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 devices: 2 in Coaxial configuration

Crew required: 1 in Side-by-side arrangement

Landing gear: Wheels (non-retractable)

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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