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

References

References and sources used

Jane's Helicopter Markets and Systems
Jane's Information Group Limited
2003 (page 185)
Book

OKB N.I.Kamova
G.I. Kuznetsov
1999 (page 274)
Book

Russian Helicopters, Ka-27
Russian Нelicopters, JSC
5 July 2017 (page 185)
Website

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