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MS-14

The engines MS-14 are designed to be used together with the AV-17 or AV-36 propellers in regional line airplanes accommodating up to 30 passengers. The engine can be used in the An-3, An-38, and Be-132MK aircraft.
High level of designing and production capabilities gave the opportunity to create the engines that feature high performance, reliability and long service life.
The engines comply with the requirements of Aviation Rules AP-33.

Main advantages of the engine:

  • high economy;
  • reliability and trouble-free operation;
  • the engine is controlled by combined electrohydraulic control and monitoring system featuring full electronic authority;
  • levels of pollutant emission and exhaust opacity are lower than those required by ICAO Standards;
  • low noise level.

Basic specifications:

Takeoff power condition (H=0, Mfl=0, ISA +25°C)
Propeller shaft horsepower, hp (kW) 1500(1103)
Specific fuel consumption, kg/eq.hp·h (kg/eqkW·h) 0.240(0.326)
Maximum cruise power condition (H=3000 m, Mfl=0.35, ISA +60°C)
Propeller shaft power, hp (kW) 1050 (772)
Specific fuel consumption, kg/eq.hp·h (kg/eqkW·h) 0.255 (0.347)
Dry weight, max, kg 310+10



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Applicability


  • An-3
  • An-38
  • Be-132MK

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