Il 14
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Specifications Il 14 blueprint
The Il-14 is a versatile twin-engine aircraft designed and built by the Soviet Union's Ilyushin aircraft manufacturer. Built from 1946 to 1959, the Il-14 had a maximum takeoff weight of 6,600 kilograms and a range of 1,150 kilometers. The Il-14 had a high-wing design paired with a rugged construction that allowed for rough landings and short takeoffs. The aircraft was powered by two Shvetsov M-11FR engines, each with a nominal power of 800 horsepower. The Il-14's wing was of a classic "Butterfly" shape, allowing for an aerodynamic profile during flight. The Il-14 had a capacity of up to 16 passengers and had the provisions to carry freight as well. It could also accommodate various combinations of passengers and freight, and could be configured as a passenger or a freight aircraft. The Il-14 was robust and reliable, even in difficult conditions. It was also equipped with a two-axis autopilot, enabling it to be flown by inexperienced pilots with minimal training. The aircraft was widely used in passenger and freight transport, and was the first choice for Soviet agricultural aviation. It was also used extensively for medevac flights, rescue operations, geophysical survey work, and military transport. Its versatility enabled it to be used for a variety of missions in the Soviet Union. Overall, the Il-14 is a highly reliable and versatile aircraft that can accommodate various payloads. Its robust design and versatility made it arguably the most important passenger transport aircraft during the 1950s.
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