Product Description
| Rotax915 iSA| iScA |iS C24 |iSc C24 Aircraft Engines |
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 |
| |
**99.0kW |
135 |
| 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
Dynamic iS engine with best power-to-weight ratio.
- 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
Audited Supplier 
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