TYPE: Four-seat utility twin.

PROGRAMME: Development began in 2003, although aircraft not revealed until 2005. Prototype first flown 29 November 2005.

DESIGN FEATURES: High-wing lightplane with design elements of A-33 apparent.

FLYING CONTROLS: Conventional and manual. Flaps.

STRUCTURE: Strut-braced, constant-chord wing. Sweptback fin and underfin.

LANDING GEAR: Tricycle type; fixed. Optional twin floats.

POWER PLANT: Two 84.6 kW (113.4 hp) Rotax 914 UL engines driving three-blade propellers. Fuel capacity 265 litres (70.0 US gallons; 58.3 Imp gallons).

ACCOMMODATION: Door on port side of fuselage; baggage door on port side of fuselage behind cockpit.

All data are provisional.

DIMENSIONS, EXTERNAL:

  • Wing span: 12.00 m (39 ft 4½ in)
  • Length overall: 7.20 m (23 ft 7½ in)
  • Height overall: 3.70 m (12 ft 1¾ in)

AREAS:

  • Wings, gross: 17.40 m² (187.3 sq ft)

WEIGHTS AND LOADINGS:

  • Weight empty: 850 kg (1,874 lb)
  • Max T-O weight: 1,400 kg (3,086 lb)

PERFORMANCE:

  • Normal cruising speed: 119 kt (220 km/h; 137 mph)
  • Service ceiling: 3,500 m (11,480 ft)
  • Range with max fuel: 809 n miles (1,500 km; 932 miles)
  • g limits: +4/-2