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| U-1 |  |
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| Training aircraft | ||
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Specification: | |
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Year deployed
Wing span, m Lenght, m Height, m Wings area, m2 Weight, kg - empty aircraft - normal take-off Engine Power, hp Maximum speed, km/h Cruising speed, km/h Range, km Rate of climb, m/min Service ceiling, m Crew |
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1921 - 10.85 - 8.78 - 3.21 - 30.00 - 600 - 840 - 1 PE M-2 - 1 У 120 - 137 - 109 - 185 - - 4500 - 2 |
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