Manufacturer | UTVA |
Model | UTVA-75 |
Modification | UTVA-75А21 |
Country | Yugoslavia |
Years | 1976 |
Type | Reconnaissance aircraft |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 9.73 m |
Length | 7.11 m |
Height | 3.15 m |
Wing area | 14.63 m2 |
Zero fuel weight | - |
Empty weight | 685 kg |
Maximum takeoff weight | 960 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 1 Textron Lycoming IO-360-B1F |
Power | 1 x 180 HP |
Thrust | - |
Maximum speed | 215 km/h |
Cruising speed | 185 km/h |
Rate of climb | - |
Practical range | 2000 km |
Service ceiling | 4000 m |
Hovering ceiling | - |
Crew | 2 |