EC120 Colibri / H120

Aircraft type

Data given for the Airbus Helicopters EC120 B Colibri in basic configuration.

Manufacturer Airbus Helicopters
Aircraft family Helicopter
Engine type Turboshaft
Engine count 1
ICAO code EC20

Technical specifications

Design
Main rotor blades
3
Main rotor count
1
Tail rotor blades
8
Tail rotor count
1
Dimensions
Height
3.4 m
11.15 ft
Length
9.6 m
31.5 ft
Main rotor diameter
10 m
32.81 ft
Tail rotor diameter
0.75 m
2.46 ft
Width
1.5 m
4.92 ft
Fuel
Fuel capacity
406 l
107 us gal
Performance
Service ceiling
20,000 ft
6,100 m
Speed limits
Vne
150 kt
278 km/h / 173 mph
Weight limits
MLW
1,715 kg
3,781 lb
MTOW
1,715 kg
3,781 lb

Aircraft models

Engine models

Manufacturer Name Cont. T/O
Safran Helicopter Engines Arrius 2F 335 kW 376 kW