BRAND and MODEL
MAGNUS FUSION 212
TYPE
Two-seat single-engine light sport monoplane
ORIGIN
Czech Republic
ENGINE
one 75 kw (100 hp) Rotax ULS 2 four-cylinder horizontally-opposed liquid and air cooled engine
SPECIFICATIONS
Wingspan: 8.44 m (27 ft 7 in)
Length: 6.62 m (21 ft 7 in)
Never exceed speed: 280 km/h (174 mph)
Max speed: 241 km/h (150 mph)
Cruising speed: 215 km/h (134 mph)
Stalling speed with flaps – LSA: 83 km/h (52 mph)
Take-off distance: 130 m (426 ft)
Landing distance: 150 m (492 ft)
Service ceiling: 3,650 m (11,975 ft)
Max range: 1,100 km (683 miles)
Fuel capacity: 90 litres (19.8 Imp gals)
Limits:
Cross-wind landing: 37 km/h (23 mph)
Baggage capacity: 20 kg (44 lb)
Loaded weight [LSA]: 600 kg (1,323 lb
PHOTO
Robb Report:Source of phothograph
