(2)
Lift the flap track No. 2 movable fairing (Ref. TASK 57-55-11-410-001).
(3)
Install the pylon aft moveable fairing (Ref. TASK 54-55-00-400-001).
(4)
Install the hinge 1A fairings (Ref. TASK 57-55-11-400-005).
(5)
Install the fairing panels 193AB(194AB) and 193BB(194BB) as follows:
(a) For the fairing panel 193AB(194AB): 1 Put the fairing panel in position on the aircraft.
_
2 Install the attachment screws and washers.
_
(b) For the fairing panel 193BB(194BB): 1 Fully retract the flaps (Ref. TASK 27-50-00-866-009).
_ 2 Put the hook of the sliding panel (3) in position on the flap
_ drive trunnion. Hold the sliding panel (3) in this position.
3 With the sliding panel (3) held in position, align the fairing
_
panel with it.
4 Move the fairing panel onto the sliding panel (3).
_
5 Turn the fairing panel, together with the sliding panel (3),
_ and put it in its installed position on the aircraft. Install the attachment screws.
1EFF : 301-399, 1 27-54-61Page A439 1 1 Aug 01/05R 1 1 1CES 1
(6)
Install the applicable wing access panels:
(a) For the LH wing:
-
install 573CB (Ref. TASK 57-51-37-400-002)
-
install 575AB, 575BB (Ref. TASK 57-51-37-400-004).
(b) For the RH wing:
-
install 673CB (Ref. TASK 57-51-37-400-002)
-
install 675AB, 675BB (Ref. TASK 57-51-37-400-004).
(7)
Extend the flaps (Ref. TASK 27-50-00-866-008) sufficiently to install the rubbing strip (2).
(8) Install the rubbing strip (2) and the support (1). Subtask 27-54-61-820-063
Q. Adjustment of the Inboard Flap to Fuselage Belly-Fairing Seals
(Ref. Fig. 428/TASK 27-54-61-991-025)
(1)
Loosen the screw (247) and adjust the forward seal (246) to the belly-fairing (245) to get dimension X. This must be 33.5 mm (1.3188 in.) -1 mm (0.0393 in.).
(2)
Loosen the screws (249) and (251) and adjust the aft seals (250) to the belly-fairing (248) to get dimension Y. This must be 23.5 mm (0.9251 in.) -1 mm (0.0393 in.).
(3)
TORQUE the screws (247), (249) and (251) to between 0.4 and 0.5 m.daN
(35.39 and 44.24 lbf.in). Subtask 27-54-61-865-057
R. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 6CV, 8CV.
Subtask 27-54-61-710-051
S. Operational 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).
1EFF : 301-399, 1 27-54-61Page A440 1 1 Aug 01/05R 1 1 1CES 1
Adjustment of the Inboard Flap to Fuselage Belly-Fairing Seals
Figure 428/TASK 27-54-61-991-025
1EFF : 301-399, 1 27-54-61Page A441 1 1 Aug 01/05R 1 1 1CES 1
5. Close-up
________ Subtask 27-54-61-942-056
A. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the access platform(s).
(5)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
R 1EFF : 301-399, 1 27-54-61Page A442 1 1 Aug 01/05 1 1 1CES 1
Adjustment of the Track 1 Forward Eccentric
Figure 429/TASK 27-54-61-991-009
INBOARD FLAP - INSPECTION/CHECK_______________________________
TASK 27-54-61-220-001
Dimensional Check of the Joints that Connect the Flap Actuator Levers to the Flap Drive Struts (Tracks 1 and 2)
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.
R R R R R 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__________________
Because the free movement of the inboard flap is more than that in TASK 27-54-00-200-003.
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