915 iS A | iSc A | iS C24 | iSc C24 141 HP
Dynamic iS engine with best power-to-weight ratio, full take-off power and a service ceiling up to 23.000 feet.
- Four-stroke piston engine with four liquid and air-cooled cylinders
- Redundant electronic fuel injection and ignition, eco mode
- Turbocharger, stainless steel exhaust
- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets
- Engine management system (EMS)
- Electric starter (12 or 24 volt)
- Propeller speed reduction gearbox
- Air intake system / intercooler
- TBO 1,200 hrs
- Maximum operating altitude 23.000 feet
- Customizable version available (engine comes with neutral black covers and without logo branding, ready to get your very individual design)
- 24V power supply delivering up to 800W
Engine configurator
Set up your individual rotax engine with our engine configurator.
Launch configurator
Engine Data
| WEIGHT | kg | lb |
| Engine with propeller speed reduction gearbox i = 2,54 with overload clutch, turbocharger, intercooler, exhaust system | 82.2 | 181.2 |
| Engine suspension frame | 2.0 | 4.4 |
| External alternator | 3.0 | 6.6 |
| Air guide hood | 0.4 | 0.8 |
| Fuel pumps assy | 1.6 | 3.5 |
| PERFORMANCE | ||
| 104kW | 141 hp | |
| **99.0kW | 135 hp |
| BORE | |
| 84.0 mm | 3.31 in |
| STROKE | |
| 61.0 mm | 2.4 in |
| DISPLACEMENT | |
| 1352 cm³ | 82.6 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
iS: ASTM compliant | iSc: certified according to EASA CS-E
