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Ka-26

The Ka-26 ( NATO codification : Hoodlum - “Hooligan” ) is a Soviet multi-purpose helicopter developed at the Kamov Design Bureau . Serial production was carried out at the aircraft factory in Ulan-Ude and the aircraft factory in Kumertau . In total, 816 helicopters were built, including 257 delivered to 14 countries.

Ka-26
Helicopter Kamov Ka-26 cockpit.jpg
Ka-26
Type ofmultirole helicopter
ManufacturerUnion of Soviet Socialist Republics OKB "Kamov"
Chief Designer
The first flightAugust 18, 1965
Start of operation1969 year
Statusoperated by
Operators, and
Years of production1969 - 1985
Units produced816
OptionsKa-126

The helicopter was mainly used for civilian purposes, however, it was also used in the air forces of Romania and Hungary , the police of the GDR and the Federal Republic of Germany .

Further constructive development is the Ka-126 helicopter with one gas turbine engine and the Ka-226 helicopter with two gas turbine engines.

Content

  • 1 History of creation
  • 2 Design
    • 2.1 Engine
    • 2.2 Main rotors
    • 2.3 fuselage
    • 2.4 Cab
    • 2.5 fuel system
  • 3 Manufacturing Options
  • 4 Flight performance
  • 5 records
  • 6 Operation
  • 7 Operators
  • 8 Disasters & Accidents
  • 9 Gallery
  • 10 Ka-26 in the movies
  • 11 Notes
  • 12 Links

Creation History

  • The beginning of the 1960s - the N. I. Kamov Design Bureau was tasked with creating an agricultural helicopter capable of using various sets of equipment. Design and manufacturing work was headed by Deputy Chief Designer - M. A. Kupfer.
  • 1965 - the first prototype of a helicopter was made.
  • May 24, 1965 - test pilot V.I. Gromov completed the first hang.
  • August 18, 1965 - the first flight in a circle.
  • 1966 - the beginning of state trials.
  • At the international exhibition of agricultural machinery and equipment, Ka-26 was awarded a gold medal.
  • 1967 - demonstration at the air show in Le Bourget . The Ka-26 successfully passed tests and was certified according to the American airworthiness standards FAR-29 (the first of the domestic helicopters).
  • 1969 - mass production was organized.

Design

Helicopter coaxial twin-screw circuit with two piston engines and four-wheeled landing gear.

It was built according to the “flying landing gear” scheme: various types of suspension could be installed behind the cockpit (depending on the desired task): passenger / cargo cabin, tanks and sprayers for aviation chemical work, a hoisting winch, etc. (3-person crew in 1.5―2 hours it is able to convert a helicopter from one option to another).

Engine

The helicopter is equipped with two piston 9-cylinder star-shaped engines with air cooling M-14V26 Vedeneeva , located in the engine nacelles on the sides of the fuselage. The engines and the main gearbox were developed by the Voronezh Experimental Design Bureau of Motor Engineering .

Main rotors

Three-bladed, coaxial, opposite rotation, with hinged blades mounted from each other at a distance of 1.17 m. The blades are made - for the first time in the practice of world helicopter engineering - made of fiberglass based on fiberglass and epoxy-phenolic binder (were developed specifically for Ka-26 have an almost unlimited resource). The spar is hollow, of variable cross-section, light tail sections are glued to it and a steel node for attaching the blades is bolted. The toe of the blade is protected by a light-resistant rubber coating, a counterweight is located inside the toe. Inside the counterweight there are tubes of the anti-icing system, through which liquid from the tank, which was located in the compartment at the rear of the central fuselage section between the root parts of the tail beams, was supplied to the socks of the blades.

Fuselage

It is presented in the form of a “flying chassis” with a rectangular rectangular platform-platform compartment, to which the crew cabin is attached in front and two tail beams supporting the horizontal tail. A main gearbox with a supporting system is installed on top of the central compartment, and two gondolas with M-14V26 engines on the sides.

Cabin

The crew cabin is double, with good visibility and sliding doors, has a large glazing area, in the agricultural version it is equipped with an air purification system with a centrifugal separator-supercharger that creates excess pressure in the cabin and a filter with an absorber. The windshields are equipped with wipers and an anti-icing system. The installation of a second control kit is envisaged in the cab. Behind the crew seats are compartments of electronic and instrumentation equipment with large hatches for maintenance.

Fuel System

It has 3 fuel tanks (2 front, 1 rear) with a total capacity of 620 liters, it is also possible to install two tanks with a capacity of 160 liters on the sides of the cargo-passenger compartment.

Manufacturing Options

The Ka-26 helicopter was produced in the following versions:

  • agricultural (without a cargo-passenger cabin, with tanks or bunkers for spraying and spraying chemicals with a strip of 20-60 m wide at a flight speed of 30-130 km / h);
  • transport (with a cargo-passenger cabin for transporting 6 passengers or goods weighing 900 kg or with a cargo platform instead of a cabin);
  • sanitary (for transporting two patients on a stretcher and two on seats with an accompanying paramedic and equipment);
  • Forest patrol (for patrolling forests and rescue operations in case of fire; equipped with an electric hoist LPG-150 with a lifting capacity of 150 kg with a cable length of 40 m and a hook);
  • flying crane (for installation and transportation of goods weighing 900 kg on an external sling, when the goods due to the dimensions are not placed on the cargo platform);
  • ship rescue (with electric hoist ЛПГ-150-M3, with a system for raising victims, a rescue boat LAS-5М3 with a radio station "Coral" and a television camera, emergency balloons for landing on water);
  • patrol (for traffic police, with loudspeakers, electric winch, cargo hook , can be equipped with a television camera and used for shooting from the air).
  • geological exploration with magnetic exploration equipment located in the cargo-passenger cabin and a ring antenna mounted around the fuselage.

All options except ship and exploration could be converted from one to another by a team of two or three technicians in less than a working day. It is also possible re-equipment of the ship version in all but exploration.

  • Ka-26ss is an experimental model for studying the jet control system of a helicopter and the compensation of the rotor torque of a rotor known as NOTAR [1] .

Flight performance

Data Source: [2]

Specifications
  • Crew : 2 people
  • Passengers: 6 people
  • Payload : 700 kg
  • Length : 7.75 m
  • Rotor Diameter: 13.00 m
  • Height : 4.05 m
  • Maximum take-off weight : 3250 kg
  • Powerplant : 2 × PD M-14V-26
  • Engine power: 2 × 325 l. from. (2 × 239 kW)
Flight characteristics
  • Maximum speed: 170 km / h
  • Cruising speed : 135 km / h
  • Practical range: 520 km
  • Practical ceiling : 3000 m


Records

5 world records were set on the helicopter, including: altitude record for helicopters with take-off weight in the class of 1750-3000 kg - 5330 m

  • Rate of climb: reaching a height of 3000 m in 8 minutes 51.2 seconds [3] .

Operation

 
The Ka-26 helicopter performs aviation chemical work.

Received the most effective application in the performance of aviation chemical work.

It was widely used in the national economy of the USSR, many machines are in operation now (2009).

Operators

  •   Russia
  •   Belarus
  •   Bulgaria
  •   Hungary
  •   Sweden
  •   Mongolia
  •   GDR
  •   Sri Lanka
  •   Romania
  •   Japan
  •   USA (sold through a shell company)

and other countries.

Disasters and Accidents

date ofBoard numberPlace of disaster or accidentVictims / On boardShort description
09/19/1969  24052  а / п Krasnovodsk5/6Failure in the operation of engines due to the complete exhaustion of fuel. Knowing that the fuel supply was at the limit, the pilot did not take the only right decision to choose a site for emergency landing [4] .
07/13/1972  24097  Bashkir Autonomous Soviet Socialist Republic , Kaltasinsky district , 3 km east of the village Sharipovo6/6The cause of the disaster was a deliberate reduction and violation by the helicopter commander of a safe flight height, after which he could not cope with the piloting and allowed a collision with trees.
12/27/1972  19392  Orenburg region , Perevolotsky district , 3 km north-east of the village. Abramovka2/2The reduction of the helicopter by the pilot to a height below safe for visual flight. The helicopter suddenly fell into the fog over a landmarkless snowy terrain, as a result of which it collided with the ground [5] .
06/09/1974  19487  is unknown1 / n d.FAC performed a flight while intoxicated. The helicopter crashed.
07/16/1974  19473  Ukrainian SSR , Zaporizhzhya region , near the village. Orekhovka, Priazovsky District5/5The cause of the disaster was a lightning strike in a helicopter and the occurrence of a fire in flight [6] .
12/09/1974  24070  Ukrainian SSR , Kharkov region , near the village. Bidylo, Krasnokutsky district5/7Faced in the wires of power lines , advanced 25 meters on the ground, collapsed and burned. Violation by the pilot of the flight mode at an altitude below safe [7] .
02/13/1975  19350  Stavropol Territory , Neftekumsky District , 10 km southeast of n. item Zereterechny2/2The main cause of the disaster is a helicopter flight below a safe height with the horizon turned off over a snowy field in the presence of bright sun and poor visibility of the natural horizon, which led to a loss of spatial position.
02/13/1975  19556  Stavropol Territory , Budyonnovsk District , near Budyonnovsk0/2The main cause of the disaster was helicopter flight below a safe height above a snowy field in the absence of landmarks and the visibility of the natural horizon, which led to a loss of spatial position.
05/14/1975  19509South Pacific2/2According to the commission, the cause of the disaster was the separation of the rotor blade.
07/29/1975  24090  Ryazan region , Novoderevensky district , near the village Olkhovka1/3The cause of the accident was the criminal actions of the pilot V. Bystrov, his gross violations of discipline and flight rules in isolation from the base - the flight in a drunken state
03/23/1976  19482  Voronezh region , Kalacheevsky district , 7 km north of n. p. Podgornoye3/3The error in calculating the minimum height in weather is worse than the minimum [8] .
07/06/1976  24055  Ukrainian SSR , Kherson region , 5 km north-west of the village of Burgunka, Berislavsky district1/1The helicopter performed aerochemical work. According to witnesses, the helicopter began to rotate on its axis to the right and soon fell to the ground in the vineyards and completely burned down. Reason: destruction of the power transmission of the gearbox [9] .
01/05/1977  19656  Oryol Oblast , Pokrovsky District , near the village Alexandrovka0/2As a result of a pilot error due to the negligence of the crew (acting commander V. Radetsky, navigator Lyalenkov Yu.V.), the leading helicopter crashed into the follower, as a result of which the follower helicopter crashed and burned down. His crew, consisting of the PIC and the official passenger aboard, died [10] .
07/29/1977  19480  Moldavian SSR , Criuleni district , 1 km southwest of Vadul-lui-Voda1/1The cause of the disaster was a solid object (a stone thrown from the ground) falling into the rotor blade, which caused the destruction of the blade, the helicopter was completely unbalanced and became uncontrollable. In this situation, the pilot physically could not prevent the catastrophic situation [11]
08/02/1977  19397  Ukrainian SSR , Kherson region , near n. Gladkovka village, Golopristansky district1/1Carried out aircraft chemical work. The right engine failed, as a result of which the helicopter began to involuntarily decline and collided with power lines [12] .
04/16/1979  24380  а / п Leningrad ( Rzhevka )2/2The emergency situation in flight arose as a result of the breakdown of the dynamic thrust of the blade No. 1 of the upper bearing system with its subsequent lowering into the plane of rotation of the lower bearing system [13] .
06/06/1979  24358  Kazakh SSR , Chimkent region , Leninsky district, 5 km east of the village. Karatobe of the Lenger region2/2Collision of a helicopter with power lines wires. It was not possible to unambiguously determine the cause of the disaster due to the complete destruction of the helicopter and its components [14] .
06/23/1979  24320  Stavropol Territory , Karachay-Cherkess Autonomous Okrug , 1.5 km south of Ust-Dzheguty3/3Collision of a helicopter with power lines and a fall into the river [15] .
11/02/1979  19515  Kazakh SSR , Guryev region , 26 km north of n. n. New Ushtagan2/2The main cause of the disaster was the breakage of the upper rotor blade on the finger of the axial joint of the sleeve No. 3 of the upper sleeve [16] .
02/19/1980  19520  Moldavian SSR , Grigoriopol district , n. n. Novovladimirovka1/2The cause of the accident was the PIC error in determining the actual wind speed when hovering and turning in place. A concomitant reason was the alignment of the helicopter, which was close to the extreme front [17] .
05/17/1980  19458  Stavropol Territory , Kochubeyevsky District , 11.5 km south of Nevinnomyssk1/1The exact cause of the disaster due to significant destruction and fire has not been established. Possible failure of control systems [18] .
03/23/1981  19286  Bashkir Autonomous Soviet Socialist Republic , Ilishevsky District , 2 km southeast of n. Kyzyl-Yulduz (Red Star)1/2Faced power lines from distraction from piloting [19] .
04/09/1981  19490  Karelian Autonomous Soviet Socialist Republic , Medvezhyegorsk district , Putkozero , near n. Shunga2/2According to eyewitnesses during the flight, a “howling” sound of engines appeared. From the helicopter, the parts of the main rotors began to separate, then the main system with the gearbox and part of the gearbox parted off. With a steep decline and simultaneous left rotation around the vertical axis, the helicopter fell onto the ice, collapsed and caught fire. The reason is the internal destruction of the gear in flight [20] .
04/30/1982  19380  Lipetsk region , Lebedyansky district , near n. Kulikovka-21/2Carried out aircraft chemical work. After finishing work, he flew against the sun below a safe height and collided with telephone and telegraph wires stretched across the river. The collision resulted in the destruction of the rotor blades and damage to the structure of the helicopter. After a collision with the wires, the helicopter went into cabling, and after losing translational speed - into a dive, and with the left bank collided with the right side of the bow of the pilot's cabin with the surface of the water, flying 200 m from the communication line. The helicopter collapsed and sank [21] .
07/10/1982  24332  Primorsky Territory , Kirovsky district , near n. p. Pavlo-Fedorovka2/2After carrying out aviation chemical work, the helicopter pulled in the direction of a large state farm field and began to decline at a small vertical speed. The flight course crossed the swampy, hummocky, high-grassed valley of the Shmakovka River. Then, at an altitude of 20-25 m, the helicopter went into a vigorous decline with a right turn and roll until it collided with a tree 6 m high, standing in a row with other trees on the field border, collapsed and completely burned down. The true cause of the disaster could not be established in connection with the destruction of most of the structure of the helicopter, its systems and units in case of fire. Perhaps a failure in the control system [22] .
11/24/1983  24085  а / п Kirovsk0/1There were obstacles at the chosen takeoff course (communication line posts). After a control hover, the aircraft commander began to disperse with virtually no climb, believing that there were no wires between the posts. However, the wires were, but poorly visible on the general background of the area, as they were covered with hoarfrost. Flying 120 m, at a height of 6 m, the helicopter collided with the wires of the communication line, fell to the port side and collapsed [23] .
05/13/1984  19513  Primorsky Territory , Shkotovsky District , Romanovka Village1/2The cause of the accident was the unintentional withdrawal of the helicopter beyond the limits of the rear windward (more than 5 m / s), which led to a temporary loss of longitudinal controllability when the helicopter moves backward in the tail-forward position. The outcome of the flight was influenced by the front alignment of the helicopter, close to the maximum permissible [24] .
07/28/1984  19365  Ukrainian SSR , Kherson region2/2The pilot performed a ferry flight with an official passenger on board. When approaching, the main gearbox R-26 failed (breakage of the shafts of the upper and lower rotors). An uncontrolled helicopter collided with the ground and collapsed [25] .
02.24.1985  19674  а / п Segezha1/1The crew performed a transport-connected flight. After takeoff, the helicopter suddenly fell into a strip of industrial smoke and clouds. FAC (3365 hours of flight on Ka-26, total flight time of 12297 hours) decided to return Segezha to the airport of departure. Upon return, the pilot lost visual contact with landmarks. The helicopter with a decrease and with the right bank collided with the ground on the right side of the runway 400 m from its end and collapsed.
05/11/1985  19673  Astrakhan region , Liman district, near the village. Estuary1/1FAC (4219 hours of flight on the Ka-26) performed a transport-connected flight. In flight at an altitude lower than safe, he distracted himself from piloting and, due to insufficient prudence, allowed a collision with power line wires. The helicopter crashed to the ground, collapsed and burned down. FAC died.
04/21/1986  24317  Belgorod region , 29 km from Belgorod airport3/3The crew performed a ferry flight. During a flight in the TIR zone of the Belgorod airport in conditions of rain and low cloudiness, communication with the board was lost. A crashed helicopter was discovered 29 km from Belgorod Airport. He collided with trees at an angle of 50 ° to the earth's surface and completely collapsed.
05/06/1986  19625  Moldavian SSR , near Dubossar1/2Carrying out aircraft chemical work, not maintaining the safe height of the overhead power line span, collided with a power line wire and crashed [26] .
07/15/1986  19654  Kaluga region , n. v. Novosyolki1/1FAC (attack on the Ka-26 2225 hours), without prior application for flight, independently flew to the site at n. n. Novosyolki and began to carry out the AHR without control by the command and flight staff of its readiness, without conducting an inventory of the fields and not knowing the location of the obstacles. Performing a flight over the cultivated area at an altitude of 5-7 m, the helicopter collided with power lines, collapsed and burned down. FAC died.
05/23/1989  19615  Alfatar1/1Carried out aircraft chemical work. Performing a call to the cultivated area with the intersection of power lines with a height of 13 m, the pilot made a collision with the wires. An uncontrolled helicopter crashed to the ground, collapsed and burned [27] .
01/20/1990  19273  near the village of New-Aktanyshbash, Krasnokamsky district, Bashkir Autonomous Soviet Socialist Republic4/4Hooked on a power line. Killing all those on board.
05/16/1990  19312  Belorussian SSR , Brest region0/1The emergency situation began to develop after a 90 ° turn and exit to the tailwind component of the wind. The aircraft commander noticed a drop in RP speed from 96% to 90%, speeds less than 50 km / h, the appearance of a decrease in helicopter. Instead of taking the helicopter out of the U-turn and increasing the translational speed, the FAC continued the U-turn. The helicopter collided with the ground, capsized, collapsed [28] .
03/20/1995   Tyumen region , Khanty-Mansi Autonomous Okrug , 40 km from Nizhnevartovsk0/4On the 30th minute of the flight, there were signs of a failure of the right engine. PIC decided to perform an emergency landing in front of him, on a forest. The helicopter sustained serious damage, including the destruction of the HB blades, the struts of the right and the upper attachment points of the front shock struts. FAC and passengers were not injured.
09/15/2002   Moscow Region , Noginsk District , Noginsk5/5At the final stage of the flight over the multi-storey buildings in Noginsk, at an altitude of about 30 m above the roofs of the houses, the helicopter crew ( Honored Test Pilot of the Russian Federation V. A. Lavrov [29] and the deputy chief for flight training of the Regional ATSC ROSTO of the city ​​of Noginsk O. E Podporin), trying to get away from a collision with a flock of birds, undertook a sharp maneuver of decline. The helicopter hooked on a cable stretched on a metal cable between the roofs of two 9-story buildings, lost control, fell to the ground, collapsed and burned down [30] [31] .
03/14/2003  00594  30 km east of Krasnoyarsk3/3The helicopter took off at 5.01 (Moscow time) on the route Krasnoyarsk - Rybnoye - Nizhnyaya Poima. As a result of the fall of the car, a pilot, a flight engineer and a customer representative died [32] [33] .
05/07/2010  ER19358  near the village of Podgorodnaya in the Nikolaev region.1/1During agricultural operations, the screw caught on the high-voltage power line [34] .
08/26/2010   near the village of Velikaya Mikhailovka , Odessa region2/26 km north of the village of Velikaya Mikhailovka. When landing during an overhead gas pipeline at an altitude of 3-5 m, the breakage of the rotor blade. Killed the pilot and master of the gas section.
03/19/2011  RA-24313  airfield Zabelsky0/2Loss of altitude control and collision with the earth's surface after hovering completed. Pilot error as a result of loss of pilot skills (interruption of more than 12 years) [35] .
03/05/2014  RA-1927G  Rostov region0/1The helicopter is damaged, the pilot was not injured, an investigation is underway [36] .
05/19/2016  LZ-6042  near Nessebar1/1The helicopter crashed during agricultural work.
04/12/2018  HA-MCH 0 / n d.A helicopter with a load of fertilizers crashed during takeoff during agricultural work. No one was hurt [37] .
05/23/2018  0/2The helicopter crashed during agricultural work. Both men in the cockpit managed to survive [38] .
05/08/2019n d.  near the village of SapantaelevenThe body of a pilot - a citizen of Belarus who disappeared two months before, and a destroyed helicopter without identification marks were found in a forest near the Romanian-Ukrainian border. Presumably, the pilot was engaged in smuggling and tried to illegally cross the border at night at low altitude [39] [40] .

Gallery

  •  

    Helicopter Ka-26 in Ukraine.

  •  

    Ka-26 in Hungary (2004).

  •  

    Helicopter Ka-26 in Hungary (2005).

  •  

    Stamp with the image of the Ka-26 (1980).

  •  

Ka-26 in the movies

The widespread use of the Ka-26 helicopter in agriculture and the traffic police of the USSR predetermined its demand on the Soviet cinema screen. It can be seen in many detective and comedy films of 1970-1990.

  • In the parody comedy “The Old Robbers ”, the hero of Yuri Nikulin flies in dreams over the city, hanging on the stairs attached to the helicopter.
  • In the comedy film “ The Dog Walked on the Piano, ” the agricultural Ka-26, like its young pilot, is practically one of the heroes of the film.
  • In the film “ Everything will be fine! »The helicopter of the GAI accompanies the convoy.
  • In the children's film “ Three Happy Shifts, ” in the second film on Ka-26, Pavel, a friend of Mikoshi, works.
  • In the detective film " Detective " - a traffic police helicopter.
  • In the Hungarian comedy-detective film Pagan Madonna , 1980, detective superman Kapelka is chasing international criminals on the Ka-26 in the colors of the local traffic police.

Notes

  1. ↑ Kuznetsov G.I., Design Bureau N.I. Kamov. Volume 1
  2. ↑ Ka-26
  3. ↑ History of Helicopter Records (inaccessible link)
  4. ↑ The accident of Ka-26 of the Myachkovsky OJSC in the airport Krasnovodsk (USSR-24052), September 19, 1969. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and ...
  5. ↑ Catastrophe Ka-26 of the Ukrainian CAA in the Orenburg Region (USSR-19392 board), December 27, 1972. // AirDisaster.ru - aircraft accidents, incidents and air crashes in the CCC ...
  6. ↑ Catastrophe Ka-26 of the Ukrainian CAA near the village. Orekhovka, Zaporizhzhya region (USSR-19473 board), July 16, 1974. // AirDisaster.ru - aircraft accidents, incidents and air cassettes ...
  7. ↑ Catastrophe Ka-26 of the Ukrainian CAA in the Krasnokutsky district of Kharkov region (USSR-24070 board), December 9, 1974. // AirDisaster.ru - aviation accidents, incidents and ...
  8. ↑ The Ka-26 crash of the Kaluga UGAC OJSC in the Kalach region (USSR-19482 board), March 23, 1976. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and R ...
  9. ↑ Catastrophe Ka-26 of the Ukrainian CAA in the Kherson region (USSR-24055 board), July 6, 1976. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and R ...
  10. ↑ Disasters of Belarusian civilian aircraft // Museum of Aviation Engineering - Borovaya .
  11. ↑ Catastrophe Ka-26 of the Moldavian UGA near Vadul-lui-Voda .
  12. ↑ Catastrophe Ka-26 of the Ukrainian CAA in the Kherson region (USSR-19397 board), August 2, 1977. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR ...
  13. ↑ Catastrophe of Ka-26 of the Leningrad UGA in the a / p Leningrad (Rzhevka) (USSR-24380), April 16, 1979. // AirDisaster.ru - aviation accidents, incidents and air crashes in ...
  14. ↑ Catastrophe Ka-26 of the Uzbek UGA in the Chimkent region (USSR-24358 board), June 6, 1979. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and R ...
  15. ↑ Catastrophe Ka-26 of the North Caucasian CAA in the region of Ust-Dzheguty (board of the USSR-24320), June 23, 1979. // AirDisaster.ru - aviation accidents, incidents and air crashes in ...
  16. ↑ Catastrophe Ka-26 of the North Caucasus CAA in the Guryev region (USSR-19515 board), November 2, 1979. // AirDisaster.ru - aviation accidents, incidents and air crashes in ...
  17. ↑ Catastrophe Ka-26 of the Moldavian RPO GA in n. Novovladimirovka settlement (USSR-19520 board), February 19, 1980. // AirDisaster.ru - aviation accidents, incidents and air crashes in ...
  18. ↑ Catastrophe Ka-26 of the North Caucasian CAA in the region of Nevinnomyssk (USSR-19458 board), May 17, 1980. // AirDisaster.ru - aviation accidents, incidents and air crashes in ...
  19. ↑ Catastrophe Ka-26 of the Volga UGA in the Ilishevsky district of the Bashkir Autonomous Soviet Socialist Republic (USSR-19286), March 23, 1981. // AirDisaster.ru - aircraft accidents, incidents and airplanes ...
  20. ↑ AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and Russia - facts, history, statistics
  21. ↑ Catastrophe Ka-26 of the Moldavian RPO GA in the Lipetsk Region (USSR-19380 board), April 30, 1982. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR ...
  22. ↑ Catastrophe Ka-26 of the Far Eastern CAA in the area of ​​n. p. Pavlo-Fedorovka (USSR-24332), July 10, 1982. // AirDisaster.ru - aircraft accidents, incidents and air crashes ...
  23. ↑ The accident of Ka-26 of the Leningrad UGA in the district of a / p Kirovsk (USSR-24085 board), November 24, 1983. // AirDisaster.ru - aviation accidents, incidents and air crashes in the USSR and Russia ...
  24. ↑ Ka-26 crash of the Far Eastern CAA near Romanovka, Primorsky Territory (USSR-19513 board), May 13, 1984. // AirDisaster.ru - aircraft accidents, incidents and air crashes ...
  25. ↑ Catastrophe Ka-26 of the Ukrainian CAA in the Kherson region (USSR-19365 board), July 28, 1984. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and R ...
  26. ↑ The Ka-26 crash of the Moldavian UGA in the Dubossar area (USSR-19625 board), May 6, 1986. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and Russia ...
  27. ↑ Ka-26 crash of the Moldavian UGA in Bulgaria (board of the USSR-19615), May 23, 1989. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and Russia - fact ...
  28. ↑ Ka-26 accident of the Belarusian UGA in the Brest region (USSR-19312 board), May 16, 1990. // AirDisaster.ru - aviation accidents, incidents and air accidents in the USSR and Russia ...
  29. ↑ Lavrov Vladimir Alexandrovich . (1951-2002) (neopr.) . "Testers" - a portal of aerospace technology . TestPilot.ru (January 8, 2009) . Date of appeal October 26, 2018.
  30. ↑ Andrei Salnikov. A helicopter was cut by a bird flock : All who were on board died // Kommersant : gas. - 2002. - No. 166 (September 16). - S. 4. - ISSN 1561-347X .
  31. ↑ Catastrophe of Ka-26 of the Regional ATCC ROSTO in Noginsk (Neopr.) . Air accidents, incidents and air accidents in the USSR and Russia . AirDisaster.ru. - Facts, history, statistics. Date of appeal October 26, 2018.
  32. ↑ A criminal case has been instituted on the accident of Ka-26 | RIA Novosti news feed
  33. ↑ https://www.gazeta.ru/2003/03/14/last79794.shtml
  34. ↑ newspaper "Ukraine Young"
  35. ↑ See the results of the investigation of the Interstate Aviation Committee Archived on April 10, 2009.
  36. ↑ 05.03.2014 Ka-26M "Master" RA-1927G (unavailable link)
  37. ↑ https://aviation-safety.net/wikibase/209185
  38. ↑ https://aviation-safety.net/wikibase/211347
  39. ↑ https://aviation-safety.net/wikibase/224903
  40. ↑ https://sputnik.by/incidents/20190510/1041103957/Propavshiy-v-Karpatakh-belorus-razbilsya-na-vertolete-v-Rumynii.html

Links

  • Ka-26 in the aviation encyclopedia "Corner of the sky"
  • Ka-26 in the virtual encyclopedia of rotorcraft "All helicopters of the world"
  • OKB Kamov at the International Joint Biographical Center
Source - https://ru.wikipedia.org/w/index.php?title=Ка-26&oldid=100772633


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Clever Geek | 2019