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Technical Data

Specification

Testing of two (late stage) prototype aircraft, with UL Power 520is 200 hp engines and Sensenich 3-blade ground-adjustable propellers, set for spring/summer 2014.
Rapid-build kit version of the aircraft (FAA Experimental) is contemplated for release in 2015.
Airframe is constructed of carbon-composite structure providing high fatigue and corrosion resistance.
Hydraulic-actuated tricycle landing gear that can be deployed and retracted in the water.
Retractable water rudder assists maneuvering at slow speed.
Glass panel including Aspen and Garmin avionics included in prototype version. Kit version to have basic VFR instruments with docking capability for portable GPS.

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
(Provisional weight/load factors)
Max. load: 67 kg/sq m / 147 lbs/ sq ft
MTOW: 800 kg/1760 lbs
Fuel: 150 l / 39 gal

Performance (estimated)

Vr : 60 km/h | 35 kts
Vc : 185 km/h | 100 kts
Vne : 230 km/h | 124 kts
Vso: 68 km/h | 37 kts
Vs1 (clean): 82 km/h | 45 kts
Range: 1300 km | 700 nm

*Note: all factors provisional; to be revised following flight testing.

 

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