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Antonov An-26
First flight year — 1969
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Antonov An-26 Specifications
| An-26-100 | |
| Dimensions | |
| Length (m) | 23.8 |
| Wingspan (m) | 29.2 |
| Height (m) | 8.58 |
| Wing area (m2) | 74.98 |
| Weight | |
| Maximum take-off weight (kg) | 24 000 |
| Operating empty weight (kg) | 15 020 |
| Maximum payload (kg) | 6 500 |
| Performance | |
| Maximum range (km) | 2 550 |
| Maximum cruise speed (km/h) | 440 |
| Maximum operating altitude (km) | 7 500 |
| Engines | AI-24VT, 2 x 2820 shp |
| Fuel flow rate (kg/h) | 1 000 |
| Cabin Data | |
| Passengers (1-class) | 35-43 |
| Cabin length (m) | 11.10 |
| Cabin width (m) | 2.78 |
| Cabin height (m) | 1.91 |
Typical Cabin Configuration of Antonov An-26
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