The Antonov An-10 is a four-engine turboprop airliner with a capacity of maximum 132 passengers by the Soviet design bureau <I>OKB Antonov (today Antonov ASTC, Ukraine)</I>.
| Crew | 3 | |
| Passengers | 84-132 | |
| Propulsion | 4 Turboprop Engines | |
| Engine Model | Iwtschenko / Ivchenko / ZMKB Progress AI-20K | |
| Engine Power (each) | 2940 kW | 3943 shp |
| Speed | 726 km/h | 392 kts |
| Service Ceiling | 12.000 m | 39.370 ft |
| Range | 4.074 km | 2.200 NM |
| Empty Weight | 30.500 kg | 67.241 lbs |
| max. Takeoff Weight | 55.000 kg | 121.254 lbs |
| Wing Span | 38,00 m | 124,7 ft |
| Wing Area | 121,7 m² | 1310 ft² |
| Length | 37,00 m | 121,4 ft |
| Height | 9,80 m | 32,2 ft |
| First Flight | 07.03.1957 | |
| Production Status | out of production | |
| Total Production | 108 | |
| NATO Code | Cat | |
| Data for (Version) | Antonov / Antonow An-10A | |
| Variants | An-10, An-10A, An-10B, An-10AS, An-10TS |
Remarks
The Antonov An-10 was in operation with the Soviet Aeroflot and the Soviet Air Force only.
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