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- Rotax_277 abstract "The Rotax 277 is a 26 hp (19 kW), single-cylinder, two-stroke aircraft engine, that was built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft.".
- Rotax_277 wikiPageID "21975436".
- Rotax_277 wikiPageRevisionID "587032108".
- Rotax_277 bore "72.0".
- Rotax_277 compression "Theoretical 11.8, effective 6.7".
- Rotax_277 coolingsystem "fan or free air".
- Rotax_277 displacement "268.7".
- Rotax_277 fuelsystem "pneumatic pump pressurized".
- Rotax_277 fueltype "premium unleaded autofuel".
- Rotax_277 hasPhotoCollection Rotax_277.
- Rotax_277 majorApplications Ultralight_aviation.
- Rotax_277 manufacturer Rotax.
- Rotax_277 nationalOrigin Austria.
- Rotax_277 oilsystem "premixed in the fuel at 50:1".
- Rotax_277 power "19".
- Rotax_277 weight "0.64".
- Rotax_277 ref "ROTAX 277 UL Data Sheet".
- Rotax_277 seeAlso "*Hirth F-30 *KFM 107".
- Rotax_277 stroke "66.0".
- Rotax_277 type Aircraft_engine.
- Rotax_277 type Piston.
- Rotax_277 type "two-stroke air-cooled aeroengine".
- Rotax_277 valvetrain "piston ports".
- Rotax_277 weight "29.5".
- Rotax_277 subject Category:Air-cooled_aircraft_piston_engines.
- Rotax_277 subject Category:Rotax_engines.
- Rotax_277 subject Category:Two-stroke_aircraft_piston_engines.
- Rotax_277 comment "The Rotax 277 is a 26 hp (19 kW), single-cylinder, two-stroke aircraft engine, that was built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft.".
- Rotax_277 label "Rotax 277".
- Rotax_277 sameAs m.05pch_y.
- Rotax_277 sameAs Q7370338.
- Rotax_277 sameAs Q7370338.
- Rotax_277 wasDerivedFrom Rotax_277?oldid=587032108.
- Rotax_277 isPrimaryTopicOf Rotax_277.