Technical Specifications

Engine Rotax 912 ULS2
Power 100 HP (73.5Kw) at 5800 RPM
Fuel Mogas RON 95, Avgas 100 LL, EN 228
Propeller Sensenich Fixed 3-blade (*)
Wingspan 28.22 ft (8.6 m)
Length 21.72 ft (6.62 m)
Height 7.60 ft (2.315 m)
Wing surface area 132.4 sq ft (12.3 m²)
Cockpit width 3.85 ft (1.17 m)
MTOW 1,320 lbs (600 kg)
Empty weight 855.4 lbs (388 kg)
Max. baggage weight in cockpit compartment 40 lbs (18 kg)
Max. baggage weight in each wing locker 22 lbs (10 kg)
Cruise speed at 3,000 ft and 75% power 93 KIAS (172 km/h)
Max. horizontal speed 119 KIAS (220 km/h)
VNE 138 KIAS (255 km/h)
Stall speed VS0 31 KIAS (55 km/h)
Climb rate 825 ft/min (4.2 m/s)

Take-off distance to 50 ft (15 m)

Concrete 1,270 ft (387 m)
Grass 1,499 ft (457 m)

Braking distance

Concrete 479 ft (146 m)
Grass 364 ft (111 m)
Range (30 min. reserve) 516 NM (953 km)
Endurance 5 hours 25 min
Fuel capacity 30 US Gal. (114 l)
Average fuel consumption 4.6 US Gal./Hour (17.5 l/h)