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TV3-117VMA-SBM1V, Series 4E

It is used for installation in transport helicopters. The engine features a single-shaft gas generator and free turbine. It maintains the power at high ambient air temperatures, high airfield altitude and high flight altitude. The takeoff power is 1,500 hp. The 2.5-min. power rating ensures safe takeoff and landing of the helicopter with one engine inoperative.

Main advantages of the engine:

  • high reliability;
  • increased power maintained in hot and high conditions;
  • low SFC;
  • long service life;
  • easy in-service maintenance;
  • high repairability;
  • stable operation under conditions of heavy smoke and dust;
  • low cost of life cycle.

Basic specifications:

2.5-minute power rating and
Continuous power rating - 60 min (Cont 1) with OEI
(SLS, ISA +20°C)

Power, shp (KW) 1,700 (1,251)
flat-rated up to tamb, °C +35
Continuous power rating - 60 min (Cont 2) OEI
Continuous takeoff power rating (CTO) 30-min,
Takeoff power rating (SLS, ISA)
Power, shp (kW) 1,500 (1,104)
flat-rated up to tamb, °C +55
Specific fuel consumption, kg/hp•h 0.251
Cruise power setting (SLS, ISA):
Power, shp (kW) 1,000 (736) to +60°C
Specific fuel consumption, kg/hp•h 0.280
Dry weight, kg 295

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