R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 002)
**ON A/C 301-399,
(Ref. Fig. 002A)
**ON A/C ALL
(2) Movable fairing
The movable fairing is made of carbon fibre with a honeycomb core. Silicon rubber seals and seal mouldings, which are attached to the top edge of the fairing, touch the wing bottom skin. There is a pivot seal on the forward end which closes the joint between the fixed and movable fairings. The fairing has two pivot mounting brackets which hold bearings and are made of aluminum alloy. Clip-in covers of polyester protect the pivot bolt-heads.
An aluminum alloy platform attaches the flap link connecting rod to the rear of the fairing (Ref. 27-54-00). Aft of the platform there is an aluminum alloy mounting bracket to which a top cover, made of glass fiber with a honeycomb core, is attached. A thermo-plastic tailcone is attached to the aft end of the fairing. It has a static discharger and retainer (Ref. 23-60-00).
**ON A/C 301-399,
C. Flap Tab Hinge Fairings (Ref. 27-50-00)
(1) Inboard hinge (1A) fairing
The inboard hinge, nearest to the wing root, has three main parts:
-
a hinged forward section which is connected to the shroud box
-
a fixed centre section connected to the inboard flap
-
a movable aft section connected to the flap tab and hinge.
(2) Outboard hinge fairings (Ref. 27-50-00)
The other hinge fairings (outboard of hinge 1A) have two main parts:
-
a fixed forward section connected to the flap
-
a movable aft section connected to the flap tab and hinge.
There is one fairing of this type on the inboard flap. All the fairings on the outboard flap are of the 2-section type.
**ON A/C ALL
D. Engine Pylon Aft Fairings
The engine pylon has two aft fairings:
-
the aft fixed fairing which has one attachment point on the bottom surface of the wing at the false rear spar (Ref. 54-54-00)
-
the aft movable fairing which is linked to the inboard flap by a swivel rod (Ref. 54-55-00).
1EFF : ALL 1 57-55-00Page 8 1 1 May 01/05R 1 1 1CES 1
FAIRINGS - DEACTIVATION/REACTIVATION
____________________________________
TASK 57-55-00-040-001
Deactivation of the Flap-Track Fairing
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
__________________
Refer to the CDL TASK: 27-1 Flap Track Fairing To remove the fairing and/or connections from the flap-track beam after a fairing has become damaged or missing.
NOTE : Only one fairing must be removed.
____
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R No specific cable ties No specific safety barriers No specific warning notices No specific adjustable access platform 3.5 m (11 ft. 6 in.)
R 98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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