(c)
If there is no gap (between the levers (17) and (27)), apply a load to the outboard end of the inner flap to get a gap of 0.1 mm
(0.004 in.). The load must be applied vertically in line with the lever (27) and must not be more than 20 daN (45 lbf).
(5)
If necessary, remove the bolt (22) and the lever (27).
(6)
Install the lever (27) with the correct thickness of spacer(s) (21) between the levers (17) and (27).
(7)
Install the bolt (22).
(8)
Remove the PIN RIGGING FLAPS (193) at the track 1 position.
(Ref. Fig. 421/TASK 27-54-62-991-042)
(9)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to
extend the flaps to position 1.
(10)
Install the washer (26) and the nut (25) on the bolt (22).
(11)
TORQUE the nut (25) to between 0.9 and 1.0 m.daN (79.64 and 88.49 lbf.in).
(12)
Safety the nut (25) with a new cotter pin (24).
(13)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to retract the flaps to the 0 position.
(14)
Install the remaining spacer(s) (21) above the washer (20) and the nut (19).
(15)
TORQUE the nut (19) to between 3.1 and 3.6 m.daN (22.86 and 26.54 lbf.ft).
(16)
Safety the nut (19) with a new cotter pin (18).
(17)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to extend the flaps to position 1.
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(18)
Install the interconnecting strut to the outboard flap (Ref. TASK 27-
51-44-400-001).
(19)
Use the pneumatic wrench and the ADAPTOR-DRIVE, SLAT (AND FLAP) to retract the flaps to the 0 position.
(20)
Install the PIN RIGGING FLAPS (193) at the track 1 position.
(21)
Remove the ADAPTOR-DRIVE, SLAT (AND FLAP) (98D27804001000).
(22)
Connect the right angle gearbox (Ref. TASK 27-54-41-400-001).
(23)
Remove the PIN RIGGING FLAPS (193) at the track 1 position.
(24)
Extend the flaps to the position 1 (Ref. TASK 27-50-00-866-008).
(25) Install the flap kink seals (Ref. TASK 27-54-61-400-006). Subtask 27-54-62-710-052
N. Test
(1)
Do an operational test of the flap system (Ref. TASK 27-54-00-710-001).
(2)
Do an operational test of the spoiler system (Ref. TASK 27-64-00-710-001).
5. Close-up
________ Subtask 27-54-62-410-054
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Lift the flap track No. 3 and No. 4 movable fairings and adjust if necessary (Ref. TASK 57-55-11-410-002).
(3)
Install the access panels:
(Ref. Fig. 409/TASK 27-54-62-991-021)
-
for the left wing, panels 575AB, 575BB, 573CB
-
for the right wing, panels 675AB, 675BB, 673CB.
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Subtask 27-54-62-942-053
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.
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TASK 27-54-62-000-003
Removal of the Leading Edge Panels 2 and 5 on the Outboard Flap
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.
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
__________________
To get visual access for internal structure.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵6(77)
