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- Rotax_447 abstract "The Rotax 447 is a 41.6 hp (31 kW), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft.".
- Rotax_447 wikiPageID "21892451".
- Rotax_447 wikiPageRevisionID "605514210".
- Rotax_447 bore "67.5".
- Rotax_447 compression "9.6".
- Rotax_447 coolingsystem "fan or free air".
- Rotax_447 displacement "426.5".
- Rotax_447 fuelcon "11".
- Rotax_447 fuelsystem "pneumatic pump pressurized".
- Rotax_447 fueltype "regular autofuel".
- Rotax_447 hasPhotoCollection Rotax_447.
- Rotax_447 majorApplications Quad_City_Challenger.
- Rotax_447 manufacturer Rotax.
- Rotax_447 nationalOrigin Austria.
- Rotax_447 oilsystem "premixed in the fuel at 50:1 or oil injection".
- Rotax_447 power "at 6800 rpm".
- Rotax_447 weight "1.12".
- Rotax_447 reductionGear "Rotax 'B' gearbox: 2.00, 2.24, 2.58 ratios".
- Rotax_447 ref "OPERATORS MANUAL FOR ENGINE TYPES 447, 503 & 582".
- Rotax_447 stroke "61.0".
- Rotax_447 type Aircraft_engine.
- Rotax_447 type Piston.
- Rotax_447 type "two-stroke air-cooled aeroengine".
- Rotax_447 valvetrain "piston ports".
- Rotax_447 weight "26.8".
- Rotax_447 subject Category:Air-cooled_aircraft_piston_engines.
- Rotax_447 subject Category:Rotax_engines.
- Rotax_447 subject Category:Two-stroke_aircraft_piston_engines.
- Rotax_447 comment "The Rotax 447 is a 41.6 hp (31 kW), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft.".
- Rotax_447 label "Rotax 447".
- Rotax_447 sameAs m.05p45_f.
- Rotax_447 sameAs Q7370341.
- Rotax_447 sameAs Q7370341.
- Rotax_447 wasDerivedFrom Rotax_447?oldid=605514210.
- Rotax_447 isPrimaryTopicOf Rotax_447.