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).


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