| Manufacturer | Shorts |
| Model | C-23 Sherpa |
| Modification | С-23А |
| Country | United Kingdom, USA |
| Years | 1984 |
| Type | Transport aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 22.76 m |
| Length | 17.69 m |
| Height | 4.95 m |
| Wing area | 42.08 m2 |
| Zero fuel weight | - |
| Empty weight | 6680 kg |
| Maximum takeoff weight | 11566 kg |
| Normal takeoff weight | 10390 kg |
| Flight duration | - |
| Engine | 2 Pratt Whitney Canada T101-CP-100 PT6A-45R |
| Power | 2 x 1200 HP |
| Thrust | - |
| Maximum speed | - |
| Cruising speed | 352 km/h |
| Rate of climb | - |
| Practical range | 1240 km |
| Service ceiling | 6095 m |
| Hovering ceiling | - |
| Crew | 2-3 |
