The Antonov An-32 is a twin-engined turboprop transport aircraft for operations in hot and heigh regions by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine). The An-32 is in operation with both military and civil operators.
Crew | 3 | |
Propulsion | 2 Turboprop Engines | |
Engine Model | Iwtschenko / Ivchenko / ZMKB Progress AI-24M | |
Engine Power (each) | 3812 kW | 5112 shp |
Speed | 641 km/h | 346 kts |
Service Ceiling | 9.500 m | 31.168 ft |
Range | 2.500 km | 1.350 NM |
Empty Weight | 16.800 kg | 37.038 lbs |
max. Takeoff Weight | 27.000 kg | 59.525 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 | 1978 | |
Production Status | out of production | |
Total Production | 356 | |
ICAO Code | AN32 | |
IATA Code | AN6 | |
NATO Code | Cline | |
Data for (Version) | Antonov / Antonow An-32 |
Remarks
The An-32 is a development of the Antonov An-26.
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