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Ilyushin Il-62
First flight year — 1963
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Ilyushin Il-62 Specifications
| Il-62M | |
| Dimensions | |
| Length (m) | 53.1 |
| Wingspan (m) | 43.2 |
| Height (m) | 12.3 |
| Wing area (m2) | 279.5 |
| Weight | |
| Maximum take-off weight (kg) | 165 000 |
| Maximum landing weight (kg) | 110 000 |
| Operating empty weight (kg) | 74 000 |
| Maximum zero fuel weight (kg) | 97 500 |
| Maximum payload (kg) | 25 000 |
| Standard fuel capacity (litres) | 105 300 |
| Performance | |
| Range with max payload (km) | 8 000 |
| Maximum cruise speed (km/h) | 830 |
| Take-off field length (m) | 3 150 |
| Landing field length (m) | 2 500 |
| Engines | D-30KU, 4 x 24240 lb |
| Fuel efficiency (g/pass*km) | 46.6 |
| Fuel flow rate (kg/h) | 6 600 |
| Cabin Data | |
| Passengers (1-class) | 180 |
| Passengers (2-class) | 144 |
| Cabin width (m) | 3.45 |
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