ROTAX 915 iS

915 ISA / ISC A / IS C24 / ISC C24

141 HP

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Dynamic iS engine with best power-to-weight ratio, full take-off power and a service ceiling up to 23.000 feet.feet (7,010 m).

  • 4-cylinder
  • 4-stroke liquid/air-cooled engine with horizontally
    opposed cylinders
  • Dry sump forced lubrication with separate oil tank,
    automatic adjustment by hydraulic valve tappet
  • Redundant electronic fuel injection and ignition
  • Engine management system (EMS)
  • Electric starter (12 or 24 volt)
  • Propeller speed reduction gearbox
  • Air intake system with intercooler
  • Turbocharger with stainless steel exhaust
  • TBO (Time between overhauls) 1,200 hours
  • Maximum Operating Altitude of 23,000 feet
Category:
ENGINE DATA
WEIGHTkglb
Engine with propeller speed reduction gearbox i = 2,54 with overload clutch, turbocharger, intercooler, exhaust system82.2181.2
Engine suspension frame2.04.4
External alternator3.06.6
Air guide hood0.40.8
Fuel pumps assy1.63.5
PERFORMANCE
104kW141 hp
**99.0kW135 hp
BORE
84.0 mm3.31 in
STROKE
61.0 mm2.4 in
DISPLACEMENT
1352 cm³82.6 cu in
FUEL*

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

iS: ASTM compliant | iSc: certified according to EASA CS-E

Downloads

C24 Product Sheet A4

C24 Brochure

Rotax Genuine Parts Flyer

Rotax Aircraft Engines Brochure

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