The Antonov An-12 is a four-engine transport aircraft by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine). The An-12 was mainly in military operation.
| Crew | 2+3 | |
| Propulsion | 4 Turboprop Engines | |
| Engine Model | Iwtschenko / Ivchenko / ZMKB Progress AI-20M | |
| Engine Power (each) | 3125 kW | 4191 shp |
| Speed | 650 km/h | 351 kts |
| Service Ceiling | 10.200 m | 33.464 ft |
| Range | 3.400 km | 1.836 NM |
| Empty Weight | 30.500 kg | 67.241 lbs |
| max. Takeoff Weight | 61.000 kg | 134.482 lbs |
| Wing Span | 38,00 m | 124,7 ft |
| Wing Area | 121,7 m² | 1310 ft² |
| Length | 33,10 m | 108,6 ft |
| Height | 10,53 m | 34,5 ft |
| First Flight | März 1957 | |
| Production Status | out of production | |
| Production Range | 1958-1973 | |
| Total Production | 1248 | |
| ICAO Code | AN12 | |
| IATA Code | ANF | |
| NATO Code | Cub | |
| Data for (Version) | Antonov / Antonow An-12 |
Remarks
The Antonov An-12 was produced in several different variants including combined freight and passenger variants. The An-12 was license-produced in the Peoples Republic of China as Shaanxi Y-8.
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