The design was introduced at the AERO Friedrichshafen show in 2007 as a mock up and in 2011 as a flying aircraft.

[1][2][3][4] The Shark was designed with the goal of providing similar performance to other twin-engined light aircraft, but on 30% less power.

It features a cantilever low-wing, a five-seat enclosed cabin, retractable tricycle landing gear and twin wing-mounted engines in tractor configuration.

The wing has an area of 16.2 m2 (174 sq ft) and mounts split flaps that can be extended 50°.

The standard engines fitted are a pair of 160 hp (119 kW) Lycoming O-320-D1A four-stroke powerplants.