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 (V_NE): 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)