Project Description
4 seats (including the pilot)
maximum takeoff weight: 1089 kg / empty weight: 654 kg
maximum range: 555 Km
maximum speed: 230 km/h
cruising speed: 208 km/h
maximum altitude: 4662 m
engine: Lycoming O-540-F1B5
average fuel consumption: 60 l/h
main rotor diameter: 11 m
height: 4 m / length: 13 m
