Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H125

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 3.34 m (11.0 ft)

Overall Length: 12.94 m (42.5 ft)

Overall Width: 10.69 m (35.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Turbomeca Arriel 2D turbine

Engine manufacturer: Turbomeca

Max continuous power: 638 kW (855 hp)

Take-off / rated power: 710 kW (952 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2250 kg (4960 lb)

Max Range: 631 km (341 nm)

Max Endurance: 4.5 hrs (4.5 hrs)

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