(a)
Remove the scale block (20).
(b)
Remove the pin (22) and remove the fin (21) from the base assembly (23).
(c)
Loosen the knurled screws (27) and remove the base assembly (23) from the flap track beam (28).
(3)
Measure the clearance of the flap guide-roller and adjust if necessary (Ref. TASK 27-54-63-400-001).
**ON A/C 001-001,
Subtask 27-51-00-480-061
G. Install the Inboard Flap Rigging Kit
(Ref. Fig. 516/TASK 27-51-00-991-067, 518/TASK 27-51-00-991-068, 523/TASK 27-51-00-991-073)
(1)
Install the PIN RIGGING-FLAPS (TRACK 1) (98D27504005000) (1) in the drive-lever (5) at track 1.
(2)
At the track 1 position install the TOOL RESTRAINING TK1
(98D27504039000).
(a)
Put the body assembly (65) in position on the flap track beam (63).
(b)
Connect the stop (67) to the flap carriage (60).
(c)
Assemble the side-plate (62) and the thumb-nut (61) to the body assembly (65).
R 1EFF : 001-001, 062-099, 106-149, 151-199, 1 27-51-00Page A551 1204-299, 401-499, 1Aug 01/05 1 1 1CES 1
Rigging Kit Installation - Inboard Flap
Figure 523/TASK 27-51-00-991-073- 12 (SHEET 1)
R 1EFF : 001-001, 1 27-51-00Page A552 1 1 Aug 01/05 1 1 1CES 1
Rigging Kit Installation - Inboard Flap
Figure 523/TASK 27-51-00-991-073- 22 (SHEET 2)
R 1EFF : 001-001, 1 27-51-00Page A553 1 1 Aug 01/05 1 1 1CES 1
(d)
Adjust the screw (66) with the knob (64) until the flap carriage
(60)
is held in position.
(3)
At the track 2 position, install the KIT-FLAP RIGGING (98D27504038000):
(a)
Install the base assembly (71) on the flap track beam (76). Make sure that the aft dowels (73) touch the track beam end-stop (72).
(b)
Move the two bottom clamps (74) into position below the flap track beam (76) and tighten the knurled screws (75).
(c)
Move the fin (69) into position on the base assembly (71) and install the pin (70).
(d)
Put the setting block (68) on the fin (69).
(e)
Install the carriage restraint (78) between the base assembly
(71)
and the flap carriage (77). Make sure that the cut-out in the fork-end of the carriage restraint (78) is at the top. This will prevent damage to the greaser.
(f)
Adjust the carriage restraint (78) until it holds the flap carriage (77) in position.
(4)
Disconnect the flap drive-arms (4) and the rotary actuator drive-levers (5) at the track 1 and track 2 position (Ref. TASK 27-54-61-000-001).
(5)
Carefully lower the flap until the trailing edge of the flap touches the setting block (68) on the fin (69).
(6)
Install a LOCK-TORQUE SHAFT (FLAPS AND SLATS) WITH CLAMP-PIVOT (98D27504030001) on the torque shaft inboard (as near as is possible) of the track 3 actuator (Ref. TASK 27-50-00-400-003).
NOTE : This will stop the outboard flap from moving when the track 2
____
drive shaft is disconnected.
(Ref. Fig. 522/TASK 27-51-00-991-072)
(7) Measure and write down the dimension M (the horizontal distance between the outer fixed shroud and trailing edge of the outboard flap).
R 1EFF : 001-001, 1 27-51-00Page A554 1 1 Aug 01/05 1 1 1CES 1
(8) Disconnect the torque shafts at the universal-joints, at the two sides of the flap track 2 actuator (Ref. TASK 27-54-49-000-002).
NOTE : This will let the actuator turn when the rigging pin is
____
removed.
**ON A/C 002-049, 051-061, 101-103, 201-203,
Subtask 27-51-00-480-061-A
G. Install the Inboard Flap Rigging Kit
(Ref. Fig. 518/TASK 27-51-00-991-068, 523A/TASK 27-51-00-991-073-A)
(1)
Install the PIN RIGGING-FLAPS (TRACK 1) (98D27504005000) (1) in the drive-lever (5) at track 1.
(2)
At the track 1 position install the TOOL RESTRAINING TK1
(98D27504039000).
(a)
Put the body assembly (65) in position on the flap track beam (63).
(b)
Connect the stop (67) to the flap carriage (60).
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵4(72)
