Designed and financed by the Kazan Helicopters plant, development of the Aktay light multipurpose helicopter began in 1997.

Overview

Data on design, manufacture and status

Design authority: Kazansky Vertoletnyi Zavod OAO (Kazan Helicopter Plant JSC)

Primary manufacturer: Kazansky Vertoletnyi Zavod OAO (Kazan Helicopter Plant JSC)

Parent type: No type defined

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: Skids

Overall Dimensions

Data on aircraft size

Overall Width: 10.00 m (32.8 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: AvtoVAZ VAZ-4265 reciprocating

Engine manufacturer: AvtoVAZ

Take-off / rated power: 200 kW (268 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Range: 400 km (216 nm)

Max Endurance: 4.0 hrs (4.0 hrs)

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Related Public Resources

Resources related to the Aktay , provided by public sources across the internet.

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