TYPE: Side-by-side ultralight/kitbuilt.
PROGRAMME: Developed version of GR-912 (which see); certified in Australian Primary category. Uses original LightWing type certificate.
CUSTOMERS: 10 built by end 2002.
COSTS: A$88,9O0 factory built; A$45,900 kit, including alternative 59.6 kW (79.9 hp) Werner engine (2003).
FLYING CONTROLS: Conventional and manual. Horn-balanced tail surfaces; elevator pushrod-operated; aileron and rudder cable-operated.
STRUCTURE: Welded steel tube fuselage; riveted aluminium alloy wings; mainly fabric covered, with non-structural glass fibre fairings.
LANDING GEAR: Non-retractable tricycle type.
POWER PLANT: One 59.6 kW (79.9 hp) Rotax 912 UL flat-four driving an Aerofiber two-blade fixed-pitch wooden propeller. Fuel capacity 62 litres (16.4 US gallons; 13.6 Imp gallons).
|Wing span||9.50 m (31 ft 2 in)|
|Length overall||5.68 m (18 ft 71/2in)|
|Height overall||2.20 m (7 ft 21/2in)|
|Wings, gross||15.14 m2 (163.0 sq ft)|
|WEIGHTS AND LOADINGS:|
|Weight empty||300 kg (661 lb)|
|Max T-O weight||480 kg (1,058 lb)|
|Cruising speed at 75% power||72 kt (133 km/h; 83 mph)|
|Stalling speed||35 kt (65 km/h; 41 mph)|
|T-O and landing from 15 m (50 ft)||300 m (985 ft)|
|Range with max fuel||300 n miles (555 km; 345 miles)|