The Antonov An-28 is a twin-engined turboprop multi-purpose STOL transport aircraft developed by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
| Crew | 1-2 | |
| Passengers | max. 14 | |
| Propulsion | 2 Turboprop Engines | |
| Engine Model | Gluschenkow / Glushenkov TWD-10B / TVD-10B | |
| Engine Power (each) | 705 kW | 945 shp |
| Speed | 350 km/h | 189 kts |
| Service Ceiling | 6.000 m | 19.685 ft |
| Range | 509 km | 275 NM |
| Empty Weight | 3.500 kg | 7.716 lbs |
| max. Takeoff Weight | 6.100 kg | 13.448 lbs |
| Wing Span | 22,06 m | 72,4 ft |
| Wing Area | 40,3 m² | 434 ft² |
| Length | 12,98 m | 42,6 ft |
| Height | 4,60 m | 15,1 ft |
| First Flight | September 1969 | |
| Production Status | out of production | |
| Production Range | 1975-1993 | |
| Total Production | 191 | |
| ICAO Code | AN28 | |
| IATA Code | A28 | |
| NATO Code | Cash | |
| Data for (Version) | Antonov / Antonow An-28 |
Remarks
The An-28 is a turboprop-powered development of the Antonov An-14. The An-28 was license-produced by PZL-Mielec in Poland.
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