ROTAX 915 iS

915 ISA / ISC A / IS C24 / ISC C24

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

ENGINE DATA

WEIGHT	kg	lb
Engine with propeller speed reduction gearbox i = 2,54 with overload clutch, turbocharger, intercooler, exhaust system	82.2	181.2
Engine suspension frame	2.0	4.4
External alternator	3.0	6.6
Air guide hood	0.4	0.8
Fuel pumps assy	1.6	3.5

BORE
84.0 mm	3.31 in

STROKE
61.0 mm	2.4 in

DISPLACEMENT
1352 cm³	82.6 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

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