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- Der Continental O-240 ist ein luftgekühlter Vierzylinderboxermotor, der vom US-amerikanischen Hersteller Continental Motors in den späten 1960er Jahren für den Einsatz in Leichtflugzeugen entwickelt wurde. Der Motor wurde am 7. Juli 1971 musterzugelassen. (de)
- The Continental O-240 engine is a four-cylinder, horizontally opposed, air-cooled aircraft engine that was developed in the late 1960s for use in light aircraft by Continental Motors, Inc. The first O-240 was certified on 7 July 1971. (en)
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- 6915 (xsd:nonNegativeInteger)
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- Aerosance FADEC system (en)
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- 1971 (xsd:integer)
- 1993 (xsd:integer)
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- TYPE CERTIFICATE DATA SHEET NO. E7SO (en)
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- dbr:Aircraft_engine
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- "4-cylinder, air-cooled, naturally aspirated, horizontally opposed, fuel-injected, spark ignition, four-stroke, direct drive. The engine incorporates a full authority digital electronic control system to control the ignition and fuel injection functions." (en)
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- One intake and one exhaust valve per cylinder (en)
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- Der Continental O-240 ist ein luftgekühlter Vierzylinderboxermotor, der vom US-amerikanischen Hersteller Continental Motors in den späten 1960er Jahren für den Einsatz in Leichtflugzeugen entwickelt wurde. Der Motor wurde am 7. Juli 1971 musterzugelassen. (de)
- The Continental O-240 engine is a four-cylinder, horizontally opposed, air-cooled aircraft engine that was developed in the late 1960s for use in light aircraft by Continental Motors, Inc. The first O-240 was certified on 7 July 1971. (en)
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- Continental O-240 (de)
- Continental O-240 (en)
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