TYPE: Tandem-seat ultralight.
PROGRAMME: Development being undertaken during late 2002; announced January 2003.
DESIGN FEATURES: Will meet ultralight criteria in most countries. Low wing with slight sweepback and upturned wingtips; sweptback fin; constant-chord tailplane. Wing has removable outer panels for storage and ground transportation.
FLYING CONTROLS: Conventional and manual.
STRUCTURE: Fuselage of wood with elliptical cross-section and composites panels behind cockpit. Two-spar cantilever wooden wing has wooden leading-edges with fabric-covered rear section. Fabric-covered control surfaces.
LANDING GEAR: Tailwheel type; fixed. Sprung steel main legs with 400x100 mainwheels and brakes. Steerable tailwheel.
POWER PLANT: One 47.8 kW (64.1 hp) Rotax 582 UL engine in prototype; options will include Rotax 912 and Parma-Technik Mikron engines. Fuel capacity 35 litres (9.2 US gallons; 7.7 Imp gallons).