IL96-400
Caractéristiques techniques IL96-400
| Dimensions (external) | |
|---|---|
| wing span (m) | 60,105 |
| length (overall) (m) | 63,939 |
| height (overall) (m) | 15,717 |
| wing area (m2) | 350 |
| sweepback angle at 1/4-chord line (degree) | 30 |
| fuselage diameter (m) | 6,08 |
Engines |
|
| engine type | PS-90A by-pass turbojet engine |
| number of engines (pcs) | 4 |
| max take-off thrust (International Standard Atmosphere, Н=0) (kg) | 4 х 16000 |
| bypass ratio | 4,4 |
| ICAO standards compliance | App.16, Ch.3 |
Weights and Volumes |
|
| max take-off weight (t) | 265 |
| max payload (t) | 58 |
| max fuel tanks capacity (liter) | 152620 |
Performance |
|
| cruise speed (km/h) | 870 |
| range with max passenger capacity (km) | 10000 |
| flight altitude (m) | 9000-12000 |
| take-off run distance (m) | 2700 |
| landing run distance (m) | 1650 |
Seats |
|
| flight crew | 3 |
| passengers in | single class version – 436 two classes version – 386 three classes version – 315 |