TYPE: Two-seat lightplane.
PROGRAMME: First flown June 2003.
DESIGN FEATURES: Low wing with winglets; sweptback fin with root-mounted tailplane.
FLYING CONTROLS: Conventional and manual. No aerodynamic balances on tail surfaces.
STRUCTURE: Generally of glass fibre, with carbon fibre and duralumin.
LANDING GEAR: Tricycle type. Mainwheels retract inwards: nosewheel rearwards.
POWER PLANT: Not specified. Three-blade propeller. Fuel capacity 114 litres (30.0 US gallons; 25.0 Imp gallons).
|Wing span||8.75 m (28 ft 4½ in)|
|Length overall||7.50 m (24 ft 7¼ in)|
|Height overall||3.20 m (10 ft 6 in)|
|WEIGHTS AND LOADINGS:|
|Weight empty||450 kg (992 lb)|
|Max T-O weight||800 kg (1,763 lb)|
|Never-exceed speed (VNE)||156 kt (290 km/h; 180 mph)|
|Cruising speed at 75% power||135 kt (241 km/h; 150 mph)|
|Stalling speed, power off:|
|flaps up||53 kt (97 km/h; 60 mph)|
|flaps down||44 kt (81 km/h; 50 mph)|
|Max rate of climb at S/L||304 m (1,000 ft)/min|
|Service ceiling||4,570 m (15,000 ft)|
|T-O run, ISA: at S/L||200 m (660 ft)|
|at 1,220 m (4,000 ft)||350 m (1,150 ft)|
|Landing run||400 m (1,315 ft)|
|Range||955 n miles (1,770 km; 1,100 miles)|