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Letov S-139


General information


ManufacturerLetov
ModelS-139
ModificationS-139
CountryCzechoslovakia
Years1933
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.00 m
Length6.14 m
Height-
Wing area14.00 m2
Zero fuel weight-
Empty weight315 kg
Maximum takeoff weight515 kg
Normal takeoff weight-
Flight duration-
Engine1 Pobjoy R
Power1 x 85 HP
Thrust-
Maximum speed174 km/h
Cruising speed154 km/h
Rate of climb-
Practical range480 km
Service ceiling4700 m
Hovering ceiling-
Crew2