(c)
Make sure that the spherical bearing, the splined bush (180) and the locking plate (179) are engaged correctly.
(d)
Install a new crushable spacer (176) and the nut (174).
(e)
TORQUE the nut (174) to between 15 and 20 m.daN (110.61 and
147.49 lbf.ft).
(f) Safety the nut (174) with a new cotter pin (175).
(g) Install the washer (178) and the nut (177).
Subtask 27-54-61-220-055-A
J. Do a Check of the Flap Rigged Position
(1) Make sure that the inboard flap remains in the correct rigged position (Ref. TASK 27-51-00-820-003).
Subtask 27-54-61-420-074
K. Continue to Safety the Inboard Flap Connections
**ON A/C 001-049, 051-061, 101-103, 201-203,
(Ref. Fig. 406/TASK 27-54-61-991-007) R **ON A/C 062-099, 104-149, 151-199, 204-299, 401-499,
(Ref. Fig. 406A/TASK 27-54-61-991-007-A) R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(1) At the track 1 position:
(a)
TORQUE the locknut (110) using the TORQUE ADAPTOR-TRUNNION NUT (98D27504035000) to between 5.4 and 7.0 m.daN (39.82 and 51.62 lbf.ft).
(b)
Lock the locknut (110) with the lockwasher (109).
(c)
Apply a layer of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004A) to the retainer (113).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 442 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(d)
Install the retainer (113), the tabwasher (112) and the bolt (111).
(e)
TORQUE the bolt (111) to between 1.0 and 1.5 m.daN (88.49 and
132.74 lbf.in) and safety with the tabwasher (112).
(2) At the track 2 position:
(a) TORQUE the nuts (184) to 0.12 m.daN (10.61 lbf.in) maximum.
(b)
Safety the nuts (184) with MISCELLANEOUS (Material No. 19-010). Subtask 27-54-61-820-068
L. Completion of the Flap Rigging Procedure
(1)
Complete the flap rigging procedure (Ref. TASK 27-51-00-820-008). **ON A/C 001-001,
Subtask 27-54-61-220-051
M. Alignment of the Outboard Cruise Roller of the Inboard Flap
(Ref. Fig. 408/TASK 27-54-61-991-008)
(1)
Measure the dimension Y. This must be 8.0 mm (0.3149 in.) minus the dimension X, plus or minus 0.5 mm (0.0196 in.). If the dimension Y is not correct you must adjust the cruise roller.
(2)
To adjust the cruise roller:
(a)
Remove the nut (123), the collar (122) and the serrated plate (124).
(b)
Turn the eccentric (125) until the dimension Y is correct.
(c)
Lock the eccentric (125) with the serrated plate (124).
(d)
Install the collar (122) and the nut (123).
(e)
TORQUE the nut (123) to between 4.8 and 5.4 m.daN (35.39 and
39.82 lbf.ft).
(3)
Measure the dimension Y again.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 443 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
(4) Measure and record the clearance between the bottom surface of the shroud box and the flap upper surface (measured at the outboard end of the shroud box). This must be between 5 mm (0.1968 in.) and 12 mm (0.4724 in.).
R **ON A/C 002-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-61-220-051-A
M. Alignment of the Outboard Cruise Roller of the Inboard Flap
(Ref. Fig. 408/TASK 27-54-61-991-008)
(1)
Measure the dimension Y. This must be 6.0 mm (0.2362 in.) minus the dimension X, plus or minus 0.5 mm (0.0196 in.). If the dimension Y is not correct you must adjust the cruise roller.
(2)
To adjust the cruise roller:
(a)
Remove the nut (123), the collar (122) and the serrated plate (124).
(b)
Turn the eccentric (125) until the dimension Y is correct.
(c)
Lock the eccentric (125) with the serrated plate (124).
(d)
Install the collar (122) and the nut (123).
(e)
TORQUE the nut (123) to between 4.8 and 5.4 m.daN (35.39 and
39.82 lbf.ft).
(3)
Measure the dimension Y again.
(4)
Measure and record the clearance between the bottom surface of the shroud box and the flap upper surface (measured at the outboard end of the shroud box). This must be between 5 mm (0.1968 in.) and 12 mm (0.4724 in.).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-54-61Page 444 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 001-049, 051-099, 101-105, 151-158, 201-210,
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱6(27)
