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Start | LKL | LKL-2


General information


ManufacturerLKL
ModelLKL-2
ModificationLKL-2
CountryPoland
Years1930
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan11.50 m
Length7.00 m
Height2.54 m
Wing area18.54 m2
Zero fuel weight-
Empty weight438 kg
Maximum takeoff weight842 kg
Normal takeoff weight-
Flight duration-
Engine1 Walter Vega
Power1 x 85 HP
Thrust-
Maximum speed150 km/h
Cruising speed130 km/h
Rate of climb-
Practical range600 km
Service ceiling4300 m
Hovering ceiling-
Crew3
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