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The engine is designed for civil, passenger and cargo airplanes of local and regional airlines.
High-tech development and production have enabled to create the TV3-117VMA-SBM1 engine possessing superior operating performances, dependability, and extensive service life.

Main advantages of the engine:

  • High efficiency;
  • Long service life;
  • Reliability and trouble-free operation;
  • Engine and propeller joint electronic control system;
  • Two emergency power conditions making it possible to take off and maintain a flight level with one engine inoperative;
  • Low-emission combustor;
  • Low noise level;
  • Low operating costs;
  • Flat-rating up to high ambient temperatures.

Basic specifications:

Maximum emergency power condition: (SLS, ISA +22°C)
Propeller shaft horse-power, shp (kW) 2800 (2059)
Emergency power condition: (H=5170 m, Hfl=0.3, ISA +10°C)
Propeller shaft horse-power, shp(kW) 2130 (1567)
Takeoff power condition: (SLS, ISA +15°C)
Propeller shaft horse-power, shp (kW) 2500 (1838)
Specific fuel consumption, kg/ehp.•h (kg/eqkW•h) 0.199 (0.270)
Maximum cruise power condition: (H=6000 m; Mfl=0,5; ISA)
Propeller shaft horse-power, shp (kW) 1750 (1287)
Specific fuel consumption, kg/ehp•h (kg/eqkW•h) 0.188 (0.256)

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