Twin seats in tandem, double pitch
Cell composition: Truss, Pipes, Carbon fiber cabin, Plexiglass canopy
Powerplant: Rotax 914, 4 cylinders, 4 strokes, Turbocharger, Liquid cooling
Multiple engine temp. gauges
Tachometer motor-rotor, Map.
2 engine cooling fans
2 petrol electric pumps
2 servo trim
Tank capacity: 40 l = 30 kg
Hourly fuel consumption to 75% of the power generated by the motor: 16 l / h = 12 kg / h
Fuel: Avio 100 LL, Gasoline minimum MON83 or RON90 octane Car Super Gasoline or Gasoline lead-free
Payload: 205 kg
Main rotor diameter: 6.20 m (20.30 ft) 2 blades
Angular speed â€“ 104 % : 173 m/sec (550 fps)
Tail rotor diameter: 1.02 m (3.34 ft) 2 blades
Angular speed - 104% : 163 m/sec (535 fps)
Fuel: Avio 100 LL
Gasoline minimum MON83 or RON90 octane, Car Super Gasoline or Gasoline lead-free
Frame made of steel 4130-tight pressure of 2 bar of nitrogen gas
The inspection must be carried out by the manufacturer in Italy
Registration number by AeCI: I-5918
The helicopter is sold as assembly kit or is assembled by the manufacturer for a higher price.
I-5918 has been assembled by the builder.