TECHNICAL DATA

Specification

• VLA and LSA-Class certification (in progress, expected in summer 2009)
• Glass and carbon-composite structure providing high fatigue and corrosion resistance

• Main wing can be rotated 90 degrees for easy transport

• Electric driven tricycle landing gear that can be deployed and retracted in the water

• Electric driven fowler-flaps up to 30 degress – STOL-capability and good slow-flight behavior

• Water rudder assists maneuvering at slow speed


Dimensions
Seats: 2
Span: 9.0m/29.5ft
Length: 6.75m/22.1ft
Height: 2.1m/6.9ft
Wing area: 12 sq.m / 129 sq. ft
Max. load: 54 kg/sq m / 111 lbs/ sq ft
Weight: 480kg/1056 lbs
MTOW: 800 kg/1760 lbs
Fuel: 150 l / 39 gal


Performance (Rotax 912S, 100HP)
Vr : 60 km/h | 35 kts
Vc : 185 km/h | 100 kts
Vne : 230 km/h | 124 kts
Nso: 68 km/h | 37 kts
Vs1 (clean): 82 km/h | 45 kts
Climb rate: 3.77 m/s | 700 ft/min*
Range: 1300 km | 700 nm
TO-Distance (land/sea): 100 m | 130 m*
LDG-Distance (land/sea): 90 m | 110 m*



Notes:
* - preliminary