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IDET
22.-24.5. 2013

International Exhibition of Defence and Security Technologies

Aircraft Industries, a.s.

 

L410 UVP-E20 excellent plane for short haul transport

  • 19 seat commuter for transportation of passengers, cargo or for special missions
  • Lowest operating and maintenance costs in its category
  • Unsurpassed durability and proven reliability in extreme conditions
  • Reliable operation on short unpaved runways (STOL)
  • Superb “hot and high” performance
  • High versatility with a number of quick change conversion kits
  • An excellent safety record
  • Large luggage compartments
  • A very roomy and comfortable passenger cabin (most spacious in its category)

All-metal, high-wing, twin turboprop commuter aircraft, powered by two engines H80-200 is successfully operating in both Sahara desert as well as Siberian tundra. The L 410 UVP-E20 received full EASA Type Certificate valid for all EU (EASA) countries. Aircraft has been certified on the basis of FAR 23 regulation (Amendment 34), but it is known as well as L420 which is variant of the L 410 UVP-E20 certified on the basis of FAR 23 regulation (Amendment 41).

Until today more than 1100 aircraft have been produced. 19 seat turboprop commuter aircraft has been in production for over forty years and it holds an impressive safety record. Users from various regions appreciate its remarkable "hot and high” performance and excellent STOL capability even on unpaved runways. They especially value its tough and durable structure and its ability to operate under extreme climatic conditions, ranging from –50°C up to +50°C. Durable airframe and unique design offer exceptional performance both in the torrid desert heat of Africa and Latin America as well as the most frigid regions of the world.



The wide-body, oval fuselage, with 17.9 cu m. (632 cu ft) of passenger cabin volume, provides the highest standard of passenger comfort in the standard commuter variant as well as maximum versatility and utilization of the aircraft for a number of other applications and special missions, including executive, cargo, fast medical aid, ambulance, paratroops, photogrammetric, maritime patrol, surveillance and others. The L 410 represents ideal technical and economic solutions for short haul air transport of passengers and loads, which is easy to handle and simple to maintain.



Basic technical data

Wing span 19,98m
Length 14,42m
Height 5,969m
Max. take-off weight 6600kg
Max. landing weight 6400kg
Max. payload 1800kg
Max. fuel weight (with wing tip tanks) 1300kg
Max. cruising speed 398km/h TAS
Max. range (EFC, 14.000ft, ISA, 45min. holding) 1520km

 

Crew: 2 pilots

Autopilot, HF Transceiver,  TCAS II,  installed on request.

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