Utva Trojka
| Utva C-3 Trojka | |
|---|---|
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| Type: | Trainer aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
1946 |
| Number of pieces: |
about 80 |
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The Utva C-3 Trojka ( Serbian - Cyrillic Утва БЦ-3 Тројка ) was a trainer aircraft made by the Yugoslav manufacturer Utva .
History and construction
The Utva C-3 Troika was a light trainer aircraft developed in Yugoslavia shortly after World War II as a result of a government competition to equip flying clubs with a country-built aircraft. The winning design was submitted by Boris Cijan and Dragoslav Petkovic , and the prototype was built by Ikarus as Ikarus 251 . The serial production took place at Utva under the designation C-3 . The aircraft was a conventional low wing aircraft with a fixed tail wheel landing gear . The teacher and student sat side by side in a closed cabin with a sliding roof. The model was produced until the mid-1950s.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 2 |
| length | 8.84 m |
| span | 10.49 m |
| height | 2.08 m |
| Wing area | 15.5 m² |
| Empty mass | 374 kg |
| Max. Takeoff mass | 602 kg |
| Top speed | 166 km / h |
| Service ceiling | 3900 m |
| Range | 605 km |
| Engines | 1 × Walter Mikron III with 49 kW (67 PS ) |
See also
literature
- Michael JH Taylor: Jane's Encyclopedia of Aviation . Studio Editions, London 1989, pp. 430-31.
- RW Simpson: Airlife's General Aviation . Airlife Publishing, Shrewsbury 1995, p. 396.
Web links
Commons : Utva Trojka - collection of images, videos and audio files
