TYPE: Side-by-side ultralight/kitbuilt.
PROGRAMME: Development of version announced in 2003 First flight date had not been announced by April 2003. Will be available only as a kit for AUF or Experimental categories.
DESIGN FEATURES: Based on company's existing LightWing GR-912 family.
FLYING CONTROLS: A S LightWing GR-912 but with flaps as standard.
STRUCTURE: A S LightWing GR-912, but with low wing. Fuselage has integral roll-cage.
LANDING GEAR: Initially offered as a non-retractable tailwheel type.
POWER PLANT: One 84.6 kW (113.4 hp) Rotax 914 driving an in-flight adjustable propeller. Fuel tanks in glass-fibre wingtips.
ACCOMMODATION: Gull-wing doors each side of fuselage. All data are provisional.
|Wing span||7.40 m (24 ft 31/4 in)|
|Length overall||6.00 m (19 ft 81/4 in)|
|WEIGHTS AND LOADINGS:|
|Max T-O weight||544 kg (1,199 lb)|
|Normal cruising speed||150 kt (278 km/h; 173 mph)|
|Stalling speed, flaps down||45 kt (84 km/h; 52 mph)|
|Service ceiling||3,050 m (10,000 ft)|