Engine VK-2500PS-03
Is a further development of the VK-2500 engine family. Thanks to new design solutions, the engine ensures more trouble-free operation of helicopters in high mountains and hot climates.
Technical characteristics
| Engine power in emergency mode | 2,700 hp |
| Engine power at takeoff | 2,000 hp |
| Specific fuel consumption at takeoff | 0.220 kg/hp h |
| Dry weight | 290 kg |
| Resource between repairs / assigned | 3,000 / 9,000 h |
Advantages
- FADEC type control system.
- Training mode of operation, providing safe training for pilots to act upon simulating failure of one engine.
- Objective monitoring of basic operational parameters with output to the pilot’s cockpit.
- Limit engine starting altitude - 6,000 meters
- 8 engine outputs for “PD 2,700” mode, 2.5 minutes per resource.
Application
- Mi-171A2. Mi-171 is a Soviet/Russian civil transport helicopter developed by the M. L. Mil Design Bureau, a modification of the Mi-8 helicopter - Mi-8AMT. The military modification of the Mi-8AMTSh helicopter was put into service in 2009.
- Mi-171A3. The newest aircraft is designed to deliver people and cargo to offshore drilling platforms, as well as conduct search and rescue operations on the high seas. The Mi-171A3 has unique transport capabilities in the offshore class. With a maximum take-off weight of 13 tons, this rotorcraft can carry up to 4 tons of cargo or up to 24 passengers. The helicopter's flight range with additional fuel tanks reaches 1000 km.
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