(d)
Lock the nut (83) with the lockwasher (84).
(e)
Apply a layer of BONDING AND ADHESIVE COMPOUNDS (Material No. 08-004A) to the stop (82).
(f)
Install the stop (82), the tabwasher (81) and the bolt (80).
(g)
TORQUE the bolt (80) to between 1.0 and 1.5 m.daN (88.49 and
132.74 lbf.in).
(h) Lock the bolt (80) with the tabwasher (81).
(2) At the track 2 position:
(a) On the carriage bolt (58) install these items:
-the locking plate (51) (make sure that the main eccentric bearing, the splined bush and the locking plate (51) are correctly engaged)
-a new crushable spacer (52)
-the nut (53).
(b)
TORQUE the nut (53) to between 15 and 20 m.daN (110.61 and 147.49 lbf.ft).
(c)
Safety the nut (53) with a new cotter pin (54).
(d)
Install the washer (56) and the nut (55).
(e)
TORQUE the nuts (57) on the failsafe hooks to between 2.5 and 3.3 m.daN (18.43 and 24.33 lbf.ft).
(f)
Safety the nuts (57) with MISCELLANEOUS (Material No. 19-010).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page A574 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 **ON A/C 001-001,
Subtask 27-51-00-820-068
L. Completion of the Flap Rigging Procedure
(Ref. Fig. 518/TASK 27-51-00-991-068, 523/TASK 27-51-00-991-073)
(1)
At the track 1 position, complete the installation of the flap drive levers (4) and (5) (Ref. TASK 27-54-61-400-001).
(2)
Connect the torque shaft universal-joint at the two sides of the track 2 actuator (Ref. TASK 27-54-49-400-002).
NOTE : It is possible that the rigging pin (2) cannot now be
____ installed at the track 2 position. When the flaps are in the correct rigged position, you must not install the rigging pin.
(3)
At the track 1 position, remove the TOOL RESTRAINING TK1 from the flap track 1 beam as follows:
(a)
Remove the thumb-nut (61) and the side-plate (62) from the body assembly (65).
(b)
Disconnect the stop (67) from the flap carriage (60).
(c)
Remove the body assembly (65) from the flap track beam (63).
(4)
At the track 2 position, remove the KIT-FLAP RIGGING from the flap track beam as follows:
(a)
Remove the carriage restraint (78).
(b)
Remove the setting block (68) from the fin (69).
(c)
Remove the pin (70) and remove the fin (69) from the base assembly (71).
(d)
Loosen the knurled screws (75) and remove the base assembly (71) from the flap track beam (76).
(Ref. Fig. 522/TASK 27-51-00-991-072)
R 1EFF : 001-001, 1 27-51-00Page A575 1 1 Aug 01/05 1 1 1CES 1
(5)
Measure the dimension M again (between the outboard flap and the outer fixed shroud) and compare it with the one you recorded before the torque shafts were disconnected.
(a)
If the dimension M has changed, disconnect the torque shaft universal-joint outboard of the flap track 2 actuator (Ref. TASK 27-54-49-000-002).
(b)
Loosen the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT at the track 3 position.
(c)
Turn the torque shaft until the dimension M is correct.
(d)
Connect the torque shaft universal-joint outboard of the track 2 actuator (Ref. TASK 27-54-49-400-002).
(6)
Remove the LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT from the torque shaft at the track 3 position (Ref. TASK 27-50-00-000-003).
(7)
Remove the rigging pin (1) at the track 1 position.
(8)
Install the adaptor drive on the gearbox.
(9)
Use the pneumatic wrench to turn the adaptor drive and fully extend and retract the flaps. Make sure that the flaps operate correctly.
(10) Install the rigging pin (1) at the track 1 position. **ON A/C 002-049, 051-061, 101-103, 201-203,
Subtask 27-51-00-820-068-B
L. Completion of the Flap Rigging Procedure (Ref. Fig. 518/TASK 27-51-00-991-068, 523A/TASK 27-51-00-991-073-A)
(1)
At the track 1 position, complete the installation of the flap drive levers (4) and (5) (Ref. TASK 27-54-61-400-001).
(2)
At the track 1 position, remove the TOOL RESTRAINING TK1 from the flap track 1 beam as follows:
(a) Remove the thumb-nut (61) and the side-plate (62) from the body assembly (65).
R 1EFF : 001-049, 051-061, 101-103, 201-203, 1 27-51-00Page A576 1 1 Aug 01/05 1 1 1CES 1
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵4(77)
