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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

40 lbs (18 kg)

Max. baggage weight in each wing lockerkg

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)

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