MAGNUS FUSION 212
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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