50 - 2010 FASCINATION F100


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    Aircraft Summary


    General

    Year
    2010
    Manufacturer
    FASCINATION
    Model
    F100
    Registration #
    50
    Serial Number
    OK-PUF
    Condition
    Used
    Total Time
    620.0
    Number of Seats
    2
    Description
    Fascination is two-seater, cantilever low-wing monoplane with crew sitting side-by-side. The aircraft’s construction is composite, mostly sandwich construction, using either fiberglass or carbon fiber. The wing is tapered, while the main and second spar is made of fiberglass composite. The lift flaps are slotted and tilt to 15 and 30 degrees. The landing gear is three wheeled, either fixed or retractable (electric) with hydraulic disc brakes on the main wheels. The nose wheel is steerable. The tailwing is of classic construction. The fuel tank containing 96 l of gasoline (N95) is integrated in wings. Mor info: http://www.fascination.aero/2014/07/f100-fascination-red/

    Airframe

    Airframe Notes
    The aircraft’s construction is composite, mostly sandwich construction, using either fiberglass or carbon fiber. The wing is tapered, while the main and second spar is made of fiberglass composite.

    Engine

    Engine Notes
    ENGINE Manufacturer: Rotax Type: 912 UL (ULS) 4-stroke, carburetor, boxer Cooling: Liquid and air cooled Max. power: 59 kW (74 kW) Shaft: 5800 rpm Aspirator silencer manufacturer: Rotax Pre-heating carburettor Exhaust manufacturer: Cervinka PROPELLER Manufacturer: Woodcomp s.r.o. Type: Variable pitch SR 3000/2W dual blade

    Props

    Prop Notes
    LANDING GEAR Electrically retractable undercarriage with 6“ low-pressure wheels on the main landing gear. Braked by open hydraulic braking system. Manual emergency opening. Fiberglass landing gear legs. Steerable front landing gear with 4? low-pressure wheel, sprung by rubber block. CONTROLS A central stick controls the wing and tail flaps via cables. Electronically balanced ailerons . Tail rudder controlled by independently-controlled pedals, connected to the rudder by stainless steel cable. Electronically controlled landing flaps.

    Modifications/Conversions

    Modifications/Conversions
    LYMAP LD with autopilot Backup speedometer Winter 61 mm Backup altimeter Winter 61 mm Backup compas CM 24 Radio ICOM A 210 E Preparation for responder SSR Garmin Rescue system Galaxy GRS 6 SD Landing lights Positioning lights Anti colision lights (strobe) Adjustable pedals (foot control) Heated cockpit Pre-heating carburettor 6? main undercarriage wheels, hydraulic brakes Retractable underarriage

    Avionics

    Avionics/Radios
    Airspeed indicator Altimeter Compass Transverse inclinometer Tachometer Oil pressure indicator Oil temperature indicator Engine temperature indicator Gyro horizon GPS navigation Autopilot Glass cockpit

    Additional Equipment

    Additional Equipment
    EMERGENCY SYSTEM Manufacturer: Stratos 07 s.r.o. Type: Magnum 501 HS, located: behind the control panel 4 mm stainless steel cable

    Exterior

    Exterior Notes
    Landing lights Positioning lights Anti colision lights (strobe) 6? main undercarriage wheels, hydraulic brakes Retractable underarriage
    Year Painted
    2010

    Interior

    Interior Notes
    Adjustable pedals (foot control) Heated cockpit Rescue system Galaxy GRS 6 SD FLYMAP LD with autopilot Backup speedometer Winter 61 mm Backup altimeter Winter 61 mm Backup compas CM 24 Radio ICOM A 210 E
    Year Interior
    2010


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