Utva 213 Vihor
   HOME

TheInfoList



OR:

Utva 213 Vihor was a late 1940s
Yugoslavia Yugoslavia (; sh-Latn-Cyrl, separator=" / ", Jugoslavija, Југославија ; sl, Jugoslavija ; mk, Југославија ;; rup, Iugoslavia; hu, Jugoszlávia; rue, label=Pannonian Rusyn, Югославия, translit=Juhoslavija ...
n two-seat advanced trainer.


Design and development

Designed and built by the Yugoslav state factory, the Type 213 was first flown in 1949, a cantilever low-wing monoplane powered by a
Ranger SVG-770-CB1 The Ranger V-770 was an American air-cooled inverted V-12 aircraft engine developed by the Ranger Aircraft Engine Division of the Fairchild Engine & Aircraft Corporation in the early 1930s. Design and development In 1931, the V-770 design was ...
engine. The prototype had a
conventional landing gear Conventional landing gear, or tailwheel-type landing gear, is an aircraft undercarriage consisting of two main wheels forward of the center of gravity and a small wheel or skid to support the tail.Crane, Dale: ''Dictionary of Aeronautical Term ...
which retracted forward, the second prototype and production aircraft had a wider track main gear that retracted inwards. It had an enclosed cockpit for the instructor and student in tandem under a long glazed canopy. For training the Vihor had two forward-facing machine guns and could carry up to 100 kg of bombs. In 1957 an improved
radial engine The radial engine is a reciprocating type internal combustion engine configuration in which the cylinders "radiate" outward from a central crankcase like the spokes of a wheel. It resembles a stylized star when viewed from the front, and is ca ...
d variant entered service as the Type 522.


Aircraft on display

One aircraft is on display at the Museum of Yugoslav Aviation, Belgrade, Serbia.


Specifications


See also


References


Notes


Bibliography

* * {{refend 1940s Yugoslav military trainer aircraft Single-engined tractor aircraft Low-wing aircraft Aircraft manufactured in Yugoslavia Aircraft first flown in 1949