Let L-410 Private Charter Flights and Prices

Development of the L-410 was started in the 1960s by the Czechoslovak aircraft manufacturer Let Kunovice. The first prototype flew on April 16, 1969. Due to delays, the prototype and first production version were powered by Pratt & Whitney Canada PT6A-27 engines. The L-410UVP-E (the most common variant of the L-410) has a take-off weight to 6400 kg, M601E engines with increased power, new five-blade propellers designated V 510 and wing tip tanks to increase fuel quantity.

Aircraft Size

Cabin Size

Performance Specifications

Performance	English	Metric
IFR Range	1,134 nm	2,100 km
Cruise Speed	216 KTAS	400 km/h
Certified Ceiling	20,721 ft	6,316 m
Rate of Climb	1,416 ft/m	432 m/m
Takeoff Distance	2,246 ft	685 m
Landing Distance	1,574 ft	480 m
Max Takeoff Weight	14,112 lbs	6,401 kg
Max Landing Weight	13,671 lbs	6,201 kg
Useful Weight	5,325 lbs	2,415 kg
Payload with Full Fuel	3,968 lbs	1,800 kg

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