UTVA / Lola-Utva UTVA 75
Trainer / Touring Aircraft
The UTVA 75 is a single-engine two-seat light trainer and touring aircraft produced by the Yugoslav manufacturer UTVA.
Today (2014) Safat Aviation from Sudan offers a modernized variant of the UTVA 75 as the Safat 03.
| Propulsion | 1 Piston Engine |
| Engine Model | Lycoming IO-360-B1F |
| Engine Power | 134 kW | 180 hp |
| Speed | 215 km/h | 116 kts
133 mph |
| Service Ceiling | 4.000 m | 13.123 ft |
| Range | 800 km | 432 NM
497 mi. |
| Empty Weight | 685 kg | 1.510 lbs |
| max. Takeoff Weight | 1.140 kg | 2.513 lbs |
| Wing Span | 9,73 m | 31 ft 11 in |
| Wing Area | 14,6 m² | 157 ft² |
| Length | 7,11 m | 23 ft 4 in |
| Height | 3,15 m | 10 ft 4 in |
| First Flight | 19.05.1976 |
| Production Status | out of production |
| Total Production | 138 |
| ICAO Code | UT75 |
| Data for (Version) | UTVA 75 |
