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 modifications. 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

The L 410 UVP-E20 model 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 model 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 for: EU (EASA), USA (FAA), Russian Federation (FATA), Brazil, Argentina, Chile, Peru, Venezuela, Cuba, Indiа, Nepal, The Philippines, Indonesia, South Africa, Algeria, Taiwan, Turkey.

Cockpit Airplane Aircraft Industries LET L 410 UVP

Interior Airplane Aircraft Industries LET L 410 UVP

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	1 640 ft

Dimensions and weights

Cabin Volume	17,9 m³	632 ft³
Passenger Door	0,8 x 1,46 m	31,5 x 57,5 in
Cargo Door	1,25 x 1,46 m	49,2 x 57,5 in
Seat Pitch	0,76 m	30 in
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