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