Single-engine aircraft Shark UL

4-stroke enginetwo-seaterVLA

Shark UL - a high-performance European UL with retractable gear, smaller wing and variable-pitch propeller. Shark UL is designed and tested for a maximum take-off weight of 600 kg. DESIGN FEATURES Designed according to European UL and US Light Sport Aircraft criteria. Composite low-wing design with classic tail and tandem seating. Model trupuSTRUCTURE 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.