L 410


General description

The L 410 is an all-metal, high-wing turboprop aircraft that is exceptionally reliable and safe to operate even in extreme climatic conditions. It is used in more than 60 countries across five continents, with the majority operating in Russia, followed by Africa, Southeast Asia, South America and Europe. Since 1969, more than 1,200 L 410 aircraft have been manufactured.

The L 410 is operated as a civilian aviation aircraft by commercial airlines, government agencies, the military and aviation clubs around world. It is a multi-purpose aircraft, produced in many variants. The L 410 constitutes an ideal combination of high performance and economical operation for the transport of civilians and cargo for short and medium range routes.


  • 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 UVP-E20


    endurance
    speed
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    uvp

    The L 410 UVP-E20 variant entered production at the end of the 1980s. Since then, more than 200 have been made and are now used in more than 30 countries. This variant remains the longest produced of the L 410. Even today, it fully meets the customers’ requirements and is supplied to operators around the world.

    The aircraft is certified in the category of transport aircraft in accordance with regulations of EASA (CS-23), FAA (Part 23), FATA (AP-23), EA-9401 (Brazil), AV-9703 (Argentina), A-B46-04/16 (Chile), 727-2006-MTC/12.04 (Peru), PRE-GGSA-GCO-2934-2015 (Venezuela), 1-99 (Cuba), 5-22/2011-AED (Indiа), 136/2013 (Nepal), 5VT9800015 (The Philippines), A048 (Indonesia), EASA.A.026 (South Africa), 1680 DACM/SDTA/AIR/08 (Algeria), CAA - VTC - 125 (Taiwan), TC EASA.A.026 (Turkey).


    cockpit
    interior
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    SPECIFICATION


    Performance


    Cruise Speed 405 km/h 219 KTAS
    Maximum Range* 1 500 km 810 NM
    Endurance* 5,1 h 306 min
    Service Ceiling 4 200 m 14 000 ft
    One Engine Inoperative Ceiling 4 755 m 15 600 ft
    Absolute Ceiling 8 382 m 27 500 ft

    * 45 minutes reserve

    Rate Of Climb 8,5 m/s 1 673 fpm
    Rate Of Climb One Engine Inoperative 1,8 m/s 354 fpm
    Take-off Distance Required 510 m 1 673 ft
    Landing Distance Required 500 m 1 604 ft

    Dimension and weights


    L410
    L410
    L410
    L410

    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 1,47 m3 51,9 ft3
    Maximum Take-off Weight 6 600 kg 14 550 lb
    Maximum Landing Weight 6 400 kg 14 109 lb
    Maximum Zero Fuel Weight 6 000 kg 13 228 lb
    Maximum Payload 1 800 kg 3 968 lb
    Maximum Usable Fuel 1 300 kg 2 866 lb

    Powerplant



    Propeller


    Model GE H80-200
    Manufacturer GE Aviation Czech s.r.o
    Take-off Power 597 kW 800 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