914 UL | F 115 HP
Low-weight engine with excellent performance at high altitudes.
- Four-stroke piston engine with four liquid and air-cooled cylinders
- Turbocharger
- Automatic wastegate control
- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
- 2 carburetors
- Dual electronic ignition
- Electric starter
- Propeller speed reduction gearbox
- Engine mount assembly
- Air intake system
- Exhaust system
- TBO 2,000 hrs
ENGINE DATA
| WEIGHT | kg | lb |
| Engine with propeller speed reduction gearbox i = 2.43 | 64.0 | 140.8 |
| Exhaust system | 4.0 | 8.8 |
| Engine suspension frame | 2.0 | 3.7 |
| Overload clutch | 1.7 | 3.7 |
| External alternator | 3.0 | 6.6 |
| PERFORMANCE | ||
| 84.8 kW | 115 hp | 5800 1/min |
| TORQUE | ||
| 144 Nm | 106 ft. lb. | 4900 1/min |
| Max RPM |
| 5800 1/min |
| BORE | |
| 79.5 mm | 3.13 in |
| STROKE | |
| 61.0 mm | 2.4 in |
| DISPLACEMENT | |
| 1211.2 cm² | 73.91 cu in |
| FUEL* |
| min. MON 85 RON 95* min AKI 91* |
Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.
* leaded, unleaded, AVGAS 100LL, Ethanol 10
** max. continuous power at 5500 1/min
*** MOGAS, no hydraulic governor
