The Antonov An-26 is a twin-engined turboprop short-to medium-range military transport aircraft by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
| Crew | 4 | |
| Passengers | max. 40 | |
| Propulsion | 2 Turboprop Engines | |
| Engine Model | Iwtschenko / Ivchenko / ZMKB Progress AI-24T | |
| Engine Power (each) | 2075 kW | 2783 shp |
| Speed | 435 km/h | 235 kts |
| Service Ceiling | 8.100 m | 26.575 ft |
| Range | 900 km | 486 NM |
| Empty Weight | 15.020 kg | 33.113 lbs |
| max. Takeoff Weight | 24.000 kg | 52.911 lbs |
| Wing Span | 29,20 m | 95,8 ft |
| Wing Area | 75,0 m² | 807 ft² |
| Length | 23,80 m | 78,1 ft |
| Height | 8,58 m | 28,1 ft |
| First Flight | 21.05.1969 | |
| Production Status | out of production | |
| Total Production | >1700 | |
| ICAO Code | AN26 | |
| IATA Code | AN6 | |
| NATO Code | Curl | |
| Data for (Version) | Antonov / Antonow An-26 |
Remarks
The An-26 is a military development of the Antonov An-24.
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