Vertipedia - Airbus Helicopters H120/EC120 B Colibri

Weights
Max Gross Weight (ground):	1,715 kg	3,781 lb
Max Gross Weight (airborne):	1,800 kg	3,968 lb
Max Take-off Weight:	1,715 kg	3,781 lb
Empty Weight:	1,001 kg	2,207 lb

Climb Performance
Max Rate of Climb:	6 m/s	1,150 fpm

Hover Performance
Hover Ceiling IGE:	2,819 m	9,249 ft
Hover Ceiling OGE:	2,316 m	7,598 ft

Limitations
Max Level Flight Speed:	223 km/h	120 kts
Never Exceed Speed:	278 km/h	150 kts
Service Ceiling:	5,182 m	17,001 ft

Range and Endurance
Max Range:	710 km	383 nm
Max Endurance:	4 hrs

Provided powerplant data is for uninstalled, sea level, static operations.

Powerplant
Number of engines:	1
Designation:	Turbomeca Arrius 2F turbine
Manufacturer:	Turbomeca

Normal Ratings
Max continuous:	336 kW	450 hp
Take-off / rated:	376 kW	504 hp
Intermediate:
Maximum:

OEI Ratings
OEI contingency:
OEI continuous:
OEI 30-second:
OEI intermediate:

Main Rotor Characteristics
Diameter:	10.00 m	32.81 ft
RPM:
Direction of Rotation:	Unknown
Hub Type:

Main Rotor Blade Characteristics
Blade Construction:
Blade Chord:
Blade Tip Geometry:
Blade Twist:
Number of Blades:	3

Main Rotor Derived Characteristics
Disc Area:	78.54 m²	845.4 ft²
Disc Loading:	21.84 kg/m²	4.472 lb/ft²
Solidity:

Main Rotor Blade Derived Characteristics
Blade area per blade:
Tip Speed:

Tail Rotor Characteristics
Diameter:	0.75 m	2.46 ft
Configuration:	Unknown
Direction of Rotation:	Unknown
RPM:

Tail Rotor Blade Characteristics
Number of Blades:	1
Blade Construction:
Blade Chord:
Blade Twist:

Tail Rotor Derived Characteristics
Disc Area:	0.44 m²	4.8 ft²
Solidity:

Tail Rotor Blade Derived Characteristics
Tip Speed:
Blade Area (per blade):

References

References and sources used

Airbus H120 Technical Data 2016

Airbus Helicopters
Airbus Helicopters, 09/19/2018
Report or Technical Manual

Civil Range

Airbus Helicopters
https://www.airbushelicopters.com/website/docs_wsw/RUB_26/tile_2581/CIVILRange-02-2015.pdf, 20 Sept 2015 (page 2)
Report or Technical Manual