Private company

Aviadvigatel

Logo: ОАО «Авиадвигатель», CC BY-SA 3.0, via Wikimedia Commons3

Russian manufacturer of aircraft engines

UEC-Aviadvigatel JSC (Russian: АО ОДК-Авиадвигатель, lit. 'Aeroengine') is a Russian developer and builder of aircraft engines, most notably jet engines for commercial aircraft. Based at the Perm Engine Plant, its products power the Ilyushin Il-76MF, Ilyushin Il-96, Tupolev Tu-204, and Tupolev Tu-214. It also designs and builds high-efficiency gas turbine units for electric power stations and for gas pumping plants.2 It was founded by Arkady Shvetsov.1 Its chief executive is Aleksandr Inozemtsev (since 2001).1 It employed 2,663 people in 2010.1 Its revenue was ₽7.6 billion in 2014.1 It is part of Rostec.1 Wikipedia text CC BY-SA 4.0

Last updated Oct 20, 2026.

Overview

1934Founded1
  • Industrymechanical engineering1
  • HeadquartersPerm1
  • Websitewww.avid.ru
  • Legal formopen joint-stock company1

UEC-Aviadvigatel JSC (Russian: АО ОДК-Авиадвигатель, lit. 'Aeroengine') is a Russian developer and builder of aircraft engines, most notably jet engines for commercial aircraft. Based at the Perm Engine Plant, its products power the Ilyushin Il-76MF, Ilyushin Il-96, Tupolev Tu-204, and Tupolev Tu-214. It also designs and builds high-efficiency gas turbine units for electric power stations and for gas pumping plants. The company has its background in the Experimental Design Bureau-19 plant, set up to manufacture aircraft engines.2

Corporate structure

Aviadvigatel is part of a group headed by Rostec. 128 entities, 3 countries on record. Switch between the flow chart and the network, and select any entity to see its details.

Built from subsidiaries, stakes and holdings from Wikidata (CC0); major holders from Schedules 13D and 13G. Each entity in the chart links to its source.

The story

Founded by Arkady Shvetsov in 1934.1

Foundation and Shvetsov era

Aviadvigatel can be traced back to the engine design and manufacturing factory (Plant No.19) founded in Perm Krai, Russian Soviet Republic, on 1 June 1934, to produce the Wright Cyclone-derived Shvetsov M-25. Arkadiy Shvetsov was named chief designer at the plant, which was also referred to as the Perm Design/Engine School. The school was given the Soviet Experimental Design Bureau designation of OKB-19, and was informally referred to as the Shvetsov Design Bureau.

The first engine to be built at OKB-19 was a licensed variant of the Wright R-1820-F3 Cyclone 9, designated the Shvetsov M-25 radial engine. Other Shvetsov-designed piston engines produced at OKB-19 were the M-11, M-71 ASh-2, ASh-21, ASh-62, ASh-73, and ASh-82. In just four years OKB-19 became the major designer and provider of radial aircraft engines for the Soviet aircraft industry. Aleksandr Mikulin's and Vladimir Klimov's separate OKB design bureaus were assigned for the creation of inline engines.

During World War II the plant exceeded its original design capacity by a factor of 12, producing more than 32,000 engines for Lavochkin La-5, Sukhoi Su-2 and Tupolev Tu-2s. In the 1950s the factory transitioned from piston engines to jet engines. The plant has consolidated its position and has become a regular partner and supplier of products for Tupolev, Ilyushin, Mikoyan, Mil, and Myasishchev.

Soloviev era

After the death of Shvetsov in 1953, leadership was taken over by Pavel Alexandrovich Soloviev, and the OKB was referred to afterwards as the Soloviev Design Bureau. Under Soloviev, the company became notable for the D-15 engine that powered the Myasishchev M-50 in 1957. Other notable designs included the D-25 turboshaft and D-20 and D-30 turbofans.

Post-Soviet era

Since 1989, and up to June, 2001, with a break in 1995-1997, the enterprise was headed by Yuri Evgenievich Reshetnikov.

The Perm Engine Company was established in 1997 as a subsidiary of Perm Motors Company, inheriting the gas turbine production facility and the rich traditions of the largest company of the West Ural. In June 2001 Alexander A. Inozemtsev, the chief designer, became the general director of Aviadvigatel Open Joint Stock Company (OJSC). Starting in October 2006, he was the managing director and chief designer.

In October 2003, "Perm Motors Group Management Company" was established to: 1) coordinate corporate relations and management of the Perm Motors Group companies, 2) resolve strategic marketing matters, and 3) perform investment planning.

"Aviadvigatel" OJSC was merged into the Perm Engine Company, Perm Motors Group.

From Wikipedia’s article on Aviadvigatel, shared under CC BY-SA 4.0.4

Leadership

Who has led Aviadvigatel, and when. Pick a name to see everywhere that person has worked.

197019801990200020102020

Products and brands

  • aircraft engine

Listed on Wikidata.1

Current products

Aviadvigatel PD-12 turboshaft, an upgrade for the Mil Mi-26, to replace the Ukrainian D-136

Aviadvigatel PS-12

Aviadvigatel PS-30, D30K variants, D30F6

Aviadvigatel PD-14 high-bypass turbofan, will power the Yakovlev MC-21

Read the full text

PD-18R geared turbofan 180 kN

PD-12V PD14V Turboshaft 8,500 kW (11,400 shp) for Mil Mi-26

Aviadvigatel PD-8 high-bypass turbofan, will power Sukhoi Superjet 100 (7500 kgf thrust, with a nacelle mass of 2,300 kg)

Aviadvigatel PD-30

UMPO R-195, powers the Sukhoi Su-25

Aviadvigatel PS-90 high-bypass turbofan, which powers Ilyushin Il-76 variants, Ilyushin Il-96 variants, Beriev A-50, and Tupolev Tu-204/214 series

GP-2 (PS-90-GP-2) Gas Turbine

GPA-5,5 (Taurus 60)

GTE-25P (PS-90GP-25) based on PS-90 and GTA-25 unit GTU-25P Gas Turbine

GTU-16P on basis PS-90A and GTU-12P

GTU-12P based on D-30, other GTs (like GTU4P GTU6P)

GTU-8 (6-8,5 MW) and GTU-16 (12,4-16,5 MW) from PD-14

GTU-30P 30 34 MW GTE30 based on D-30F6 and PS-90

GTA-14 14 MW based on Titan-130 Solar Turbines

GTU-32P (up to 34 40 MW) on basis D-30F6 and MS5002E (GPU32 "Ladoga" built in NZL plant in Saint Petersburg)

GTE180 GTE160 GT100 GTE65; unit M94yu2

Building and Development

PD-24 (around ± 240 kN)

PD-26 (around ± 255 kN)

PD-28 (around ± 280 kN)

PD-35 (up to 300/328 kN max 350) for An-124 transport and airliners (along PD24 PD28 scaled up PD14 PD18 cores)

GTUs 30 and 40 MW

Shvetsov engines

Shvetsov ASh-2 - four-row, 28 cylinder radial developed from the ASh-82, 1949; Shvetsov's last piston engine

Shvetsov ASh-21 - single-row, 7 cylinder version of ASh-82, 1947

Shvetsov ASh-62 - known as M-62 before 1941; improved M-25 with a two-speed supercharger and improved induction system, 1937

Shvetsov ASh-73 - two-row, 18-cylinder radial developed from the M-72, 1947

Shvetsov ASh-82 - also known as M-82; two-row, 14 cylinder radial developed from the M-62, 1940

Shvetsov ASh-83 - boosted version of ASh-82FN, 1944

Shvetsov ASh-84

Shvetsov M-11 - five-cylinder radial, 1923

Shvetsov M-22 - Bristol Jupiter built under license, 1918

Shvetsov M-25 - Wright R-1820-F3 Cyclone built under license, 1934

Shvetsov M-63 - improved M-62 with more power due to higher compression and higher redline, 1939

Shvetsov M-64

Shvetsov M-70 - two-row, 18-cylinder version of the M-25, 1938; cancelled due to failures of the master connecting rod and the supercharger impeller

Shvetsov M-71 - improved M-70, 1939; cancelled as there was no production capacity available

Shvetsov M-72 - boosted version of M-71, 1945; superseded by the ASh-73

Shvetsov M-80

Shvestov M-81

Shvetsov M-93

Soloviev engines

Soloviev D-20 low-bypass turbofan, which powered the Tupolev Tu-124

Soloviev D-25 turboshaft, which powers the Mil Mi-6, Mil Mi-10

Soloviev D-30 two-shaft, low-bypass turbofan, which powers the Tupolev Tu-134A-3, A-5, and B, Mikoyan MiG-31, Ilyushin Il-62, Ilyushin Il-76 variants, Beriev A-40, and the Tupolev Tu-154

From Wikipedia’s article on Aviadvigatel, shared under CC BY-SA 4.0.4

Subsidiaries and ownership

Parent company

Owners

From Wikidata.1

Acquisitions

  1. Succeeded Soloviev Design Bureau1

Employees over time

  • 20102,6631

Revenue over time

As stated on Wikidata, in the currency reported.

Revenue

  • 20147.6B RUB1

Timeline

  1. Jun 28, 2001New chief executive Aleksandr Inozemtsev becomes CEO1
  2. 1934Founded Founded1

Sources

The numbers on this page point here. Each one links to the record it came from.

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