TYPE: Two-seat lightplane.
PROGRAMME: North American marketing launched at AirVenture, Oshkosh, in July 2003 with a US-registered demonstrator.
DESIGN FEATURES: Short-field performance. Constant-chord, high-lift, high-mounted mainplanes with V-strut bracing resemble those of Zenith CH 701. Sweptback fin and root-mounted tailplane.
FLYING CONTROLS: Conventional and manual. Junkers ailerons and flaps. No aerodynamic balances on tail surfaces.
STRUCTURE: Generally of glass fibre.
LANDING GEAR: Tricycle type; fixed. Cantilever main legs with hydraulic brakes. Speed fairings on all wheels.
POWER PLANT: One flat-four piston engine; option of 73.5 kW (98.6 hp) Rotax 912 S or 84.5 kW (123.3 hp) Rotax 914, each driving a three-blade propeller. Fuel capacity 76 litres (20.0 US gallons; 16.7 Imp gallons).
ACCOMMODATION: Two persons, side by side. Baggage area behind seats. Door each side.