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
ROTAX 916 IS/ISc/IS C24/ISc C 24 (160 HP)

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

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