
General information
The H120 is a light, multi-purpose helicopter produced by the Franco-German manufacturer Airbus Helicopters. It is equipped with a turbine engine and offers seating for one pilot and four passengers. The model is versatile and used for various private and commercial purposes.


Technical data
Type: Light multi-purpose helicopter
First flight: June 9, 1995
Country of origin: Germany/France
Crew: 1
Capacity: 4 passengers
Main rotor blades: 3
Tail rotor blades: 8 (Fenestron)
Main rotor diameter: 10.00 m
Tail rotor diameter: 1.00 m
Rotor disc area: 81.70 m²
Hull length: 9.60 m
Total length: 11.52 m
Height: 3.40 m
Unladen weight: 895 kg
Maximum takeoff weight: 1,680 kg
Top speed: 278 km/h (150 kts)
Cruising speed: 222 km/h (120 kts)
Service ceiling: 6,096 m (20,000 ft)
Range: 732 km
Consumption: 95 l/h
Fuel capacity: 411 l Jet A1 (80 l in optional auxiliary tank)
Max. flight duration: 4 hours 20 minutes
Engine: 1x Turbomeca Arrius 2F
Power output: 335 kW continuous power, 376 kW starting power











