TYPE: Side-by-side ultralight/kitbuilt.
PROGRAMME: Developed version of GR-912; certified in Australian Primary category. Uses original LightWing type certificate.
CUSTOMERS: 10 built by end 2002.
COSTS: A$88,900 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).
| DIMENSIONS, EXTERNAL: | |
| Wing span | 9.50 m (31 ft 2 in) |
| Length overall | 5.68 m (18 ft 7½ in) |
| Height overall | 2.20 m (7 ft 2½ in) |
| AREAS: | |
| 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) |
| PERFORMANCE: | |
| 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) |
| g limits | +6/-4 |
