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Utva Trojka

From Wikipedia, the free encyclopedia
C-3 Trojka
An Utva Trojka on display at theTechnical Museum inZagreb
RoleCivil trainer
Type of aircraft
National originYugoslavia
ManufacturerIkarus,Utva
First flight1946
Number builtca.80

TheUtva C-3Trojka (Trey) was a light aircraft built in Yugoslavia shortly after World War II as a result of a government competition to develop a new, domestically built aircraft with which to equip the country's flying clubs. The winning design was submitted byBoris Cijan andDjordje T. Petković and the prototype was built byIkarus as theIkarus 251. Series production took place atUtva as theC-3. It was a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage. The pilot and instructor sat side by side under an expansive canopy. The type remained in production until the mid-1950s with later examples powered by the more powerfulWalter Mikron 4.

Operators

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 Yugoslavia

Specifications

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General characteristics

  • Crew: Two, pilot and instructor
  • Length: 8.84 m (29 ft 0 in)
  • Wingspan: 10.49 m (34 ft 5 in)
  • Height: 2.08 m (6 ft 10 in)
  • Wing area: 15.5 m2 (16.7 sq ft)
  • Empty weight: 374 kg (824 lb)
  • Gross weight: 602 kg (1,328 lb)
  • Powerplant: 1 ×Walter Mikron III , 49 kW (65 hp)

Performance

  • Maximum speed: 166 km/h (103 mph, 90 kn)
  • Range: 605 km (376 mi, 327 nmi)
  • Service ceiling: 3,900 m (12,800 ft)

See also

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Aircraft of comparable role, configuration, and era

References

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Wikimedia Commons has media related toUtva Trojka.
  • Taylor, Michael J. H. (1989).Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 430–31.
  • Simpson, R. W. (1995).Airlife's General Aviation. Shrewsbury: Airlife Publishing. p. 396.
  • "Utva BC-3 Trojka".Insignia: 144. Summer 1999.
  • Јанић, Чедомир; Петровић, Огњан (2017).Творци ваздухопловства Краљевине Југославије. Београд: Музеј науке и технике. pp. 170 & 230.ISBN 978-86-82977-60-5.
Ikarus aircraft
Domestic aircraft
License-built aircraft
Aircraft produced byUtva
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