Airbus Helicopters H215 C

Attribution

Attribution

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

Parent type: Airbus Helicopters H215

Aircraft status: Status unknown

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: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 4.94 m (16.2 ft)

Overall Length: 18.70 m (61.4 ft)

Overall Width: 15.60 m (51.2 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Makila 1A1 turbine

Engine manufacturer: Turbomeca

Max continuous power: 1185 kW (1588 hp)

Take-off / rated power: 1357 kW (1819 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 8600 kg (18960 lb)

Max Range: 642 km (347 nm)

Max Endurance: 3.3 hrs (3.3 hrs)

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