TYPE: Side-by-side ultralight.
PROGRAMME: First flown in 1999.
COSTS: US$35,000 to US$39,000, according to equipment (2001).
DESIGN FEATURES: High-mounted, constant-chord, strut-braced wing. Sweptback fin and mid-mounted tailplane.
FLYING CONTROLS: Conventional and manual. Flaps.
STRUCTURE: Metal airframe. Fabric-covered wing.
LANDING GEAR: Tailwheel type; fixed.
POWER PLANT: One Rotax flat-four driving a three-blade, wooden propeller: 59.6 kW (79.9 hp) Rotax 912 UL; 73.5 kW (98.6 hp) 912 ULS; or 84.6 kW (113.4 hp) 914. Fuel capacity 88 litres (23.2 US gallons; 19.4 Imp gallons).