Design and Development
The Il-14 was developed as a replacement for the widespread Douglas DC-3 and its Soviet built version, the Lisunov Li-2. A development of the earlier Ilyushin Il-12, (that first flew in 1945), the Il-14 was intended for use in both military and civil applications. The Il-12 had major problems with poor engine-out behaviour. Also, it had less payload capability than was originally planned (although the Il-12 was intended to carry 32 passengers, in service it only carried 18, which was uneconomic).
The development into the Il-14 was a vast improvement over the Il-12, with a new wing and a broader tailfin. It was powered by two 1,400 kW (1,900 hp) Shvetsov ASh-82T-7 radial piston engines. These changes greatly improved aerodynamic performance in engine-out conditions.
Total production of the Il-14 was 1,112 aircraft: 469 in Moscow (Moscow Machinery Plant Nr.30) from 1956 to 1958, 360 in Tashkent (Factory Nr.84) from 1954 to 1958. Licenced production of 80 in East Germany by VEB Flugzeugwerke Dresden (FWD) from 1956 to 1959 and 203 in Czechoslovakia by Avia, Prague, from 1956 to 1960. It was rugged and reliable, and thus was widely used in rural areas with poor quality airfields.
The type was also used by the East German aircraft industry as a test aircraft for the horizontal stabilizer of the Baade 152.
Read more about this topic: Ilyushin Il-14
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