Project Description
5 seats (including the pilot)
maximum takeoff weight: 1225 kg / empty weight: 581 kg
maximum range: 648 Km
maximum speed: 231 km/h
cruising speed: 185 km/h
maximum altitude: 4267
engine: Rolls-Royce RR300 300 shp turboshaft; derated to 270 shp for takeoff and 224 shp continuous
average fuel consumption: 90 l/h
main rotor diameter: 10.06 m
height: 3.48 m / length: 11.66 m
