Iljuschin / Ilyushin Il-86
Airliner
The Ilyushin Il-86 is a four-engine medium-range widebody airliner for max. 350 passengers developed by the Soviet design bureau Ilyushin OKB, today JSC Ilyushin Aviation Complex, Russia.
| Propulsion | 4 Turbofan Engines |
| Engine Model | Kuznetsov NK-86 |
| Engine Power (each) | 127,5 kN | 28663 lbf |
| Speed | 950 km/h | 513 kts
590 mph |
| Service Ceiling | 12.000 m | 39.370 ft |
| Range | 4.600 km | 2.484 NM
2.859 mi. |
| Empty Weight | 121.000 kg | 266.759 lbs |
| max. Takeoff Weight | 208.000 kg | 458.562 lbs |
| Wing Span | 48,00 m | 157 ft 6 in |
| Wing Area | 300,0 m² | 3229 ft² |
| Length | 59,40 m | 194 ft 11 in |
| Height | 15,80 m | 51 ft 10 in |
| First Flight | 22.12.1976 |
| Production Status | out of production |
| Production Range | 1977-1994 |
| Total Production | 103 |
| ICAO Code | IL86 |
| IATA Code | ILW |
| NATO Code | Camber Maxdome |
| Data for (Version) | Iljuschin / Ilyushin Il-86 |
