Antonow / Antonov An-32
Utility Aircraft
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.
| Propulsion | 2 Turboprop Engines |
| Engine Model | Ivchenko AI-20M |
| Engine Power (each) | 3169 kW | 4250 shp |
| Speed | 641 km/h | 346 kts
398 mph |
| Service Ceiling | 9.500 m | 31.168 ft |
| Range | 2.500 km | 1.350 NM
1.554 mi. |
| Empty Weight | 16.800 kg | 37.038 lbs |
| max. Takeoff Weight | 27.000 kg | 59.525 lbs |
| Wing Span | 29,20 m | 95 ft 10 in |
| Wing Area | 75,0 m² | 807 ft² |
| Length | 23,80 m | 78 ft 1 in |
| Height | 8,58 m | 28 ft 2 in |
| First Flight | 1978 |
| Production Status | out of production |
| Total Production | 356 |
| ICAO Code | AN32 |
| IATA Code | A32 |
| NATO Code | Cline |
| Data for (Version) | Antonov / Antonow An-32 |
