Glass-fibre and carbonfibre/epoxy airframe, with PVC foam and aramid honeycomb core in sandwich panels. Monocoque fuselage with integral fin has integrated arm rests, seat backs, floors and instrument panels. Composite wing with carbon-fibre main spar and an auxiliary spar carrying flap levers and aileron hinges has 60 % of the trailing edge occupied by powerful single-slotted flaps. Wings and horizontal tail can be quickly detached for transportation or storage

Mechanically actuated control surfaces with electric trim tab on the elevator and electrically actuated flaps

Shark 600 has tricycle type retractable undercarriage with steerable 13x4" nose wheel and 14x4” main wheels with hydraulic disc brakes

100HP Rotax 912ULS flat-four engine with variable-pitch composite propeller. Integral fuel tanks in wings, capacity 100 litres.