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Start | Let | L-410 Turbolet


General information


ManufacturerLet
ModelL-410 Turbolet
ModificationL-410
CountryCzechoslovakia
Years1969
TypeTransport aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan19.48 m
Length14.424 m
Height5.83 m
Wing area35.18 m2
Zero fuel weight-
Empty weight3800 kg
Maximum takeoff weight5800 kg
Normal takeoff weight-
Flight duration-
Engine2 Motorlet (Walter) M 601Е
Power-
Thrust2 x 560 kN
Maximum speed457 km/h
Cruising speed380 km/h
Rate of climb-
Practical range1380 km
Service ceiling6320 m
Hovering ceiling-
Crew2
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