Antonow / Antonov An-24
Short-Range Utility Aircraft
The Antonov An-24 is a twin-engined turboprop short-range transport- and passenger aircraft by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
Some of the several produced variants are equipped with an additional turbojet engine Tumanski RU-19A-30 with 8,8 kN (1978 lbf) thrust, installed in the right-hand engine nacelle. This engine served as an APU (Auxiliary Power Unit) and for improvement of the start performance. The An-24 is today still in license-production in several variants in the Peoples Republic of China as the Harbin Y-5.
Crew | 2+1 | |
Passengers | max. 50 |
Propulsion | 2 Turboprop Engines | |
Engine Model | Ivchenko AI-24 | |
Engine Power (each) | 1875 kW | 2514 shp |
Speed | 450 km/h | 243 kts 280 mph |
Service Ceiling | 8.400 m | 27.559 ft |
Range | 550 km | 297 NM 342 mi. |
Empty Weight | 13.300 kg | 29.321 lbs |
max. Takeoff Weight | 21.000 kg | 46.297 lbs |
Wing Span | 29,20 m | 95 ft 10 in |
Wing Area | 75,0 m² | 807 ft² |
Length | 23,53 m | 77 ft 2 in |
Height | 8,32 m | 27 ft 4 in |
First Flight | April 1960 | |
Production Status | out of production | |
Total Production | ca. 1100 |
ICAO Code | AN24 | |
IATA Code | AN4 | |
NATO Code | Coke | |
Data for (Version) | Antonov / Antonow An-24 |
[Photo-ID: 10473] © Karsten Palt 2014-06-08 | |
Antonov An-24V Czech Air Force Reg.: 7109 c/n: 17307109 | |
Letecke Muzeum Kbely [Prague] |
[Photo-ID: 10474] © Karsten Palt 2014-06-08 | |
Antonov An-24V Czech Air Force Reg.: 7109 c/n: 17307109 | |
Letecke Muzeum Kbely [Prague] |