MS-14
The MS-14 (MS-14-01) engines together with the AV-17 or MTV-27 propeller are designed for installation on general aviation short-haul light milti-role aircraft. Engine takeoff power in 1,500 hp. The engine is controlled by means of the digital electronic engine control. When designing the engine, design solutions and technologies were applied to the fullest extent possible. |
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Main advantages of the engine:
- high economy;
- reliability and trouble-free operation;
- the engine is controlled by combined electrohydraulic control and monitoring system featuring full electronic authority;
- levels of pollutant emission and exhaust opacity are lower than those required by ICAO Standards;
- low noise level.
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Basic specifications:
| Takeoff power rating (SLS, ISA +25°C) |
| Propeller shaft horsepower, hp (kW) |
1,500 (1,103) |
| Specific fuel consumption, kg/eq.hp•h (kg/eqkW•h) |
0.237 (0.322) |
| Maximum cruise power rating (H=2,000 m, V=235 km/h, ISA +27°C) |
| Propeller shaft power, hp (kW) |
1,050 (772) |
| Specific fuel consumption, kg/eq.hp•h (kg/eqkW•h) |
0.255 (0.347) |
| Dry weight, max, kg |
310+10 |
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