Aircraft l 410 scheme the best places. How it's done, how it works, how it works

The first L-410 aircraft was created in the 60s of the last century by Czechoslovak manufacturers by order of the USSR. It was the Soviet Union that was the main customer for this type of air transport, however, companies from other countries were also interested in this model:

Poland and Lithuania;
Bulgaria and Hungary;
Brazil.

After all, the advantages of the aircraft could be assessed even with the naked eye:

Lightness and maneuverability.
Ability to land on normal ground.
Sufficient carrying capacity and comfort.

These are the characteristics of the new liner. Photos of the cabin of the L-410 aircraft can be viewed on our Internet resource.

Aircraft L-410

The first model of the L-410 aircraft, as noted earlier, was created in the late 60s. The main purpose of the new air transport is to carry out short flights. The capacity of the cabin was to be such that it could accommodate up to 20 people, and the aircraft was to be served by airlines up to 650 km long.

The Czechoslovak manufacturer successfully coped with the task assigned to him, new model The transport aircraft turned out to be not only reliable and unpretentious, but also multi-purpose, which, in fact, was required by the customer.

Having at its disposal a new type of air transport, the liner began to be used for:

passenger and freight traffic;
for the transportation of correspondence;
for the transport of patients;
for various scientific research.

The new model of air transport was valued not only for maneuverability, but also for the ability to take off and land in places where there was no runway, which was extremely important when transporting patients or when conducting scientific research.

The first model, called the L-410, took to the skies in the late 60s, however, as the manufacturers noted, the air transport engine was underpowered. Therefore, it was decided to make several changes to the production process, in particular, they affected the engine. So, by the mid-70s, modernized L-410s with a more powerful engine were put into production, 5 of which were transferred to the Soviet Union.

The main customer was satisfied with his order and continued cooperation with the manufacturer, and the first air transport was bought by Aeroflot, the most famous company in those days. You can see photos of the aircraft Let L-410 on the website. By the beginning of the 80s, the Soviet Union had acquired more than 100 models of L-410 aircraft, and was not going to stop cooperation.

The cabin of the aircraft L-410

A variety of aircraft models L-410

The Czechoslovak manufacturer did not stop at his achievements, constantly creating more and more advanced models of liners. The production of the following models was launched:

L 410 UVP;
L 410A;
L 410 AS;
L 410 M.

The L 410 UVP model was also developed at the request of the Soviet customer, the aircraft differed from its counterparts in the increased wing length and fuselage, as well as in the plumage, made in a vertical design. Such modernization allowed the liner to take off and land at an even shorter distance, which was the main requirement of the customer.

The demand for air transport from the Czechoslovak manufacturer, of course, subsided after the collapse of the USSR, but the Ural Mining and Metallurgical Company helped to save the situation, which 8 years ago bought more than 50% of the shares from the first manufacturer. Currently, the partners are planning to increase the production of aircraft, improve the production process, and purchase new modern equipment.

Air transport characteristics

Technical characteristics of the aircraft L-410:

up to 14.42 m - the length of air transport;
up to 20 m - the wingspan of the aircraft;
35 m 2 - occupies the wing area;
5.83 m - aircraft height;
4 tons - weight of empty transport;
up to 6.6 tons - the maximum weight allowed during takeoff;
750 HP on 2 - engine power;
335 km / h - maximum speed;
up to 1500 km - is the range of air transport.

The capacity of the fuel tanks is designed for 1680 liters, the maximum fuel supply is 1300 kg. If the aircraft is fully loaded, it will be able to cover a distance of 1000 km, and for the maximum run it will need only 850 meters.

There are two places for the crew, passenger seats there are 19 pieces in the cabin, the width is 1.9 meters. A photo of the L-410 aircraft will help to get acquainted with the aircraft cabin in more detail. vehicle.

Aircraft L-410 in the sky

What else do you need to know?

Summing up, we can say that the L-410 liner is a reliable, unpretentious and maneuverable type of air vehicle, which has a reduced distance for both takeoff and landing. It is convenient to operate transport in such conditions where it is difficult to take off and land transport. Thanks to a sufficient margin of safety, which was invested by the manufacturers, the aircraft can easily land and take off from unprepared and even from unpaved areas. The spacious cabin, equipped with large windows, has good sound insulation, the passenger seats are located in the position 1+2.

This model is able to overcome about 1300 km, while carrying 19 passengers., and high-quality chassis, made according to a special method, allow the aircraft to land even on wet grassy ground. The liner showed itself well when operating in harsh climatic conditions, the excellent traction characteristics of the engine make it possible to use the aircraft both at high temperatures and at very low atmospheric pressure.

Excellent security parameters allow you to safely transport passengers, deliver cargo in integrity and without damage. Throughout the history of its existence, the liner has been constantly upgraded by the manufacturer, and the production of aircraft continues at the present time.

By joint efforts, manufacturers plan to create more advanced models in the coming years, the engines of which have increased power, area luggage compartment will increase, the cockpit will be equipped with the latest equipment, including avionics.

In contact with

How L-410 aircraft are made in the Czech Republic gelio wrote in December 4th, 2013

L-410 UVP-E20 - universal twin-engine aircraft of Czech production for local overhead lines accommodating 19 passengers. Designed for operation on unprepared unpaved, grassy, snowy areas, as well as on airfields with short runways (about 600-700 meters), which, in fact, makes it an aircraft in the off-road category. The first flight of the L-410 was made on April 16, 1969. The main customer of the aircraft was the Soviet Union. In addition, the L-410 was also supplied to Bulgaria, Brazil, Hungary, East Germany, Libya, and Poland. Despite the fact that the plant is located in the Czech Republic, it considers itself a part of the Russian aviation industry: the grounds for this were laid during its development and during its long history of operation. As of 2012, more than 400 L-410s are in operation worldwide.

Production site of Aircraft Industries in Kunovice, Czech Republic.
The Aircraft Industries plant, better known under the Let Kunovice brand, is located 300 km from Prague. The plant employs 920 people.
The enterprise manufactures the aircraft according to the full production cycle - it has its own lines for surface treatment of materials, paint and varnish production, a machine shop, assembly shops, a design bureau and an airport.

Workshop for the production of parts of the fuselage L-410. The enterprise is expanding and modernizing production - light green equipment is intended for the production of a new generation of aircraft L-410 NG (New Generation).
The production capacity of the plant is 16-18 new aircraft per year.
About 80% of aircraft are delivered to Russia. Over the past four years, 35 aircraft have been delivered to Russia.

Production of parts on a CNC milling center from the French company Creneau.

Cleaning parts before molding

Press molding

Punching press

Design documentation - drawing of the spoiler

Wing spar fabrication on a 5-axis CNC milling machine.
In the production, Russian duralumin produced by Kamensk-Uralsky Metallurgical Plant OJSC is used. The total share of components from Russia in the L-410 aircraft is about 15% - this is a legacy of the fact that the aircraft was developed by order of the USSR and with the participation of Soviet designers.

Wing panel production

Front wing assembly

Checking the quality of riveting on an aircraft wing

About 185,000 rivets of various types and sizes are used for one L-410 aircraft

Riveting work in the middle part of the fuselage

Installation of floor panels

Rear fuselage production

Manufacture of engine air intake part

Production of an air intake part for the CASA CN-235 aircraft within the framework of industrial cooperation.
The plant also cooperates with Boeing for the Boeing 787 aircraft.

Assembly conveyor of aircraft L-410 UVP-E20. It is located in one of the newest buildings of the plant, originally designed for the production of L-610.
In one half of the building there are two lines for the production of new L-410 aircraft, in the second half there is a workshop for servicing aircraft coming out of service.

At the same time, about 10 aircraft are in the assembly shop. The fuselage, wing, end tanks and tail unit come to the beginning of the line from the paint shop.
At the end of the line are aircraft undergoing flight tests and preparing to be shipped to customers.
Over the entire history of its existence, the plant has produced over 1150 aircraft of the L-410 family.
More than 850 of them were delivered to operators in the USSR.

The process of finishing the luggage compartment of the aircraft in the nose after the completion of the installation of electrical equipment

Assembling the emergency exit door

The nose of the aircraft with serial number 2915. The weather radar antenna is visible.
The forward luggage compartment doors are open.

Installation of avionics in the cockpit. Avionics traditionally include devices from Russian manufacturers

Installation of electrical equipment in the aircraft cabin

Installation of wiring harnesses

Installation of electrical wires on the wing of the aircraft in the area of the engine nacelle

The AV-725 five-bladed propellers (Avia Propeller) together with the GE H80-200 engine make up a new power plant aircraft L-410 UVP-E20. It has been installed since January 2013 on all new aircraft and is certified by EASA and the Russian AR IAC.
Young people in production are not uncommon, also due to the presence of their own vocational technical school on the territory of the plant.
The average age of the company's employees is 44 years.

Work on the GE H-80 engine carried out by a representative of GE Aviation Czech, Prague (former Walter plant).

The final assembly stage takes about 5 months - this is the most expensive part of production, so within its framework, engines, landing gear and all avionics are installed on the aircraft, where each individual unit can cost 100-250 thousand Euros.
The total duration of the aircraft production cycle from the production of the first fuselage components to the completion of flight tests takes a little less than a year.

The cockpit of the aircraft L-410 UVP-E20.
The aircraft is fully equipped for instrument flight, has an advanced ground proximity warning system (GPWS) and airborne collision warning system (TCAS II). The L 410 is designed in the metric system (not in inches), which is an exception in Western aviation.

This type of aircraft has been used for many years as a graduation for pilot training at the Sasovo Flight School. civil aviation(Ryazan region).

Pre-flight preparation. Stanislav Sklenarzh is the plant's chief test pilot.

Under the wing of the aircraft view of the river. Moravu and the city of Uhersky Ostrog

Aircraft L-410 UVP-E20 for French Guiana.
Aircraft for exotic countries often have a bright, memorable coloring.

Leaving with a turn
Practical ceiling - 8000 meters

Runway entry.
The L-410 aircraft can land both on a hard-surfaced runway and on grass, soil and snow. UVP in the name of the aircraft means the Russian abbreviation "Short Takeoff and Landing", which also recalls the Russian roots of the aircraft.

Castle New Svetlov (1480), Bojkovice.

Medieval gothic castle Buchlov (XIII century) is located 10 km from Kunovice.
Buchlov Castle is one of the most beautiful castles in South Moravia, the southeastern region of the Czech Republic.

Velegrad Monastery (XIII century) is one of the main pilgrimage temples in Czech Republic.
In 863 - 866 years. the Christian saints Cyril and Methodius lived and preached in Velegrad.

The prototype of the aircraft L-610M in Staroe Mesto, installed for viewing at the entrance to the city.

The crew performed a charter flight at the request of the Polar Geological Survey (Kuyga settlement) along the route Batagai - Magan - Lensk - Kirensk - Irkutsk. There were two service passengers on board. There was no cargo, except for the personal belongings of the crew and passengers with a total weight of about 400 kg, on board.
After arriving at the Kirensk airport at 12:37 Moscow time, the crew's working time was 11 hours 45 minutes, including flight time - 6 hours 17 minutes. The crew, in violation of the flight crew's duration of work established by the instructions, decided to proceed to Irkutsk. Then, upon receiving information about the closure of the Irkutsk airport due to the repair of the runway, the crew postponed the flight and was sent by the air traffic controller to the dispensary. In the dispensary, the appearance of the crew was not recorded. After the opening of the Irkutsk airport, the navigational control of the crew, in the absence of the navigator on duty, was carried out by the air traffic controller, who was not trained for this control.
Having passed a meteorological consultation at 14:50, at 15:06, in violation of the working hours, the crew flew from Kirensk to Irkutsk.
When establishing communication with the Irkutsk airport approach controller, the crew did not report on the receipt of information from the air navigation service (ATIS), and the controller did not require the crew to listen to it and report it. The approach controller instructed to perform a descent from 3000 m to 2100 m. After the flight of the LBM, the aircraft was transferred to the control of the circle controller, who also did not require a report on the receipt of ATIS information, and the crew did not report on the receipt of this information and on the selected approach system. The lap controller instructed to descend to the transition level of 1,800 m. The descent took place in simple weather conditions at night.
At the transition level, in violation of the requirements of NPP GA-85, the crew did not set the pressure on the barometric altimeters to the airfield pressure (710 mm Hg) and did not report the airfield pressure setting to the controller. In turn, the lap controller, having not received a report, did not require the crew to confirm the pressure setting.
As a result, the altimeter readings, at which the standard pressure of 760 mm Hg remained, differed from the true altitude by 510 m. At the command of the circle controller, the crew continued to descend to 900 m (according to the altimeter readings, the true altitude was 390 m), performed the third turn , took 700 m (190 m true altitude) and continued flying to the fourth turn. After the report of the crew "235, on the fourth, 700 m", the controller instructed to switch to communication with the landing controller. The crew did not have time to confirm the command and end the connection. After 2 seconds, at 17:18:10, the aircraft touched the tops of trees 25-35 m high, located at an elevation of 163 m with a relative elevation above the airfield of 190 m (the threshold of the airfield runway above sea level is 510 m). The crew gave the engines takeoff, but after 114 m there was a head-on collision with a tree trunk 35 cm in diameter (at the impact site). The aircraft, descending along a rectilinear trajectory and continuing to collide with large trees (trunk diameters 85-90 cm in the butt, height up to 35 m), stopped 312 m from the place of the first collision with obstacles, collapsed and partially burned out. The accident occurred 21 km from the airport with an azimuth of 122° in the area of the fourth turn with MK=297° (52°09’30” N, 104°39’40” E).
At the time of the accident, the duration of the crew's work was 15 hours 26 minutes, including a flight time of 8 hours 30 minutes, which could affect the safe outcome of the flight due to crew overwork.
Actual weather for 17:27 - cloudiness 3 points cumulonimbus 1500 m, 10 points average, upper, wind 300 ° 9 m / s, visibility 10 km, lightning, tendency - hail, frontal thunderstorm, air temperature + 21 ° С, pressure 711 mm Hg.

The cause of the accident was a violation by the crew of the flight rules, expressed in the failure to comply with the requirements of clause 7.6.9 of NPP GA-85, in terms of setting the airfield pressure at the transition level at barometric altimeters, which led to a collision of the aircraft with the earth's surface.
The accident was accompanied by the controller's failure to comply with the operating technology, rules and phraseology of radio exchange in terms of not accepting a message from the crew about receiving ATIS information, not issuing a command to listen to it and reporting it, and not receiving from the crew about setting altimeters at the level of transition to airfield pressure.

The Russian Urals Mining and Metallurgical Company (UMMC) has decided to become the sole owner of the production of a small local airliner (IL) aircraft Let L-410, also known as the Turbolet. To this end, UMMC is going to increase its own stake in the block of shares of the Czech company Aircraft Industries from 51% to 100%, ITAR-TASS reports. The L-410 aircraft is considered by the Russian side as the main model for modernizing regional aviation fleets and restoring the network of local airlines. It is expected that the leasing of new aircraft will be supported by the budget. The specific mechanisms of this chapter support Russian regions going to decide at a meeting in September 2013.

Currently, the main product of the Czech airline is the L-410UVP aircraft. This model is a short-haul aircraft with a short takeoff and landing distance for 19 passengers. The first modification of the aircraft Let L-410 took to the skies in 1969. In the post-war years, the Czech "Turbolet" became the first foreign aircraft that entered the Soviet airlines. On the basis of this machine, a large number of different modifications of transport, military and special purposes were created. In particular, this aircraft is widely used in Russian military and civilian flight schools, where it serves to train future pilots of military transport and long-range aviation.

After the transfer of 51% of the shares of the Czech company to UMMC, the Czech aircraft manufacturer received additional orders for its main product - L-410 UVP-E20. In 2009, after a rather long break, deliveries of aircraft to Russian customers resumed - first to civilian companies, and later to the RF Ministry of Defense. As of 2012, the Russian Air Force was armed with 7 L-410 UVP-E20 aircraft, while the contracts and options concluded involve bringing the fleet of these aircraft to 15 aircraft.

Today, Aircraft Industries supplies the regions of Russia with an upgraded version of the aircraft, which is equipped with H-80 turboprop engines, which are manufactured by the General Electric division in the Czech Republic. According to the UMMC, the installation of these engines has significantly improved the performance of the aircraft, increasing, in particular, the flight range from 1420 to 1520 kilometers. Currently, the L-410 aircraft is listed in the parks of the Russian companies KrasAero and Orenburg. The Buryat airline PANH and the government are ready to purchase several aircraft Khabarovsk Territory. Earlier, the Ministry of Transport and the Ministry of Industry and Trade of Russia stated that 9- and 19-seat aircraft were needed for the development of the domestic air transportation market, but such modifications were not made in Russia.

Let L-410 "Turbolet" - Czechoslovakian, later Czech twin-engine universal aircraft, designed for operation on local airlines (IL). It is a twin-engine turboprop high-wing aircraft with a single tail. Also known under the names: Let, Let L-410, L-410, Turbolet, Elka, Cheburashka. As of 2012, more than 400 aircraft of this type were operated in the world.

The most common version of the aircraft was the L-410UVP modification; in this version, the aircraft had a reduced takeoff and landing distance. The abbreviation UVP means “short takeoff and landing”. The aircraft of this modification first took to the skies in 1976. Initially, the machine was equipped with the usual set of aviation equipment of the Soviet-Czechoslovak production. The model differed from its predecessors in the increased size of the wing and vertical tail, elongated fuselage, the use of spoilers and more efficient engines.

It is worth noting that the design and production of small aircraft and air taxis in the countries of the Council for Mutual Economic Assistance (CMEA) bloc was the prerogative of the aviation industry of Czechoslovakia. Czech-made aircraft flew not only in the countries of the socialist bloc, but also in Switzerland, Italy, Great Britain, the USA, Australia and other countries of the world. Aero-45, Super Aero-45S and Aero-145 four-seater air taxis, as well as the L-200 Morava, were in particular demand. Therefore, there is nothing surprising in the fact that when the question arose of choosing a small short-haul aircraft for mass production, the choice fell on the Czech L-410, which most fully corresponded to most of the parameters announced in the terms of reference of the State Research Institute of Civil Aviation.

The small passenger aircraft L-410 "Turbolet" was designed by the designers of the company "Let" in 1966-1967, the project was headed by Ladislav Smrchek. It was assumed that this aircraft could be used in a fairly wide temperature range from +50 to -40 degrees Celsius. Czech specialists were guided by the Soviet terms of reference and took into account the difficulties in advance climatic conditions operation of the aircraft in the USSR, which was to become the main customer of the aircraft.

In total, by the end of 1978, 100 L-410M / MU aircraft were purchased in the USSR for the Ministry of Civil Aviation. In the Soviet Union, "Turbolets" replaced the famous "corn" Antonov, who transported unpretentious Soviet passengers on air pockets local airlines. At the same time, it is worth noting that the pilots who were “transferred” from the An-2 to the L-410 perceived the newcomer in two ways. On the one hand, the Czech aircraft had a lot of advantages. Firstly, he had 2 engines, he won 2 times in safety. The plane had a set of modern navigation and radio equipment, a high level of comfort was provided for passengers ... But, on the other hand, for civilian pilots air fleet An-2 always remained a free "gasoline breadwinner" of their personal Zhiguli and Volga, while the Czech plane flew on kerosene. And in operation, the An-2 was a more unpretentious machine. To be more precise, the flight technical personnel treated the issues of operating the Soviet An-2 much easier. In general, it was considered very prestigious to transfer from the An-2 to the Czech L-410.

In total, since 1969, 1104 L-410 of various models were produced in Czechoslovakia and the Czech Republic, of which 862 aircraft ended up in the USSR. Interestingly, the 1000th Turbolet was produced back in 1990 and transferred to Aeroflot, after which their production volumes were significantly reduced. With the collapse of the CMEA, and subsequently the Soviet Union, the demand for these aircraft dropped sharply. Despite this, Turbosts are still in operation in more than 45 states around the world.

Currently, the Czech Republic is producing a version of the L-410 UVP-E20 aircraft, which can be equipped with analog or digital avionics (at the customer's choice), the TCAS mid-air collision avoidance system and an autopilot. The L-410 UVP-E20 aircraft received the AR IAC certificate.

Flight performance L-410 UPV-E20:

Dimensions: wingspan - 19.48 m, length - 14.49 m, height - 5.83 m.
Wing area - 34.86 square meters. m.
The maximum takeoff weight of the aircraft is 6,600 kg, the empty weight is 4,050 kg.
Engine type - 2 HPT GE H80-200, power - 2x800 hp

The maximum speed is 395 km / h.
The practical flight range is 1500 km.
Practical ceiling - 8,000 m.
Crew - 2 people.
Commercial load - 19 passengers or 1800 kg. cargo.

Sources of information:
-http://www.newsru.com/finance/25jul2013/rul410plane.html
-http://www.airwar.ru/enc/craft/l410.html
-http://ru.wikipedia.org/wiki/Let_L-410_Turbolet

TASS-DOSIER. On November 15, 2017, a passenger plane Let L-410UVP-E20 Turbolet of Khabarovsk Airlines, flying along the route Khabarovsk - Nikolaevsk-on-Amur - the village of Nelkan (Ayano-Maisky district of the Khabarovsk Territory), made a hard landing 2 km from the destination. Six people were killed, including two crew members. One child saved.

The TASS-DOSIER editors compiled a chronology of L-410 aircraft crashes in Russia. In total, from the end of 1991 to present. in. five crashes occurred on the territory of the Russian Federation aircraft of this type (excluding the state of emergency on November 15, 2017). They killed a total of 41 people.

April 4, 1992 An L-410UVP aircraft (registration number RA-67130) of the Kamchatavia airline, flying from Petropavlovsk-Kamchatsky to Baikovo (Sakhalin Region), crashed near the destination airport. There were 12 people on board - two pilots and 10 passengers. The crew violated the approach pattern, the plane collided with the ground 5 km from the runway. The torn propeller cut the fuselage behind the cockpit, killing one of the passengers, two more people were injured. The power elements of the aircraft were significantly damaged.

August 26, 1993 in Yakutia, an L-410UVP-E aircraft (registration number RA-67656) of the Sakha-Avia airline, en route Kutana - Chagda - Aldan, crashed while landing at the last point of the route. There were 24 people on board - two pilots and 22 passengers, all of them died. The commission investigating the crash found that the aircraft was heavily overloaded. Its landing weight exceeded the maximum allowable by 550 kg, this changed the balance of the aircraft when the crew began to extend the flaps, causing the aircraft to stall and collide with the ground. Pilots were found guilty of the emergency, who decided to fly despite significant excess of takeoff and landing masses, as well as with an overestimated rear centering of the aircraft.

January 20, 1995 aircraft L-410UVP (registration number RA-67120) of the Abakan airline, flying flight 107 on the route Krasnoyarsk - Abakan, crashed during takeoff at the Krasnoyarsk airport Yelizovo. The aircraft was unable to gain altitude, collided with trees and crashed 930 m from the runway. There were 19 people on board - two pilots and 17 passengers. Both crew members and one passenger were killed, 13 people were injured. The cause of the accident was the congestion of the aircraft, the failure of the right engine and the erroneous actions of the crew during takeoff with one engine running. Exceeding the maximum allowable takeoff weight of the aircraft by 278 kg was due to the fact that the staff of the Yemelyanovo airport and the crew placed four passengers with luggage in the cabin, who did not have tickets for the flight.

March 1, 2003 a private aircraft L-410UVP (registration numbers RA-67418, FLA RF-01032), which was carrying out airborne landing flights for skydivers, crashed near the Borki sports airfield in the Kimrsky district of the Tver region. There were two crew members and 23 paratroopers on board (despite the fact that the maximum allowable number of paratroopers in this version of the cabin layout is 12). Permissible takeoff weight was exceeded by 618 kg. When, during the flight, the paratroopers headed for the exit in the tail section of the aircraft, the centering was disturbed, the machine went into stall mode and, due to off-design overloads, fell apart in the air. 11 people were killed - both crew members and nine athletes. 14 people were able to leave the plane and land on their own with parachutes, while four received fractures.

July 22, 2012 aircraft L-410UVP (registration number RF-00138) of the DOSAAF of Russia crashed at the Bolshoye Gryzlovo sports airfield (Serpukhov district, Moscow region). The aircraft was landing on an unpaved runway after landing a group of paratroopers. The front and left landing gear of the aircraft broke, resulting in significant damage to the cockpit and the lower part of the fuselage. Only two crew members were on board, both were hospitalized in serious condition. The aircraft commander died from his injuries on July 24, 2012, the co-pilot died in the hospital a month and a half later, on September 6, 2012.

Let L-410

Let L-410 Turbolet is a multipurpose twin-engine turboprop aircraft of local airlines. Developed in the 1960s. in the design office of the Let Kunovice plant (Kunovice, Czechoslovakia, now the Czech Republic). The first flight was made on April 16, 1969, now produced by the Czech company Aircraft Industries (the owner is the Russian Ural Mining and Metallurgical Company), in total more than 1.1 thousand copies of various modifications were built, of which 862 were delivered to the USSR. The most modern modification, L-410UVP-E20, is capable of carrying up to 19 passengers or 1,800 kg of cargo over a distance of up to 1,500 km. In 2016, Aircraft Industries sold nine copies of the L-410 in Russia, and another 11 units were scheduled for delivery in 2017. A variant of launching serial production of the aircraft at the Ural Civil Aviation Plant (Yekaterinburg) is being worked out.

In total, at least 117 such machines were lost during the operation, more than 420 people died in 106 accidents.

"Khabarovsk Airlines"

Khabarovsk Airlines is a regional state unitary enterprise engaged in transportation in the Khabarovsk Territory. Operates aircraft: An-24 (2 machines), one Yak-40 and An-26 each, as well as four L-410UVP-E20 2013-2015. release (registration numbers - RA-67035, RA-67036, RA-67040, RA-67047). For the airline, the November 15 disaster was the first in its history.