Wingspan (incl. winglets)

21 m

68.9 ft

18 m

59 ft

Wing area

13.2 m²

142 sqft

11.9 m²

128 sqft

Aspect ratio

33.5

27.3

Height of winglet

0.45 m

1.47 ft

0.45 m

1.47 ft

Length of fuselage

7.07 m

23.2 ft

Cockpit width

0.66 m

2.17 ft

Cockpit hight

0.877 m

2.88 ft

Span of tailplane

2.85 m

9.35 ft

Empty mass

430 kg

948 lbs

420 kg

926 lbs

Max. take off weight

700 kg

1543 lbs

630 kg

1389 lbs

Max. wing loading

53 kg/m²

10.8 lbs/sqft

53 kg/m²

10.8 lbs/sqft

Waterballast wing, max.

140 l

308 lbs

120 l

265 lbs

max. pilot weight

115 kg

253 lbs

115 kg

253 lbs

ENGINE:

Type

IAE 50R-AA

single rotary

Engine power

56 hp

41 kW

Engine displacement

294 cm³

Volume of fuselage fuel tank

16 liter

Volume with 2 wing fuel tanks

46 liter

Climb rate

4 m/s

PROPELLER:

Manufacturer

AS

Diameter

1.55 m

5.08 ft

Blades

2