Ilyushin Il-96
First flight year — 1988
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Ilyushin Il-96 Specifications
| Il-96-300 | Il-96-400 | |
| Dimensions | ||
| Length (m) | 55.3 | 64.0 |
| Wingspan (m) | 60.1 | 60.1 |
| Height (m) | 17.6 | 15.7 |
| Wing area (m2) | 391.6 | 350.0 |
| Weight | ||
| Maximum take-off weight (kg) | 216 000 | 265 000 |
| Maximum landing weight (kg) | 175 000 | |
| Operating empty weight (kg) | 117 000 | 122 300 |
| Maximum zero fuel weight (kg) | 157 000 | |
| Maximum payload (kg) | 40 000 | 58 000 |
| Standard fuel capacity (litres) | 150 400 | |
| Performance | ||
| Range with max payload (km) | 7 500 | 10 000 |
| Cruise speed (km/h) | 900 | 870 |
| Maximum speed (km/h) | 910 | 900 |
| Maximum operating altitude (m) | 12 100 | 12 100 |
| Take-off field length (m) | 2 600 | 2 700 |
| Landing field length (m) | 1 980 | |
| Engines | PS-90A, 4 x 35250 lb | PS-90A1, 4 x 38300 lb |
| Fuel efficiency (g/pass*km) | 26.4 | |
| Fuel flow rate (kg/h) | 6 700 | |
| Cabin Data | ||
| Passengers (1-class) | 300 | 435 |
| Passengers (3-class) | 235 | 315 |
| Cabin width (m) | 5.7 | 5.7 |
Typical Cabin Configuration of Ilyushin Il-96
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