Antonow / Antonov An-3
Utility Aircraft
The Antonov An-3 is a single-engine turboprop powered multi-purpose biplane aircraft developed by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
The An-3 is a tdevelopment of the
Antonov An-2. Although maiden flight was in 1980, first An-3 were delivered in late 1990's. Most An-3 are converted An-2.
| Propulsion | 1 Turboprop Engine |
| Engine Model | Glushenkov TWD-20M / TVD-20M |
| Engine Power | 1066 kW | 1430 shp |
| Speed | 259 km/h | 140 kts
161 mph |
| Service Ceiling | 4.400 m | 14.436 ft |
| Range | 1.024 km | 553 NM
636 mi. |
| Empty Weight | 3.200 kg | 7.055 lbs |
| max. Takeoff Weight | 5.800 kg | 12.787 lbs |
| Wing Span | 18,20 m | 59 ft 9 in |
| Wing Area | 43,6 m² | 469 ft² |
| Length | 14,00 m | 45 ft 11 in |
| Height | 4,00 m | 13 ft 1 in |
| First Flight | 13.05.1980 |
| Production Status | in production |
| ICAO Code | AN3 |
| Data for (Version) | Antonov / Antonow An-3T |
