Previously designated EC120 B

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H120

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Fenestron/Shrouded tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 3.40 m (11.2 ft)

Overall Length: 11.52 m (37.8 ft)

Overall Width: 10.00 m (32.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Turbomeca Arrius 2F turbine

Engine manufacturer: Turbomeca

Max continuous power: 336 kW (450 hp)

Take-off / rated power: 376 kW (504 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1715 kg (3781 lb)

Max Gross Weight (airborne): 1800 kg (3968 lb)

Max Range: 710 km (383 nm)

Max Endurance: 4.3 hrs (4.3 hrs)

Related VFS Resources

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Related Public Resources

Resources related to the H120/EC120 B Colibri, provided by public sources across the internet.

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