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: As LightWing GR-912 but with flaps as standard.

STRUCTURE: As 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)

The article appears in the following publication:
Jane's All the World's Aircraft 2004-2005. Jane's Information Group Ltd. 2004. ISBN: 0-7106-2614-2