Utva 66
| Utva 66 | |
|---|---|
 Utva 66 Hydro |
|
| Type: | STOL - liaison aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
1966 |
| Number of pieces: |
130 |
.svg){kind=small}
The Utva 66 ( Serbian - Cyrillic Утва 66 ) is a STOL aircraft made by the Yugoslav manufacturer Utva . It was developed from the Utva 60 and first flew in 1966.
construction
The Utva 66 is a single-engine, braced shoulder-wing monoplane with STOL properties, offers space for four people and can be deployed from unprepared runways. The aircraft has a fixed tail wheel landing gear and can also be equipped with floats or skis. The cockpit is equipped with double controls, so that the machine can also be used as a training aircraft. Instead of the right front and rear seats, two stretchers could be accommodated. The last aircraft were taken out of service in 1999.
variants
Utva 66 in the Belgrade Aviation Museum
- Utva 66 - production model
- Utva 66AM - ambulance version
- Utva 66H - seaplane
- Utva 66V - military version
- Utva 66AG - agricultural version
Military users
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1-2 |
| Passengers | 2–3 / 2 stretchers |
| length | 8.38 m |
| span | 11.40 m |
| height | 3.20 m |
| Wing area | 18.80 m² |
| Wing extension | 6.9 |
| payload | 569 kg |
| Empty mass | 1251 kg |
| Max. Takeoff mass | 1820 kg |
| Top speed | 230 km / h |
| Service ceiling | 6700 m |
| Range | 746 km |
| Engines | 1 × Lycoming GSO-480-B1J6 piston engine with 201 kW (273 PS ) |
See also
Web links
Commons : Utva-66 - collection of images, videos and audio files
- Utva 66 data sheet (Serbian)
- MUZEJ JUGOSLOVENSKOG RATNOG VAZDUHOPLOVSTVA (Serbian)