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TA-14-130 is a contemporary auxiliary gas-turbine engine with the equivalent power up to 106 kW. This engine is designed for APU of Jak-130 aircraft. It is used for air turbine start of the main aircraft engines, supplying on-board AC electric power  (200/115 V, power up to 20 kWA) and providing air conditioning for cockpit and cabins.

The engine is equipped with a highly efficient turbo compressor and integrated system of oil cooling. As a result, fuel consumption and the weight is reduced.

The engine is compliant with the contemporary market requirements and is equipped with a full-authority electronic digital control system that provides regulation, control and error detection as well as operation time counter.

APPLICATION: Jak-130.

Technical features:

Absorbed electric power of AC, kVA

20

Bleed air consumption, kg/s

0,55

Bleed air pressure, kgf/sm2

3,65

Bleed air temperature, C

210

Start and operation altitude, m

9000

Environmental temperature,

60

Weight (without generator), kg

63

Overall dimensions, mm

835507440

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Address: 6, Zhdanov Str., Stupino,
Moscow region, Russian Federation, 142800,
Tel.: (496) 642-33-30 Fax: (496) 642-04-24
Email: vint@aerosila.ru