Kamov Ka-226

The Kamov Ka‑226 is a twin‑engine light utility helicopter developed by the Russian manufacturer Kamov in the early 2000s. Its design traces back to the Ka‑226T prototype first flown in 2002, and series production began in 2010 after successful certification by the Russian aviation authorities. The aircraft employs a coaxial main‑rotor system, a hallmark of Kamov engineering, which eliminates the need for a tail rotor, reduces overall length, and enhances manoeuvrability in confined environments. Powered by two Allison (later Klimov) TV3‑117V turboshaft engines, the Ka‑226 delivers a maximum take‑off weight of about 3.3 tonnes and can be configured for passenger transport, cargo, medical evacuation, or specialized missions such as reconnaissance and firefighting. Its interchangeable modular pods allow rapid role changes on the ground, a feature that has attracted operators seeking versatility. The Ka‑226’s significance lies in revitalising Kamov’s civilian market presence, offering a competitively priced alternative to Western light helicopters, and supporting operations in remote, rugged regions across Russia, India, and several African nations. Its blend of compact design, flexible payload options and reliable performance underscores its growing impact on modern utility aviation.

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