916 iS A | iSc A | iS C24 | iSc C24 160 HP

Dynamic, turbocharged iS engine with best power-to-weight ratio and TBO 2,000h.
- 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
- Intercooler
- TBO 2,000 hrs
- Maximum operating altitude 23,000 feet
- Full take-off power up to 15,000 feet
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 | 85.8 | 189 |
| Engine suspension frame | 2.0 | 4.4 |
| External alternator | 3.0 | 6.6 |
| Air guide baffle | 0.4 | 0.8 |
| PERFORMANCE | ||
| 117 kW | 160 hp | 5800 1/min |
| **101 kW | 137 hp | 5500 1/min |
| TORQUE | ||
| 193 Nm | 142 ft lb | 5800 1/min |
| 175 Nm | 129 ft lb | 5500 1/min |
| 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
iS: ASTM compliant | iSc: certified according to EASA CS-E
Downloads
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