TYPE: Side-by-side ultralight.

PROGRAMME: Design work started 1991; prototype (OK-EUC 01) made first flight 22 October 1997. A second prototype has also flown. Will be certified in both ultralight and VLA categories.

DESIGN FEATURES: Typical small lightplane low-wing configuration. Wing sections NACA 2305 at root, NACA 2312 at tip.

FLYING CONTROLS: Conventional and manual. Horn-balanced rudder and one-piece elevator; central trim tab in elevator. Flaps fitted.

STRUCTURE: Mainly composites fuselage and wooden wings with single spar.

LANDING GEAR: Tricycle type; fixed. Cantilever self-sprung main units; castoring nosewheel.

POWER PLANT: One 70.8 kW (95 hp) Aero Max 2400 piston engine; two-blade propeller. Fuel capacity 40 litres (10.6 US gallons; 8.8 Imp gallons).

ACCOMMODATION: Pilot and passenger seated side by side. Doors open forwards. Baggage compartment behind seats.