About: Continental O-240

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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.

Attributes	Values
rdf:type	yago:WikicatBoxerEngines yago:WikicatContinentalAircraftEngines yago:AircraftEngine102687423 yago:Artifact100021939 yago:Device103183080 yago:Engine103287733 yago:Instrumentality103575240 yago:Machine103699975 yago:Motor103789946 yago:Object100002684 yago:PhysicalEntity100001930 yago:Whole100003553
rdfs:label	Continental O-240 (de) Continental O-240 (en)
rdfs:comment	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)
foaf:depiction
dcterms:subject	Continental aircraft engines 1970s aircraft piston engines Boxer engines
Wikipage page ID	20759661 (xsd:integer)
Wikipage revision ID	1094525761 (xsd:integer)
Link from a Wikipage to another Wikipage	Practavia Sprite Rolls-Royce Limited List of aircraft engines United Kingdom Liberty XL2 Light aircraft Continental O-360 Continental aircraft engines Continental IO-360 Continental O-200 Lycoming IO-233 Fuel injection Teledyne Continental Motors Cessna 150 Tri-R KIS TR-1 Warner Revolution II AESL Airtourer American Homebuilts John Doe Aircraft engine France Issoire APM 40 Simba Pusher configuration Reims Aviation 1970s aircraft piston engines Boxer engines Tractor configuration Diamond DA20 Avgas Piston St Croix Pietenpol Aerial Continental Motors, Inc. Roko Aero NG4 Rans S-16 Shekari Rutan Voyager FADEC Eagle Aircraft 150B Rollason Condor
sameAs	Continental O-240 Continental O-240 Continental O-240 Continental O-240 Continental O-240
specpower	0.520000 (xsd:double)
stroke	3.875 (inch)
valvetrain	One intake and one exhaust valve per cylinder (en)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Convert dbt:ISBN dbt:Refbegin dbt:Refend dbt:Reflist dbt:Short_description dbt:Infobox_aircraft_engine dbt:Pistonspecs dbt:Continental_aeroengines
thumbnail	wiki-commons:Special:FilePath/Teledyne_Continental_Motors_IO-240-B_Diamond_DA20-C1_C-GEQA.jpg?width=300
national origin	United States (en)
manufacturer	Teledyne Continental Motors
power	125 (xsd:integer)
ref	TYPE CERTIFICATE DATA SHEET NO. E7SO (en)
type	Aircraft engine Piston "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)
weight	255.0 (pound)
has abstract	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)
bore	4.438 (inch)
compression	8.500000 (xsd:double)
coolingsystem	Air-cooled (en)
developed from	Continental O-360
displacement	240.0 (cubicInch)
first run	1971 (xsd:integer)
fuelsystem	Aerosance FADEC system (en)
fueltype	100 (xsd:integer)
major applications	Liberty XL2 AESL Airtourer

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