The aircraft was originally designated EC155 B1 before Airbus Helicopters revised their aircraft designation system.

Overview

Data on design, manufacture and status

Design authority: Airbus Helicopters

Primary manufacturer: Airbus Helicopters

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 Height: 4.35 m (14.3 ft)

Overall Length: 14.30 m (46.9 ft)

Overall Width: 12.60 m (41.3 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Turbomeca Arriel 2C2 turbine

Engine manufacturer: Turbomeca

Max continuous power: 636 kW (853 hp)

Take-off / rated power: 704 kW (944 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 4920 kg (10847 lb)

Max Range: 784 km (423 nm)

Max Endurance: 4.1 hrs (4.1 hrs)

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Related Public Resources

Resources related to the H155/EC155 B1 Dauphin, provided by public sources across the internet.

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