TYPE: Single-seat sportplane kitbuilt.

PROGRAMME: Introduced 2006; maiden flight of prototype (HB-YMV) 23 September 2006.

DESIGN FEATURES: Single-seat derivative of Votec 322; rudder area reduced to 1.50 m² (16.15 sq ft).

POWER PLANT: One 261 kW (350 hp) Textron Lycoming AEIO-580; propeller as for Votec 322. Fuselage fuel tank as Votec 322, wing tanks reduced to 40 litres (10.6 US gallons; 8.8 Imp gallons) each, hence total capacity 180 litres (47.6 US gallons; 39.6 Imp gallons).

DIMENSIONS, EXTERNAL:
As Votec 322

WEIGHTS AND LOADINGS:

• Weight empty: 580 kg (1,279 lb)
• Max T-O weight: 830 kg (1,829 lb)
• Max wing loading: 79.05 kg/m² (16.19 lb/sq ft)
• Max power loading: 3.18 kg/kW (5.23 lb/hp)

PERFORMANCE:

• Never-exceed speed (V_NE): 234 kt (434 km/h; 270 mph)
• Max cruising speed: 174 kt (322 km/h; 200 mph)
• Stalling speed: 57 kt (105 km/h; 65 mph)
• Max rate of climb at S/L: 1,067 m (3,500 ft)/min
• Max rate of roll: 420°/s
• T-O run: 110 m (360 ft)
• Landing run: 350 m (1,150 ft)
• g limits: ±12