Yak-10
Yak-10 (Yak-14, internal designation) - an aircraft for communications and local airlines, a high-wing strut wing with an M-11FM engine of 145 hp. With. and VISH-327 - the development of the pre-war aircraft AIR-5 and AIR-6, with a four-seat cabin. The structure is mixed. The fuselage frame is truss, welded from M steel pipes, the wing is wooden, the plumage is duralumin, the lining is linen everywhere. Pyramid chassis, wheels 500x150 and 200x80 mm. The struts of the wing converge at the base of the axle shafts of the wheels, teardrop-shaped pipes made of M steel. The weight of the empty aircraft is 792 kg, the flight weight is 1150 kg, which made it possible to lift three people, i.e. two passengers, reloading (with three passengers) - 1230 kg. Commercial load with luggage 10 kg, with two and three passengers, respectively, 170 kg and 250 kg.The aircraft was released in January and state tests were completed in June 1945. Speed 200 km/h, range 576 km. The ease of piloting and operation, ease of repair was noted, and mass production was recommended, which soon followed, including the Yak-10V (export) version with dual controls. In 1946, with the M-11FR engine of 160 liters. With. the flight data of serial aircraft improved.
In 1947, the Yak-10S (sanitary) was released with a triangular loading door for stretchers on the port side. With the same flight masses, the Yak-10S could lift 1-2 patients on a stretcher and an accompanying person. Yak-10G (hydro) - float version on the AIR-6 type chassis, 1946. Passed only factory tests, flight data were not completely removed.
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