Utva 213 Vihor

Last updated
Vihor
BAM-44-Utva 213-3 Vihor.jpg
General information
TypeAdvanced military trainer
National origin FPR Yugoslavia
Designer
Government Factories
Primary userYugoslav Air Force
Number built196
History
Manufactured1952-54
Introduction date1952
First flight1949
Retired1961
Developed into Soko 522

Utva 213 Vihor was a late 1940s Yugoslavian two-seat advanced trainer. [1]

Contents

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 520 hp (388 kW) Ranger SVG-770-CB1 engine. [1] The prototype had a conventional landing gear which retracted forward, the second prototype and production aircraft had a wider track main gear that retracted inwards. [1] It had an enclosed cockpit for the instructor and student in tandem under a long glazed canopy. [1] For training the Vihor had two forward-facing machine guns and could carry up to 100 kg of bombs. [1] In 1957 an improved radial engined variant entered service as the Type 522. [1]

Aircraft on display

Vihor on display at the Museum of Yugoslav Aviation 213uMuzejuJvBeogradSlika1.jpg
Vihor on display at the Museum of Yugoslav Aviation

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

Specifications

Data from Jane's All The World's Aircraft 1956–57 [2]

General characteristics

Performance

Armament

See also

Related development

References

Notes

  1. 1 2 3 4 5 6 Orbis 1985, p. 1996
  2. Bridgman 1956, pp. 349–350.

Bibliography

  • Bridgman, Leonard (1956). Jane's All The World's Aircraft 1956–57. New York: The McGraw Hill Book Company.
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing.