Antonow / Antonov An-10
Airliner
The Antonov An-10 is a four-engine turboprop airliner with a capacity of maximum 132 passengers by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
The Antonov An-10 was in operation with the Soviet Aeroflot and the Soviet Air Force only.
| Propulsion | 4 Turboprop Engines |
| Engine Model | Ivchenko AI-20K |
| Engine Power (each) | 2940 kW | 3943 shp |
| Speed | 726 km/h | 392 kts
451 mph |
| Service Ceiling | 12.000 m | 39.370 ft |
| Range | 4.074 km | 2.200 NM
2.532 mi. |
| Empty Weight | 30.500 kg | 67.241 lbs |
| max. Takeoff Weight | 55.000 kg | 121.254 lbs |
| Wing Span | 38,00 m | 124 ft 8 in |
| Wing Area | 121,7 m² | 1310 ft² |
| Length | 37,00 m | 121 ft 5 in |
| Height | 9,80 m | 32 ft 2 in |
| 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 |
