Il-86 Camber
Dimensions (external) | |
|---|---|
| wing span (m) | 48,06 |
| length (overall) (m) | 59,54 |
| height (overall) (m) | 15,5 |
| wing area (m2) | 361 |
| sweepback angle at 1/4-chord line (degree) | 35 |
| fuselage diameter (m) | 6,08 |
Engines | |
| engine type | NK-86 by-pass turbojet engine |
| number of engines (pcs) | 4 |
| max take-off thrust (International Standard Atmosphere, Í=0) (kg) | 4 õ 13000 |
| bypass ratio | 1,15 |
| ICAO standards compliance | App.16, Ch.2 |
Weights and Volumes | |
| max take-off weight (t) | 206 |
| max payload (t) | 42 |
| max fuel tanks capacity (liter) | 83676 |
Performance | |
| cruise speed (km/h) | 850-900 |
| range with max passenger capacity (km) | 3800 |
| flight altitude (m) | 10000-12000 |
| take-off run distance (m) | 2700 |
| landing run distance (m) | 1980 |
Seats | |
| flight crew | 3 |
| passengers | 350 |
Service Life | |
| calendar | 20 years |
| flights | 20000 |
| flight hours | 30000 |
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