The Antonov An-8 is a twin-engined military transport aircraft by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
| Crew | 6 | |
| Propulsion | 2 Turboprop Engines | |
| Engine Model | Iwtschenko / Ivchenko / ZMKB Progress AI-20D | |
| Engine Power (each) | 3082 kW | 4133 shp |
| Speed | 520 km/h | 281 kts |
| Service Ceiling | 9.600 m | 31.496 ft |
| Range | 3.900 km | 2.106 NM |
| Empty Weight | 24.400 kg | 53.793 lbs |
| max. Takeoff Weight | 43.400 kg | 95.680 lbs |
| Wing Span | 37,00 m | 121,4 ft |
| Wing Area | 117,2 m² | 1262 ft² |
| Length | 30,70 m | 100,7 ft |
| Height | 9,70 m | 31,8 ft |
| First Flight | 11.02.1956 | |
| Production Status | out of production | |
| Production Range | 1957-1961 | |
| Total Production | 151 | |
| ICAO Code | AN8 | |
| NATO Code | Camp | |
| Data for (Version) | Antonov / Antonow An-8 |
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