_
5 Install the collar (102) and the nut (103).
_
6 TORQUE the nut (103) to between 4.8 and 5.4 m.daN (35.39 and
_
39.82 lbf.ft).
(d) Do a check of the dimension X again.
(3) To align the outboard end of the flap with the outer fixed shroud: (Ref. Fig. 528/TASK 27-51-00-991-078)
(a)
Use a straight-edge to measure the alignment between the outboard flap top surface and the outer fixed-shroud top surface.
(b)
If the dimension is less than 2 mm (0.0787 in.), the position of the outer roller (114) is correct.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page A580 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
Alignment of the Outer Roller of the Outboard Flap
Figure 528/TASK 27-51-00-991-078
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page A581 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 (c) If the dimension is more than 2 mm (0.0787 in.), you must adjust the outer roller (114). To do this:
1_ Remove and discard the cotter pins (111) and (118).
2_ Remove the nut (110) and the washer (112).
3_ Remove the bolt (113) and release the locking plate (116) from
the spigot (115).
4_ Loosen the nut (117) sufficiently to let you turn the spigot
(115).
5_ Turn the spigot (115) until the roller (114) moves the flap
within the specified limits.
6_ Install the locking plate (116).
7_ Install the washer (112) and the nut (110).
8_ TORQUE the nut (110) to between 0.5 and 0.6 m.daN (44.24 and
53.09 lbf.in).
9_ Install the new cotter pin (111).
10__ TORQUE the nut (117) to between 1.3 and 1.4 m.daN (115.04 and
123.89 lbf.in). Make sure that the roller (114) is free to
turn.
11 Install the new cotter pin (118).
__ (Ref. Fig. 518/TASK 27-51-00-991-068)
(4) Remove the rigging pin (1) at the track 1 position. Subtask 27-51-00-420-076
N. Completion of the Flap Connection
(1)
Connect the interconnecting strut to the outboard flap (Ref. TASK 27-54-62-400-001).
(2)
Install the flap kink seals (Ref. TASK 27-54-61-400-006).
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page A582 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 Subtask 27-51-00-710-070
P. Operational Test of the Flap System
(1)
Remove the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER from the flap/slat control lever.
(2)
Do an operational test of the flap system (Ref. TASK 27-54-00-710-001).
5. Close-up
________ Subtask 27-51-00-410-060
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the access panels:
(a) For the LH wing, install:
-573AB, 573CB (Ref. TASK 57-51-37-400-002)
-575AB (Ref. TASK 57-51-37-400-004)
(b) For the RH wing, install:
-673AB, 673CB (Ref. TASK 57-51-37-400-002)
-675AB (Ref. TASK 57-51-37-400-004) Subtask 27-51-00-942-079
B. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-00Page A583 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
**ON A/C 301-399,
TASK 27-51-00-820-009
Adjustment of the Flap Rigged Position With the Sharks Fin Tool (A321)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job__________________
Flap rigging is done:
-
when specified in an AMM Task
- 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(79)
