed by the bushes and bearing. The extractor pin does not cover the locking ring.
(g) Removal of the carriage bolt: CAUTION : THE FLAP TO CARRIAGE BOLT ASSEMBLY HAS AN INNER AND AN
_______
OUTER BOLT WHICH MAKE ONE PART.
DO NOT APPLY AN END OR A TORSION FORCE TO THE INNER
BOLT BECAUSE THIS WILL CAUSE DAMAGE TO THE ASSEMBLY.
APPLY FORCE TO THE OUTER BOLT ONLY WHEN YOU
REMOVE/INSTALL THE BOLT ASSEMBLY.
1_ Remove the carriage bolt (181) using the EXTRACTOR - PIN to
push the carriage bolt (181) through the bushes and bearing.
NOTE : If necessary, carefully lift the flap with the hoist____
and sling sufficiently to release the weight off the
bolts (181).
(h)
Remove the nut (177) and the washer (178).
(i)
Remove the locking plate (179) and the splined bush (180).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 419 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Flap Installation Tool
Figure 405/TASK 27-54-61-991-013
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 420 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-061, 101-103, 201-203,
Subtask 27-54-61-020-051
R D. Continue with the Removal Procedure (Ref. Fig. 406/TASK 27-54-61-991-007, 407/TASK 27-54-61-991-049)
(1) Disconnect the inboard flap from the flap track carriage at the track 1 position:
(a)
Remove the nut (118), the washer (117), the bolt (116) and release the bonding strap (115).
(b)
Remove these items:
-
the bolt (111)
-
the tabwasher (112)
-the retainer (113) R - the locknut (110) using the TORQUE ADAPTOR-TRUNNION NUT R (98D27504035000)
-
the lockwasher (109)
-
the toothplate (108).
(c)
Remove the eccentric bush (107). If necessary, carefully lift the flap with the hoist and the sling to release the weight from the eccentric bush (107).
(d)
Discard the tabwasher (112) and the lockwasher (109).
(2) Remove the flap from the wing:
CAUTION : MAKE SURE THAT THE SUPPORT STRUCTURE IS CLEAN AND DOES NOT
_______
HAVE ANY SHARP POINTS.
CAUTION : MAKE SURE THAT THE FLAP DOES NOT HIT THE AIRCRAFT
_______
STRUCTURE.
(a)
Lift the flap with the hoist until it is clear of the flap track carriage at the track 2 position.
(b)
Move the outboard end of the flap, aft, until it is clear of the wing.
(c)
Pull the flap outboard until the flap drive trunnion is clear of the flap track carriage of the track 1 position.
Flap to Flap Carriage Connection (Track 1)
Figure 406/TASK 27-54-61-991-007
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Flap to Flap Carriage Connection (Track 1)
Figure 406A/TASK 27-54-61-991-007-A
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Flap Drive Trunnion - Detail
Figure 407/TASK 27-54-61-991-049
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(d) Move the flap with the hoist to a flat support structure and lower it onto the support.
(3) Put covers, where necessary, over the disconnected items of the flap.
R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
Subtask 27-54-61-020-051-A
R D. Continue with the Removal Procedure (Ref. Fig. 406A/TASK 27-54-61-991-007-A, 407/TASK 27-54-61-991-049)
(1) Disconnect the inboard flap from the flap track carriage at the track 1 position:
(a) Remove these items:
-
the bolt (111)
-
the tabwasher (112)
-the retainer (113) R - the locknut (110) using the TORQUE ADAPTOR-TRUNNION NUT R (98D27504035000)
-
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