Development of the Russian helicopter began in 1984 for the Ka-126, a derivative of the Kamov Ka-26.  Compared to its predecessor, the Ka-126: has a single engine, eliminating the feature of an engine pod on either side of the aircraft; has a cabin capacity of seven passengers.

Overview

Data on design, manufacture and status

Design authority: Kamov Design Bureau

Primary manufacturer: Kamov

Parent type: Kamov Ka-26

Aircraft status: Status unknown

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

Related VFS Resources

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Related Public Resources

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