| Specifications
|
|---|
| Country of Origin | Russia
|
| Builder |
|
| Role |
|
| Similar Aircraft |
|
| Model | IL-96-300 | IL-96-400
|
| wing span | (m) 57,66 | (m) 60,105
|
| length (overall) | (m) 55,345 | (m) 63,939
|
| height (overall) | (m) 17,55 | (m) 15,717
|
| wing area | (m2) 350 | (m2) 350
|
| sweepback angle at 1/4-chord line | (degree) 30 | (degree) 30
|
| fuselage diameter | (m) 6,08 | (m) 6,08
|
| engine type | PS-90A by-pass turbojet engine | PS-90A by-pass turbojet engine
|
| number of engines (pcs) | 4 | 4
|
| max take-off thrust (International Standard Atmosphere, ?=0) | (kg) 4 ? 16000 | (kg) 4 ? 16000
|
| bypass ratio | 4,4 | 4,4
|
| ICAO standards compliance | App.16, Ch.3 | App.16, Ch.3
|
| max take-off weight | (t) 240 | (t) 265
|
| max payload | (t) 40 | (t) 58
|
| max fuel tanks capacity | (liter) 152620 | (liter) 152620
|
| cruise speed | (km/h) 850-870 | (km/h) 870
|
| range with max passenger capacity | (km) 9000 | (km) 10000
|
| flight altitude | (m) 10000-12000 | (m) 9000-12000
|
| take-off run distance | (m) 2700 | (m) 2700
|
| landing run distance | (m) 1260 | (m) 1650
|
| flight crew | 3 | 3
|
| passengers in single class version | 300 | 436
|
| two classes version | 262 | 386
|
| three classes version | 235 | 315
|
| Service Life calendar | 20 years | 20 years
|
| flights | 12000 | 20000
|
| flight hours | 60000 | 60000
|
| Cost |
|
| User Countries |
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