Kamov Ka-26

Twin Rotorcraft

The Kamov Ka-26 is a Soviet-designed light utility helicopter distinguished by its signature coaxial contra-rotating rotor system, eliminating the need for a tail rotor, and a unique modular fuselage that allows operators to swap mission-specific pods in minutes. First flown in 1965, the Ka-26 was built primarily for agricultural work, cargo transport, and passenger service across the USSR and Eastern Bloc, with over 850 produced through 1985. Its twin Vedeneyev M-14V-26 radial piston engines, mounted on outrigger pylons, give it unusual redundancy for a light helicopter and a distinctive appearance. The coaxial rotor design provides excellent hover stability and a compact footprint, making it ideal for confined-area operations. Though the Ka-26 never achieved widespread adoption in Western markets, a small number found their way to North America as surplus aircraft in the post-Cold War era, where they've been operated by private owners and agricultural operators. The type's rugged construction and simple systems have kept a handful airworthy decades after production ended, though parts support remains challenging. Maximum speed is modest at around 93 knots, with a service ceiling near 10,000 feet and typical mission endurance of two to three hours depending on payload configuration. SkyMeter has tracked 2 flights across 1 airframes and 1 operators, with MCLANAHAN JOHN P the largest observed operator.