A continuation of the Ka-26 design, the Ka-226 remains modular in its configuration.  Maximum internal and slung loads are 1400 kg and 1500 kg, respectively.

There are several versions, including: the Ka-226A rescue version, with 9 seats and a rescue winch with a lift capacity of 300 kg; the fire fighting version; the passenger version, equipped with 6-8 seats.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-26

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Coaxial (x2)

Crew required: 1

Crew seating: Side-by-side

Landing gear: Wheels (non-retractable)

Overall Dimensions

Data on aircraft size

Overall Height: 4.15 m (13.6 ft)

Overall Length: 13.00 m (42.7 ft)

Overall Width: 13.00 m (42.7 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 2

Engine designation: Allison 250-C20B (de-rated for use on Bell 206) turbine

Engine manufacturer: Allison Engine Company

Max continuous power: 201 kW (270 hp)

Take-off / rated power: 236 kW (317 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 3400 kg (7496 lb)

Max Range: 600 km (324 nm)

Max Endurance: 4.3 hrs (4.3 hrs)

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