Note: MGW of 2950kg  is available within specified constraints

Overview

Data on design, manufacture and status

Latest or last design authority: Airbus Helicopters Deutschland GmbH
Originally designed by Eurocopter Deutschland GmbH

Latest or last primary manufacturer: Airbus Helicopters Deutschland GmbH
Originally manufactured by Eurocopter Deutschland GmbH

Parent type: Airbus Helicopters H135/EC135

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 Width: 10.20 m (33.5 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Arrius 2B2 turbine

Engine manufacturer: Turbomeca

Take-off / rated power: 472 kW (633 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 2910 kg (6415 lb)

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Related Public Resources

Resources related to the EC135 T2+ , provided by public sources across the internet.

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