An Entity of Type: Light-sport aircraft, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

The Bushcaddy R-80 is a Canadian ultralight and light-sport aircraft that was designed by Jean Eudes Potvin of Lac Saint-Jean, Quebec in 1994 and produced by his company Club Aeronautique Delisle Incorporated (CADI). It was later built by Canadian Light Aircraft Sales and Service (CLASS) of St. Lazare, Quebec and later Les Cedres, Quebec and now Bushcaddy of Lachute, Quebec. The R-80 designation indicates that the aircraft was originally designed for a Rotax engine of 80 hp (60 kW). The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.

Property Value
dbo:abstract
  • The Bushcaddy R-80 is a Canadian ultralight and light-sport aircraft that was designed by Jean Eudes Potvin of Lac Saint-Jean, Quebec in 1994 and produced by his company Club Aeronautique Delisle Incorporated (CADI). It was later built by Canadian Light Aircraft Sales and Service (CLASS) of St. Lazare, Quebec and later Les Cedres, Quebec and now Bushcaddy of Lachute, Quebec. The R-80 designation indicates that the aircraft was originally designed for a Rotax engine of 80 hp (60 kW). The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft. (en)
dbo:manufacturer
dbo:numberBuilt
  • 80 (xsd:nonNegativeInteger)
dbo:origin
dbo:productionStartYear
  • 1994-01-01 (xsd:gYear)
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dbo:type
dbo:wikiPageExternalLink
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  • 35875493 (xsd:integer)
dbo:wikiPageLength
  • 9111 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1065457265 (xsd:integer)
dbo:wikiPageWikiLink
dbp:airfoil
  • NACA 4413 (en)
dbp:capacity
  • one passenger (en)
dbp:ceilingFt
  • 16000 (xsd:integer)
dbp:climbRateFtmin
  • 800 (xsd:integer)
dbp:crew
  • one (en)
dbp:cruiseSpeedMph
  • 105 (xsd:integer)
dbp:cruiseSpeedNote
  • at 75% power (en)
dbp:designer
  • Jean Eudes Potvin (en)
dbp:emptyWeightLb
  • 710 (xsd:integer)
dbp:eng1Hp
  • 100 (xsd:integer)
dbp:eng1Name
dbp:eng1Number
  • 1 (xsd:integer)
dbp:eng1Type
  • four cylinder, liquid and air-cooled, four stroke aircraft engine (en)
dbp:gLimits
  • +5.7/-3.8 (en)
dbp:grossWeightLb
  • 1320 (xsd:integer)
dbp:grossWeightNote
  • (en)
dbp:introduced
  • 1994 (xsd:integer)
dbp:lengthFt
  • 22 (xsd:integer)
dbp:lengthIn
  • 1 (xsd:integer)
dbp:manufacturer
dbp:nationalOrigin
dbp:neverExceedSpeedMph
  • 120 (xsd:integer)
dbp:numberBuilt
  • 80 (xsd:integer)
dbp:primeUnits?_
  • imp (en)
dbp:produced
  • 1994 (xsd:integer)
dbp:ref
  • Bayerl and Bushcaddy (en)
dbp:spanFt
  • 32 (xsd:integer)
dbp:stallSpeedMph
  • 34 (xsd:integer)
dbp:status
  • In production (en)
dbp:type
  • Ultralight aircraft and Light-sport aircraft (en)
dbp:wikiPageUsesTemplate
dbp:wingAreaSqm
  • 15.600000 (xsd:double)
dbp:wingLoadingLb/sqft
  • 8.900000 (xsd:double)
dcterms:subject
gold:hypernym
rdf:type
rdfs:comment
  • The Bushcaddy R-80 is a Canadian ultralight and light-sport aircraft that was designed by Jean Eudes Potvin of Lac Saint-Jean, Quebec in 1994 and produced by his company Club Aeronautique Delisle Incorporated (CADI). It was later built by Canadian Light Aircraft Sales and Service (CLASS) of St. Lazare, Quebec and later Les Cedres, Quebec and now Bushcaddy of Lachute, Quebec. The R-80 designation indicates that the aircraft was originally designed for a Rotax engine of 80 hp (60 kW). The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft. (en)
rdfs:label
  • Bushcaddy R-80 (en)
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