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.
| DIMENSIONS, EXTERNAL: | |
| Wing span | 7.40 m (24 ft 3¼ in) |
| Length overall | 6.00 m (19 ft 8¼ in) |
| WEIGHTS AND LOADINGS: | |
| Max T-O weight | 544 kg (1,199 lb) |
| PERFORMANCE: | |
| 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) |
