Designed for the use on light helicopters and aircraft in the take-off weight class of 1500-4000 kg. Usable as part of aircraft twin-engine and single-engine power plants.
| Takeoff (H=0 m; M=0; ISA ) | |
| Power, hp | 465 |
| Specific fuel consumption, kg/h/hp | 0.260 |
| Air flow, kg/sec | 1.72 |
| Мax cruise | |
| Рower, hp | 300 |
| Specific fuel consumption, kg/h/hp | 0.297 |
| Weight, dry (without propfan), kg | 103 |
| Dimensions, mm | 1,085 х 536 х 515 |
| Specified service life, h | 3,000 |
Applicability
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Ка-226