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TA-14 is a contemporary auxiliary gas-turbine engine with the equivalent power up to 108 kW. This engine is designed for aircraft and helicopter APUs. 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 noise level of the TA-14 engine, when installed on the craft, does not exceed 87 dBA.

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.

 

The engine complies with the requirement of the Aviation Rules (section Auxiliary Engines) and has a type certificate 203-VD issued by the Aviation Register of the Interstate Aviation Committee (27.12.2001).

APPLICATION: Il-112, Il-114, Tu-324, An-140, MiG-110, Mi-8AMT, Mi-8MTB, S-80, Ka-62.

Technical features:

Absorbed electric power of AC, kVA

20

Bleed air consumption, kg/s

0,55

Bleed air pressure, kgf/sm2

3,70

Bleed air temperature, C

205

Start and operation altitude, m

9000

Environmental temperature,

60

Weight (without generator), kg

56

Overall dimensions, mm

840510455

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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