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.
|Wing span:||8440 mm|
|Cabin width:||1170 mm|
|Kabin height:||1080 mm|
|Number of seats:||2|
|Fuel:||90 l (95 RON unleaded fuel)|
|Baggage room:||20 kg|
|Landing speed (with brakes released):||45 kts|
|Landing:||150 – 200 m|
|Cross-wing landing:||20 kts|
|Distance:||800 – 1100 km|
|Fuel consumption:||16 – 21 l/hr|
|Load:||+6 / -3 G|
|Maximum height:||3650 m|
|4-point seat belts, Adjustable Pedals, Carpet, Dual Control System, Leather Seat Covers, Leather Upholstery, Simple cabin heating|
|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|
|6" wheels, Castor type nose gear, Differential Brakes, Parking Brake|
|JUNKERS Magnum 601 Ballistic Recovery System|
|ROTAX 912 ULS 2 (100 hp)|
|DUC Inconel Flash 3 Blades|
The Fusion 212 of Magnus, due to its side by side seat placement and its duplicable control system, is ideal for instruction. Thanks to its Rotax engine, fuelled by 95 RON unleaded petrol, and the composite fuselage, the owner can use the energy and cost that would be devoted to maintenance and fuel for other purposes. This is possible due to the fact that the fuel consumption of the Fusion is 16–21 l/hour.
The built-in ballistic recovery system connected to the aircraft at three points, can protect the whole aircraft in case of an emergency, largely decreasing the likelihood of accidents and improving flight security. Thanks to its symmetrical wing profile, the aircraft ensures a stable but dynamic flight experience at the same time. Besides these, the aircraft, due to its structural design, can easily bear a load of +6/-3 G, thus it is suitable for performing the basic aerobatics maneuvers.
Thanks to its light construction, it has a large, up to 1200 km range; for take-off, only 120 metres, and for landing, only 150 metres are necessary. Last, but not least, the panoramic cabin rooftop provides an even more intense flight experience.