TYPE: Two-seat lightplane.

PROGRAMME: Go-ahead for prototype issued 12 May 2004; prototype has flown. Marketed as suitable for a range of tasks, including flight training and cropspraying.

DESIGN FEATURES: Low-wing cantilever monoplane. Similar to Aeropract-33.

FLYING CONTROLS: Conventional and manual.

STRUCTURE: Wing and fuselage of three-part composites.

LANDING GEAR: Tailwheel type; fixed. Fuselage-mounted, spring titanium cantilever mainwheel legs; drum brakes.

POWER PLANT: One 73.5 kW (98.6 hp) Rotax 912 ULS flat four driving a Kiev 284/1800 three blade propeller.

ACCOMMODATION: Pilot and passenger side-by-side.

DIMENSIONS, EXTERNAL:

  • Wing span: 10,215 m (33 ft 6¼ in)
  • Wing aspect ratio: 7.6
  • Length overall: 6.70 m (21 ft 11¾ in)
  • Height overall: 3.07 m (10 ft 1 in)
  • Wheel track: 2.305 m (7 ft 7 in)

AREAS:

  • Wings, gross: 13.67 m² (147.14 sq ft)

WEIGHTS AND LOADINGS:

  • Weight empty: 477 kg (1,052 lb)
  • Max T-O weight: 750 kg (1,653 lb)
  • Max wing loading: 54,86 kg/m² (11.24 lb/hp)
  • Max power loading: 10.20 kg/kW (16.77 lb/sq ft)

PERFORMANCE:

  • Never exceed speed (VNE): 118 kt (220 km/h; 136 mph)
  • Max operating speed: 97 kt (180 km/h; 112 mph)
  • Normal cruising speed: 81 kt (150 km/h; 93 mph)
  • Stalling speed, power off, flaps down: 41 kt (75 km/h; 47 mph)
  • Max rate of climb at S/L: 300 m (984 ft)/min
  • Service ceiling: 3,500 m (11,480 ft)
  • T-O run: 80 m (263 ft)
  • Landing run: 90 m (296 ft)
  • Range: 486 n miles (900 km; 559 miles)