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Start | LKL | LKL-4


General information


ManufacturerLKL
ModelLKL-4
ModificationLKL-4
CountryPoland
Years193
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan11.60 m
Length7.12 m
Height2.30 m
Wing area18.00 m2
Zero fuel weight-
Empty weight462 kg
Maximum takeoff weight740 kg
Normal takeoff weight-
Flight duration-
Engine1 Cirrus III
Power1 x 85 HP
Thrust-
Maximum speed155 km/h
Cruising speed130 km/h
Rate of climb-
Practical range800 km
Service ceiling3000 m
Hovering ceiling-
Crew2
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