MGW is 3850 kg  without the addition of a Service Bulletin

Overview

Data on design, manufacture and status

Latest or last design authority: Airbus Helicopters
Originally designed by Sud-Aviation

Primary manufacturer: Aérospatiale, Helicopter Division

Parent type: Airbus Helicopters H155/EC155/AS365/SA.365

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: Wheels (all retractable)

Overall Dimensions

Data on aircraft size

Overall Width: 11.93 m (39.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Arriel 1C turbine

Engine manufacturer: Turbomeca

Max continuous power: 437 kW (586 hp)

Take-off / rated power: 492 kW (660 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 4000 kg (8818 lb)

Related VFS Resources

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Related Public Resources

Resources related to the SA.365N Dauphin 2, provided by public sources across the internet.

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