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 devices: 1 Single main rotor

Dedicated control device: 1 Fenestron/Shrouded tail rotor

Crew required: 1 in Side-by-side arrangement

Landing gear: Wheels (all retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

References

References and sources used

Airbus H155 Technical Data 2016
Airbus Helicopters
Airbus Helicopters, 09/21/2018 (page )
Report or Technical Manual

Related VFS Resources

Resources related to the H155/EC155 B1 Dauphin, provided by the Vertical Flight Society.
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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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