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- Hirth_F-30 abstract "The Hirth F-30 is a horizontally opposed four-cylinder, two-stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft and homebuilts.".
- Hirth_F-30 wikiPageID "25480504".
- Hirth_F-30 wikiPageRevisionID "571270545".
- Hirth_F-30 compression "9.5".
- Hirth_F-30 coolingsystem "free air or fan".
- Hirth_F-30 displacement "1042.0".
- Hirth_F-30 fuelsystem "Fuel injection".
- Hirth_F-30 fueltype Avgas.
- Hirth_F-30 hasPhotoCollection Hirth_F-30.
- Hirth_F-30 manufacturer Hirth.
- Hirth_F-30 nationalOrigin Germany.
- Hirth_F-30 oilsystem "50".
- Hirth_F-30 power "at 6200 rpm with free-air cooling, at 6200 rpm with fan cooling".
- Hirth_F-30 reductionGear "G-40 gearbox with reduction ratios of 2.03:1, 2.25:1, 2.64:1, 2.96:1 and 3.33:1 available. Optional centrifugal clutch.".
- Hirth_F-30 ref "Recreational Power Engineering".
- Hirth_F-30 seeAlso "*2si 808 *Arrow 1000 *Rotax 912".
- Hirth_F-30 type "Four-cylinder two-stroke aircraft engine".
- Hirth_F-30 type "Four-cylinder, two-stroke, horizontally opposed, aircraft engine".
- Hirth_F-30 unitCost "US$8049".
- Hirth_F-30 weight ", including starter and exhaust system, with gearbox, exhaust system and electric start. Fan cooling adds".
- Hirth_F-30 subject Category:Air-cooled_aircraft_piston_engines.
- Hirth_F-30 subject Category:Two-stroke_aircraft_piston_engines.
- Hirth_F-30 comment "The Hirth F-30 is a horizontally opposed four-cylinder, two-stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft and homebuilts.".
- Hirth_F-30 label "Hirth F-30".
- Hirth_F-30 sameAs m.09rt4zx.
- Hirth_F-30 sameAs Q5771747.
- Hirth_F-30 sameAs Q5771747.
- Hirth_F-30 wasDerivedFrom Hirth_F-30?oldid=571270545.
- Hirth_F-30 isPrimaryTopicOf Hirth_F-30.