ROTAX 916 IS/ISc/IS C24/ISc C 24 (160 HP)
-Dynamic, turbocharged iS engine with best power-to-weight ratio, full take-off power, and a maximum operating altitude 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*** )
- PropellerPropeller speed reduction gearbox
- Intercooler
- TBO 2,000 hrs
- Maximum operating altitude 23,000 feet
- Critical altitude 15,000 feet (maximum continuous power) *** 24 Volt available mid 2024
ENGINE DATA 916 iS
| 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 | 5.800 1/min | |
| ***101 kW | 137 hp | 5.500 1/min | |
| Torque | |||
| 193 Nm | 124 ft lb | 5.800 1/min | |
| 175 Nl | 129 ft lb | 5.500 1/min | |
| BORE | STROKE | ||
| 84.0 mm | 3.31 in | 61.0 mm | 2.4 in |
| DISPLACEMENT | FUEL* | ||
| 1352 cm³ | 82.6 cu in |
min. MON 85 RON 95 min. AKI 91 |
|
* leaded, unleaded, AVGAS 100LL, Ethanol 10
** max. continuous power at 5500 1/min