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Ilyushin Il-62
Aircraft type: Commercial airplane
Manufacturer: Ilyushin
Maiden flight year: 1963
Copyright Alexandr Zhukov
Ilyushin Il-62 Specifications
| Il-62 | Il-62M | |
Dimensions | ||
|---|---|---|
| Length (m) | 53.1 | 53.1 |
| Wingspan (m) | 43.2 | 43.2 |
| Height (m) | 12.3 | 12.3 |
| Wing area (m2) | 279.5 | 279.5 |
Weight | ||
| Maximum take-off weight (kg) | 161 600 | 165 000 |
| Maximum landing weight (kg) | 110 000 | |
| Operating empty weight (kg) | 70 400 | 74 000 |
| Maximum zero fuel weight (kg) | 97 500 | |
| Maximum payload (kg) | 25 000 | |
| Standard fuel capacity (litres) | 105 300 | |
Performance | ||
| Maximum range (km) | 10 000 | 11 000 |
| Range with max payload (km) | 6 700 | 8 000 |
| Cruise speed (km/h) | 850 | 850 |
| Maximum speed (km/h) | 870 | 870 |
| Maximum operating altitude (m) | 12 000 | 12 000 |
| Take-off field length (m) | 3 150 | |
| Landing field length (m) | 2 500 | |
| Engines | NK-8, 4 x 21000 lb | D-30KU, 4 x 24240 lb |
| Fuel efficiency (g/pass*km) | 46.6 | |
| Fuel flow rate (kg/h) | 7 300 | 6 600 |
Cabin Data | ||
| Passengers (1-class) | 180 | 180 |
| Passengers (2-class) | 144 | 144 |
| Cabin width (m) | 3.45 | 3.45 |
Ilyushin Il-62 Airplane
| 75% | 15% | 10% |
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