Background
The development of the L-410 started in Czechoslovakia in the 1960s. The first prototype, called L-410 Turbolet, flew on April 16, 1969. New versions followed, including the L-410UVP, which had an improved performance in take-off and landing, and the L-410UVP-E, the most common variant of the plane, which had an increased maximum take-off weight. The first flight of the L-410UVP-E took place in 1984. The production of this variant started two years later. The seating capacity for the different versions ranged from 15 to 19 passengers.