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Ilyushin Il-114
Aircraft type: Commercial airplane
Manufacturer: Ilyushin
Maiden flight year: 1990
Copyright Alexandr Zhukov
Ilyushin Il-114 Specifications
| Il-114-100 | Il-114-300 | |
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) | 23 500 | 23 500 |
| Maximum landing weight (kg) | 23 500 | 23 500 |
| Operating empty weight (kg) | 15 900 | 15 900 |
| Maximum payload (kg) | 6 500 | 6 500 |
| Standard fuel capacity (litres) | 8 360 | 8 780 |
Performance | ||
| Maximum range (km) | 5 100 | |
| Range with max payload (km) | 1 500 | 2 000 |
| Cruise speed (km/h) | 500 | 500 |
| Maximum operating altitude (m) | 8 000 | 7 600 |
| Take-off field length (m) | 1 400 | 730 |
| Landing field length (m) | 900 | 440 |
| Engines | P&WC PW127H, 2 x 2750 hp | Klimov TV7-117ST, 2 x 2900 hp |
| Fuel efficiency (g/pass*km) | 20.8 | |
| Fuel flow rate (kg/h) | 590 | |
Cabin Data | ||
| Passengers (1-class) | 64 | 60 |
| Cabin width (m) | 2.28 | 2.28 |
Ilyushin Il-114 Airplane
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Rating 3.84
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