Iljuschin / Ilyushin Il-96
Airliner
The Ilyushin Il-96 is a four-engine long-range widebody airliner for max. 300 passengers developed by the Soviet design bureau Ilyushin OKB, today JSC Ilyushin Aviation Complex, Russia.
The Il-96 is a shortened long-range development of the
Ilyushin Il-86. The Il-96-400 is a stretched version (length 63,94m / 209ft 9in).
| Propulsion | 4 Turbofan Engines |
| Engine Model | Aviadvigatel PS-90A |
| Engine Power (each) | 156,9 kN | 35273 lbf |
| Speed | 900 km/h | 486 kts
559 mph |
| Service Ceiling | 13.100 m | 42.979 ft |
| Range | 11.001 km | 5.940 NM
6.836 mi. |
| Empty Weight | 117.000 kg | 257.941 lbs |
| max. Takeoff Weight | 216.000 kg | 476.199 lbs |
| Wing Span | 60,10 m | 197 ft 2 in |
| Wing Area | 391,6 m² | 4215 ft² |
| Length | 55,30 m | 181 ft 5 in |
| Height | 17,50 m | 57 ft 5 in |
| First Flight | 28.09.1988 |
| Production Status | in production |
| ICAO Code | IL96 |
| IATA Code | I93 I9F I9M I9X I9Y |
| Data for (Version) | Iljuschin / Ilyushin Il-96-300 |
| Variants | Il-96-300, Il-96-400, Il-96-400T |
