| Manufacturer | Cessna |
| Model | U-27 |
| Modification | U-27 |
| Country | USA |
| Years | 1985 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 15.88 m |
| Length | 11.46 m |
| Height | 4.32 m |
| Wing area | 25.96 m2 |
| Zero fuel weight | - |
| Empty weight | 1752 kg |
| Maximum takeoff weight | 3629 kg |
| Normal takeoff weight | - |
| Flight duration | - |
| Engine | 1 Pratt Whitney Canada PT6A-114А |
| Power | 1 x 503 HP |
| Thrust | - |
| Maximum speed | 352 km/h |
| Cruising speed | 341 km/h |
| Rate of climb | - |
| Practical range | 2539 km |
| Service ceiling | 7770 m |
| Hovering ceiling | - |
| Crew | 1 |
