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AI-8

The APU is designed for starting the AI-20, AI-24 and D-25V turboprop and turboshaft engines, as well as for feeding various aircraft electrical systems.

Main advantages of the engine:

  • high reliability;
  • simple design;
  • simple and optimal maintainability.

Basic specifications:

Power across generator terminals, kW 60
Fuel consumption, kg/h, max 120
Dry weight, kg, max 145



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Applicability


  • Mi-6
  • Mi-10
  • Be-12
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Last updated: February 08, 2012

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