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)