The aircraft received its FAA certification on May 15, 1997

Overview

Data on design, manufacture and status

Latest or last design authority: MD Helicopters, Inc.
Originally designed by McDonnell Douglas Helicopter Systems

Latest or last primary manufacturer: MD Helicopters, Inc.
Originally manufactured by McDonnell Douglas Helicopter Systems

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 NOTAR

Crew required: 1-2 in Side-by-side arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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Related Public Resources

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