Il-62 Classic
| Specifications | |
|---|---|
| Country of Origin | Russia |
| Builder | |
| Role | Il-62M - long-range transport |
| Similar Aircraft | VC-10 |
| Wing Span | 43.20 m |
| Wing Area | 279.55 / 282.20 M2 |
| Length | 53.12 m |
| Height | 12.35 m |
| Wing sweep on line 1/4 chord | (degree) 32° 30' |
| Maximum fuselage width | 3,75 ( m ) |
| Dimensions of passenger cabin |
Maximum width 3,49 ( m ) Maximum height 2,12 ( m ) Capacity 163 ( m3 ) |
| Weight |
Empty weight 69,400 kg - 71,600 MTOW 165,000 kg Landing 105,600 Fuel reserve 105,600 |
| Engine |
ILyushin IL-62: Four Kuznetsov NK-8-4 ILyushin IL-62M: Four Soloviev D-30KU |
| Maximum speed | 900 km/h (cruising at opt. alt.) |
| Cruising speed | 850 km/h |
| Range with max payload | 7,800 km |
| Range with max payload | 8,800 km (with fuel reserve) |
| Range with payload 6 (t) | 11050 km (with fuel reserve) |
| Range with max fuel | |
| Service Ceiling | 12,000 meters |
| Required length VPP | 3,000 meters (at sea level) |
| Armament | none |
| Crew | 5 |
| Payload | 23 tons 138-198 passengers |
| Cost | |
| User Countries | |
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