Yakovlev AIR-5

AIR-5
Role Single-engined cabin monoplane
National origin Soviet Union
Manufacturer Yakovlev
First flight 1931
Number built 1
Developed into Yakovlev AIR-6

The Yakovlev AIR-5 was a prototype Soviet single-engined cabin monoplane designed by the Yakovlev design bureau.[1] The AIR-5 was a high-wing strut-braced monoplane with a 200 hp (149 kW) Wright J-4 Whirlwind engine.[1] It had a tubular steel fuselage, wooden wings and an enclosed cabin for a pilot and three passengers.[2]

When the Whirlwind engine became unavailable no further aircraft were produced and a smaller variant was designed with a locally-produced M-11 radial engine and designated the AIR-6.[2]

Specifications

Data from The History of Soviet Aircraft from 1918[3]

General characteristics

Performance


References

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Notes

  1. 1 2 Orbis 1985, p. 2296
  2. 1 2 Nemecek 1986, p. 271
  3. Nemecek 1986, pp. 428-429
  4. 1 2 3 4 Gordon, Komissarov and Komissarov 2005, p. 23.

Bibliography

  • Gordon, Yefim; Komissarov, Dmitry; Komissarov, Sergey (2005). OKB Yakovlev: A History of the Design Bureau and its Aircraft. Hinkley, UK: Midland Publishing. ISBN 1-85780-203-9. 
  • Nemecek, Vaclav (1986). The History of Soviet Aircraft from 1918. London: Willow Books. ISBN 0-00-218033-2. 
  • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. 
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