L 410


General description

The 410 NG is the latest variant of the L 410 aircraft. Its development was launched in 2010 under the MOSTA project, serial production began in 2018. This innovative model offers an improved flight envelope, use of advanced technologies and modernized avionics.

The new design of the wing with an integrated fuel tank provides increased fuel capacity, allowing for considerably longer flight range and endurance. Another crucial improvement is the increase of MTOW and payload, resulting in the ability to carry an extra 500 kg of cargo, with increased volume provided by the nose extension. The aircraft is equipped with the more powerful GE H85-200 engine and AV 725 propeller.


  • Designed for short take-off and landing (STOL)
  • Low operating and maintenance costs
  • Excellent performance in hot temperatures and high altitude conditions
  • Operates in extreme weather conditions (-50 °C to +50 °C)
  • Varieties of equipment, options to have special interchangeable configurations
  • Large cargo hold
  • Safe operation
  • The most spacious passenger cabin in its category
  • L 410 NG


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    Thanks to the implementation of these crucial changes, the customer will receive an aircraft with improved performance, including a higher cruising speed and better performance of the engines in hot temperatures and high altitude conditions. By following the damage tolerance philosophy in the design, we have also considerably increased the lifespan of the aircraft. The cockpit is equipped with a Garmin 3000 touchscreen glass integrated avionics system.

    The aircraft has been certified in the transport aircraft category in accordance with regulations of EASA.A.26 (EU), FAA, A42CE (USA), FATA (Russia).


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    SPECIFICATION


    Performance


    Cruise Speed 417 km/h 225 KTAS
    Maximum Range* 2 570 km 1 387 NM
    Endurance* 10,5 h 630 min
    Service Ceiling 6 100 m 20 000 ft
    One Engine Inoperative Ceiling 3 900 m 12 800 ft
    Absolute Ceiling 8 230 m 27 000 ft

    * 45 minutes reserve with auxilary fuel tank

    Rate Of Climb 8,5 m/s 1 673 fpm
    Rate Of Climb One Engine Inoperative 1,7 m/s 335 fpm
    Take-off Distance Required 590 m 1 936 ft
    Landing Distance Required 600 m 1 969 ft

    Dimension and weights


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    L410
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    Cabin Volume 17,9 m3 632 ft3
    Passenger Door 0,8 x 1,46 m 2,6 x 4,8 ft
    Cargo Door 1,25 x 1,46 m 4,1 x 4,8 ft
    Seat Pitch 0,76 m 2,493 ft
    Baggage Compartment Capacity 2,98 m3 105,5 ft3
    Maximum Take-off Weight 7 000 kg 15 432 lb
    Maximum Landing Weight 6 800 kg 14 991 lb
    Maximum Zero Fuel Weight 6 600 kg 14 660 lb
    Maximum Payload 2 300 kg 5 060 lb
    Maximum Usable Fuel 2 254 kg 4 969 lb

    Powerplant



    Propeller


    Model GE H85-200
    Manufacturer GE Aviation Czech s.r.o
    Take-off Power 634 kW 850 SHP
    TBO 3 600 FH 6 600 FC
    Dry Weight 201 kg 447 lb
    Model AV-725
    Manufacturer Avia Propeller s.r.o., Czech Republic
    RPM 1 950 RPM
    TBO 3 600 FH 6 600 FC
    Weight 88 kg 207 lb

    AIRCRAFT MODIFICATION







    CONTACT
    +420 572 816 111

    sales@let.cz