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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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