The Antonov An-14 is a twin-engined multi-purpose STOL transport aircraft developed by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
| Crew | 2 | |
| Passengers | 7 | |
| Propulsion | 2 Radial Engines | |
| Engine Model | Iwtschenko / Ivchenko / ZMKB Progress AI-14RF | |
| Engine Power (each) | 220 kW | 295 hp |
| Speed | 220 km/h | 119 kts |
| Service Ceiling | 5.000 m | 16.404 ft |
| Range | 650 km | 351 NM |
| Empty Weight | 2.600 kg | 5.732 lbs |
| max. Takeoff Weight | 3.450 kg | 7.606 lbs |
| Wing Span | 21,99 m | 72,1 ft |
| Wing Area | 39,7 m² | 427 ft² |
| Length | 11,36 m | 37,3 ft |
| Height | 4,63 m | 15,2 ft |
| First Flight | 15.03.1958 | |
| Production Status | out of production | |
| Production Range | 1966-1972 | |
| Total Production | ca. 300 | |
| NATO Code | Clod | |
| Data for (Version) | Antonov / Antonow An-14 |
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