Utva 75
| Utva 75 | |
|---|---|
|
|
| Type: | Beginner training aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
May 19, 1976 |
| Commissioning: |
1977 |
| Number of pieces: |
138 |
.svg){kind=small}
The Utva 75 ( Serbian - Cyrillic Утва 75 ) is a compact piston-engine powered airplane from the former Yugoslav and now Serbian manufacturer Utva . It is mainly used as a novice military training and sport aircraft .
history
The Utva 75 was designed to replace the Utva Aero 3 as a beginner trainer aircraft in the Yugoslav Air Force. More than a hundred copies were built and served in the former Yugoslav Air Force. After the fall of Yugoslavia, many were used in the successor states. The last two Utva 75 were produced in 2003 and exported to the USA.
Versions
- Utva-75A21 - two-seater with double controls, approved for blind and instrument flight.
- Utva-75A41 - four-seater with advanced avionics, first flown in 1986
Military users
-
Yugoslavia
-
Bosnia and Herzegovina ( Oružane snage Bosne i Hercegovine ): 2 -
Croatia : 11 -
North Macedonia : 4 -
Montenegro : 3 -
Serbia : 12 -
Slovenia : 12 -
Sudan : 6 (since 2009)
Technical specifications
| Parameter | Data (Utva 75A21) |
|---|---|
| crew | 2 |
| length | 7.11 m |
| span | 9.73 m |
| height | 3.15 m |
| Wing area | 14.63 m² * |
| Empty mass | 685 kg |
| Max. Takeoff mass | 1140 kg |
| Cruising speed | 175 km / h |
| Top speed | 215 km / h |
| Landing speed | 82 km / h * |
| Rate of climb | 4.6 m / s * |
| Service ceiling | 4000 m |
| Range | 800 km |
| Take-off / landing runway | 125 m / 100 m * |
| Engines | 1 Lycoming IO360 -B1F with 134 kW (182 PS ) |
* Data from Fliegerrevue No. 7/1987, p. 225
literature
- J. W. R. Taylor: Jane's All the World's Aircraft 1981-82 . 1981, p. 472 .
Web links
Commons : UTVA-75 - collection of pictures, videos and audio files
