| Manufacturer |
Antonov |
| Description |
The Antonov An-24 (Russian/Ukrainian: Антонов Ан-24; NATO reporting name: Coke) is a 50-seat twin turboprop regional airliner designed in 1957 in the Soviet Union by the Antonov Design Bureau. |
| ICAO Code |
AN24 |
| First Flight |
1959-10-29 |
| Entry Into service |
1962-01-01 |
| Production End |
1976-01-01 |
| Designer |
Antonov |
| Type |
Regional airliner / military transport |
| Length (m) |
23.53 |
| Height (m) |
8.32 |
| Cockpit Crew |
3 |
| Max Seating |
50 |
| Max Speed (km/h) |
485 |
| Cruise Speed (km/h) |
450 |
| Max Ceiling (m) |
8400 |
| Capacity Description |
50 passengers |
| National Origin |
Soviet Union |
| Number Built |
1367 |
| Powerplant Description |
2 × Ivchenko AI-24A turboprop engines, 1902 kW (2550 hp) each |
| Primary Users |
Aeroflot (former) |
| Status |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Antonov_An-24 |
| Flat Wing Span (m) |
29.2 |
| Flat Wing Area (m²) |
74.98 |
| Flat Wing Aspect Ratio |
11.7 |
| Wake Category |
M |
| Aircraft Engine |
Ivchenko AI-24 |
| Number of Engines |
2 |