Antonow / Antonov An-14
Light STOL Utility Aircraft
Photo ©: Karsten Palt
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).
| Propulsion | 2 Radial Engines |
| Engine Model | Ivchenko AI-14RF |
| Engine Power (each) | 220 kW | 295 hp |
| Speed | 220 km/h | 119 kts
137 mph |
| Service Ceiling | 5.000 m | 16.404 ft |
| Range | 650 km | 351 NM
404 mi. |
| Empty Weight | 2.600 kg | 5.732 lbs |
| max. Takeoff Weight | 3.450 kg | 7.606 lbs |
| Wing Span | 21,99 m | 72 ft 2 in |
| Wing Area | 39,7 m² | 427 ft² |
| Length | 11,36 m | 37 ft 3 in |
| Height | 4,63 m | 15 ft 2 in |
| 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 |
