| Manufacturer |
Ilyushin |
Antonov |
| Description |
The Ilyushin Il-112/Il-212 () is a high-wing light military transport aircraft being developed by Ilyushin Aviation Complex (JSC IL) for air landing and airdrop of military air cargo, equipment and personnel. |
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 |
2019-03-30 |
1959-10-29 |
| Entry Into service |
2023-01-01 |
1962-01-01 |
| Production End |
|
1976-01-01 |
| Designer |
Ilyushin |
Antonov |
| Type |
Light military transport |
Regional airliner / military transport |
| Length (m) |
24.15 |
23.53 |
| Height (m) |
8.89 |
8.32 |
| Cockpit Crew |
|
3 |
| Max Seating |
44 |
50 |
| Max Speed (km/h) |
|
485 |
| Cruise Speed (km/h) |
450 |
450 |
| Max Ceiling (m) |
7600 |
8400 |
| Capacity Description |
5,000 kg; 44 passengers |
50 passengers |
| National Origin |
Russia |
Soviet Union |
| Number Built |
2 |
1367 |
| Powerplant Description |
2 × Klimov TV7-117ST turboprop, 2610 kW (3500 hp) each |
2 × Ivchenko AI-24A turboprop engines, 1902 kW (2550 hp) each |
| Primary Users |
Russian Aerospace Forces |
Aeroflot (former) |
| Status |
In development |
In service |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Ilyushin_Il-112 |
en.wikipedia.org/wiki/Antonov_An-24 |
| Flat Wing Span (m) |
27.6 |
29.2 |
| Flat Wing Area (m²) |
65 |
74.98 |
| Flat Wing Aspect Ratio |
|
11.7 |
| Wake Category |
|
M |
| Aircraft Engine |
|
Ivchenko AI-24 |
| Number of Engines |
2 |
2 |