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- Rotax_912 abstract "The Rotax 912 is a normally aspirated, air- and water-cooled, horizontally opposed four-cylinder, four-stroke, gear reduction-drive engine commonly used on certified aircraft, light sport aircraft, ultralight aircraft and unmanned aerial vehicles.".
- Rotax_912 thumbnail Rotax912SEngineInstallationMerlin.jpg?width=300.
- Rotax_912 wikiPageExternalLink E00051EN.pdf.
- Rotax_912 wikiPageExternalLink www.rotax-aircraft-engines.com.
- Rotax_912 wikiPageExternalLink 912Sinfo.pdf.
- Rotax_912 wikiPageExternalLink 912info.pdf.
- Rotax_912 wikiPageExternalLink 914info.pdf.
- Rotax_912 wikiPageID "4627435".
- Rotax_912 wikiPageRevisionID "605154131".
- Rotax_912 bore "79.5".
- Rotax_912 compression "9".
- Rotax_912 coolingsystem "Liquid-cooled cylinder heads, air-cooled cylinders".
- Rotax_912 displacement "1211.2".
- Rotax_912 fuelcon "15".
- Rotax_912 fueltype "Unleaded: 87 octane AKI / 90 octane RON or higher. Leaded fuel and AVGAS 100 LL can be used but are not recommended.".
- Rotax_912 hasPhotoCollection Rotax_912.
- Rotax_912 length "561.0".
- Rotax_912 lists "*List of aircraft engines".
- Rotax_912 majorApplications Light-sport_aircraft.
- Rotax_912 majorApplications Ultralight_aviation.
- Rotax_912 manufacturer Rotax.
- Rotax_912 nationalOrigin "Austria".
- Rotax_912 oilsystem "Dry sump with trochoid pump, camshaft driven".
- Rotax_912 power "at 5,800 rpm".
- Rotax_912 weight "980".
- Rotax_912 similarEngines "*Arrow 1000 * D-Motor *Hirth 3701 *Hirth F-30 *HKS 700E *Jabiru 2200 *KFM 112M *Pegasus PAL 95 *Revmaster R-2300 *Sauer S 2200 UL *Sauer S 2100 ULT *Sauer S 2400 UL *ULPower UL260i *".
- Rotax_912 specfuelcon "285".
- Rotax_912 specpower "48.71".
- Rotax_912 stroke "61.0".
- Rotax_912 type Aircraft_engine.
- Rotax_912 type Piston.
- Rotax_912 type "four-cylinder, four-stroke liquid / air-cooled engine with opposed cylinders, dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet, dual CD carburetors, mechanical diaphragm pump, electronic dual ignition, electric starter, integrated reduction gear 1 : 2.273 or 1 : 2.43".
- Rotax_912 valvetrain "OHV, hydraulic lifters, pushrods, rocker arms".
- Rotax_912 variantsWithTheirOwnArticles Rotax_914.
- Rotax_912 weight "60".
- Rotax_912 width "576.0".
- Rotax_912 subject Category:Aircraft_piston_engines_1980–1989.
- Rotax_912 subject Category:Boxer_engines.
- Rotax_912 subject Category:Rotax_engines.
- Rotax_912 comment "The Rotax 912 is a normally aspirated, air- and water-cooled, horizontally opposed four-cylinder, four-stroke, gear reduction-drive engine commonly used on certified aircraft, light sport aircraft, ultralight aircraft and unmanned aerial vehicles.".
- Rotax_912 label "Rotax 912".
- Rotax_912 label "Rotax 912".
- Rotax_912 label "Rotax 912".
- Rotax_912 label "Rotax 912".
- Rotax_912 label "Rotax 912".
- Rotax_912 label "Rotax 912".
- Rotax_912 sameAs Rotax_912.
- Rotax_912 sameAs Rotax_912.
- Rotax_912 sameAs Rotax_912.
- Rotax_912 sameAs Rotax_912.
- Rotax_912 sameAs m.0cdcxj.
- Rotax_912 sameAs Q2005638.
- Rotax_912 sameAs Q2005638.
- Rotax_912 wasDerivedFrom Rotax_912?oldid=605154131.
- Rotax_912 depiction Rotax912SEngineInstallationMerlin.jpg.
- Rotax_912 homepage www.rotax-aircraft-engines.com.
- Rotax_912 isPrimaryTopicOf Rotax_912.
