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MS-500V

The engines are intended for installation in civil purpose helicopters with takeoff mass of 3.5 to 6 t and permit to attain high economic standards in the course of commercial use.

Main advantages of the engine:

  • simple and effective design;
  • high reliability;
  • low specific fuel consumption;
  • high stability of characteristics in service;
  • compliance with current and future environmental requirements;
  • extended service life and durable calendar life;
  • ease and convenience of maintenance and repair;
  • low cost of life cycle.

Basic specifications:

Engine MS-500V MS-500V-01 MS-500V-02
With one engine inoperative (OEI) (SLS, ISA):
2,5-min power; hp (kW)
(flat-rated to tAMB, °C)
710 (522)
(+35)
1000 (735)
(+15)
1200 (833)
(+20)
30,0-min power; hp (kW)
(flat-rated to tAMB, °C)
659 (485)
(+40)
850 (625)
(+30)
1000 (735)
(+35)
Take-off power rating (SLS, ISA):
Power, hp (kW)
(flat-rated to tAMB, °C)
630 (463)
(+35)
810 (596)
(+35)
950 (699)
(+35)
Cruise power rating (SLS, ISA)  
Power, hp (kW)
(flat-rated to tAMB, °C)
450(331)
(+50)
450(331)
(+50)
500(368)
(+50)

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