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Ilyushin Il-114
First flight year — 1990
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Ilyushin Il-114 Specifications
| Il-114 | Il-114-100 | |
| Dimensions | ||
| Length (m) | 26.9 | 26.9 |
| Wingspan (m) | 30.0 | 30.0 |
| Height (m) | 9.2 | 9.2 |
| Wing area (m2) | 81.9 | 81.9 |
| Weight | ||
| Maximum take-off weight (kg) | 22 700 | 23 500 |
| Maximum landing weight (kg) | 22 700 | 23 500 |
| Operating empty weight (kg) | 15 000 | 15 900 |
| Maximum zero fuel weight (kg) | 21 500 | |
| Maximum payload (kg) | 6 500 | 6 500 |
| Standard fuel capacity (litres) | 8 360 | 8 360 |
| Performance | ||
| Range with max payload (km) | 1 000 | 1 500 |
| Maximum operating altitude (km) | 8 000 | 8 000 |
| Take-off field length (m) | 1 360 | 1 400 |
| Landing field length (m) | 1 260 | 900 |
| Engines | Klimov TV7-117, 2 x 2465 hp | P&WC PW127H, 2 x 2750 hp |
| Fuel efficiency (g/pass*km) | 20.8 | |
| Fuel flow rate (kg/h) | 590 | |
| Cabin Data | ||
| Passengers (1-class) | 64 | 64 |
| Cabin width (m) | 2.28 | 2.28 |
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