MAGNUS FUSION 212


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    Aircraft Summary


    General

    Manufacturer
    MAGNUS
    Model
    FUSION 212
    Condition
    New
    Description
    We designed the Magnus Fusion such a way that it could provide the user with a unique and exceptional flying experience. The Fusion 212 is reliable, economic, comfortable, and affordable. This aircraft is a low-wing monoplane, its symmetrical wing profile provides it with superb aerobatic capabilities. The large control surfaces ensure advanced steerability. Due to its high-strength, carbon fibre and honeycomb structure enforced design, this aircraft can take a load between -3 and +6 G.

    Airframe

    Airframe Notes
    Number of seats: 2 MTOW: 600 kg Fuel: 90 l (95 RON unleaded fuel) Baggage room: 20 kg Length: 6620 mm Wing span: 8440 mm Cabin width: 1170 mm Kabin height: 1080 mm Load: +6 / -3 G Va: 110-113 kts Vhmax: 130 kts Vne: 151 kts Vcr: 116-122 kts Maximum height: 3650 m Landing speed (with brakes released): 45 kts Take-off: 120-130 m Landing: 150 – 200 m Cross-wing landing: 20 kts Distance: 800 – 1100 km Fuel consumption: 16 – 21 l/hr

    Engine

    Engine Notes
    ROTAX 912 ULS 2 (100 hp)

    Props

    Prop Notes
    DUC Inconel Flash 3 Blades

    Avionics

    Avionics/Radios
    12V Electric System, Alternate Normal 2-1/4" instruments (Airspeed, Altimeter), AVEO PowerBurst Led wingtip lights (NAV/Strobe/Pos), DYNON Pitot/AOA System, Dynon Skyview System 10" ( 2 displays), VHF 25khz, Electrical Trim, ELT, Flybox electronic flaps controller, NVFR Set, Transponder S mode

    Additional Equipment

    Additional Equipment
    JUNKERS Magnum 601 Ballistic Recovery System

    Interior

    Interior Notes
    4-point seat belts, Adjustable Pedals, Carpet, Dual Control System, Leather Seat Covers, Leather Upholstery, Simple cabin heating


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