The Antonov An-140 is a twin-engined turboprop regional airliner with a capacity of maximum 52 passengers developed by the Ukraine manufacturer Antonov ASTC.
| Crew | 2 | |
| Passengers | 52 | |
| Propulsion | 2 Turboprop Engines | |
| Engine Model | Klimow / Klimov (Pratt & Whitney Canada) Tw3-117WMA-SBM1 (PW127A) | |
| Engine Power (each) | 1838 (1900) kW | 2465 (2548) shp |
| Speed | 533 km/h | 288 kts |
| Service Ceiling | 7.200 m | 23.622 ft |
| Range | 1.380 km | 745 NM |
| Empty Weight | 11.800 kg | 26.015 lbs |
| max. Takeoff Weight | 21.500 kg | 47.400 lbs |
| Wing Span | 25,50 m | 83,7 ft |
| Wing Area | 51,0 m² | 549 ft² |
| Length | 22,46 m | 73,7 ft |
| Height | 8,03 m | 26,3 ft |
| First Flight | 17. Sep. 1997 | |
| Production Status | in production | |
| ICAO Code | A140 | |
| IATA Code | A40 | |
| Data for (Version) | Antonov / Antonow An-140-100 | |
| Variants | IRAN-140 Faraz |
Remarks
The An-140 is also license-produced HESA (Iran) as IRAN-140 Faraz
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