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| YAK-50 |  |
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| Training aircraft | ||
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| Specification: | ||
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Year deployed
Wing span, m Length, m Height, m Wings area, m2 Weight, kg - empty aircraft - maximum take-off Internal fuel, l Engine Power, hp Maximum speed, km/h Cruising speed, km/h Range, km Endurance, h.min Service ceiling, m Maximum overload Crew |
- 1977 - 9.50 - 7.68 - 3.16 - 15.00 - 765 - 900 - 55 + 120 l in 2 tanks - 1 PE M-14P - 1 У 360 - 420 - 320 - 495 - 0.48 - 5500 - 9 - 1 |
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