ENGINE CHARACTERISTICS
- Turbocharged version
- 4-cylinder - 4-stroke liquid/air cooled engine with opposed
- Dry-sump forced lubrication with separate oil tank
- Automatic adjustment by hydraulic valve tappets
- Propeller speed reduction gearbox
- Supplementary alternator mounted coaxial with the crankshaft
- Air intake manifold in composite carbon fiber material
- Redundant electronic fuel injection system
- Closed-loop engine management system based on lambda sensor control
- CANBUS output with engine parameters to be sent to the aircraft instrumentation
- CANBUS strategies
- Fans management
ENGINE PERFORMANCE
| SPEED (rpm) |
POWER (kW) |
POWER (hp) |
TORQUE (Nm) |
| 5800 |
100*** |
135 |
164 |
| 5500 |
81** |
110 |
141 |
| 5800 |
MAX RPM* |
MAX RPM* |
MAX RPM* |
* Limited to max 5 min.
** Max continous power @ 5500 rpm
*** Unleaded RON 100, no hydraulic governor
ENGINE DATA
| BORE (mm) |
STROKE (mm) |
DISPLACEMENT (cm3) |
| 84,1 |
61,0 |
1355 |
