F. Connect the Flap Drive Arms
(1)
At the track 3 position:
(a)
Connect the flap drive arm to the rotary actuator drive-lever with the bolt (226), the washer (229) and the nut (230).
(b)
TORQUE the nut (230) to between 10.0 and 12.0 m.daN (73.74 and
88.49 lbf.ft).
(c) Safety the nut (230) with a new cotter pin (231).
(2)
At the track 4 position:
(a)
Connect the flap drive arm to the rotary actuator drive-lever with the bolt (226), the washer (229) and the nut (230).
(b)
TORQUE the nut (230) to between 2.5 and 3.3 m.daN (18.43 and
24.33 lbf.ft).
(c) Safety the nut (230) with a new cotter pin (231).
**ON A/C ALL
5. Close-up
________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-54-00-860-061
A. Aircraft Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1)
If applicable, connect the interconnecting strut (Ref. TASK 27-51-44-400-001).
(2)
If applicable, install the flap kink seals (Ref. TASK 27-54-61-400-006).
(3)
If applicable, retract the flaps fully (Ref. TASK 27-50-00-866-009).
**ON A/C 301-399,
Subtask 27-54-00-860-061-A
A. Aircraft Configuration WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROLS ARE
_______ CLEAR. MOVEMENT OF FLIGHT CONTROLS CAN CAUSE INJURY TO PERSONS AND/OR DAMAGE.
(1) Remove the DISTANCE GAUGES (60) and (64) and extend the flap tab by
hand: R (Ref. Fig. 610/TASK 27-54-00-991-020)
(a) At the hinge 1A position: 1 Remove the knurled screw (59) and the forward pin (58).
_
2 Remove the rear pin (61) and the distance gage (60).
_
(b) At the track 2 position: 1 Remove the knurled screw (66) and the forward pin (65).
_ 2 Remove the knurled screw (63), the rear pin (62) and remove
_
the distance gage (64).
(2) If applicable, attach the tab-drive control-rod (46) to the track 2
carriage (41) (inboard flap): R (Ref. Fig. 609/TASK 27-54-00-991-019)
(a)
Install the loose bush (42).
(b)
Move the tab sufficiently to install the tab drive control-rod
(46)
with the bolt (47).
(c)
Install the washer (43) and the nut (45).
(d)
TORQUE the nut (45) to between 0.8 and 1.4 m.daN (70.79 and
123.89 lbf.in).
(e) Safety the nut (45) with the new cotter pin (44).
R 1EFF : 301-399, 1 27-54-00Page A605 1 1 May 01/05 1 1 1CES 1 (3) If applicable, install the tab drive control-rod (22) at the hinge 1A
position (inboard flap): R (Ref. Fig. 608/TASK 27-54-00-991-018)
CAUTION : MAKE SURE THAT THE DISCONNECTED PARTS DO NOT TOUCH AND/OR
_______ CATCH THE ADJACENT STRUCTURE WHEN YOU MOVE THE FLAP. THIS WILL PREVENT DAMAGE TO THE WING.
(a)
Push the tab forward (at the inboard end) until the upper tab drive control-rod (22) is aligned with the bracket (26).
(b)
Install the bolt (27), the washer (28) and the nut (29).
(c)
TORQUE the nut (29) to between 2.2 and 2.4 m.daN (16.22 and 17.69 lbf.ft).
(d)
Safety the nut (29) with the new cotter pin (30).
(4) For the outboard flap, remove the DISTANCE GAUGES (115) and (112) and
extend the flap tab by hand: R (Ref. Fig. 613/TASK 27-54-00-991-022)
(a)
At the track 3 position, release the pins (113) and (114) and remove the distance gage (112).
(b)
At the track 4 position, release the pin (116) and remove the distance gage (115).
(5) If applicable, connect the tab drive control-rod (82) at the track 3
position (outboard flap): R (Ref. Fig. 611/TASK 27-54-00-991-016)
(a)
Install the loose bush (78).
(b)
Connect the control-rod (82) with the bolt (83).
(c)
Install the washer (79) and the nut (81).
(d)
TORQUE the nut (81) to between 1.4 and 2.7 m.daN (10.32 and 19.91 lbf.ft).
(e)
Safety the nut (81) with the new cotter pin (80).
R 1EFF : 301-399, 1 27-54-00Page A606 1 1 May 01/05 1 1 1CES 1 (6) If applicable, connect the tab drive control-rod (97) at the track 4
position (outboard flap): R (Ref. Fig. 612/TASK 27-54-00-991-021)
(a)
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FLIGHT CONTROLS 飛行操縱5
