Statements (34)
Predicate | Object |
---|---|
gptkbp:instanceOf |
aircraft engine family
|
gptkbp:bore |
5.25 in
|
gptkbp:category |
piston aircraft engine
|
gptkbp:certification |
gptkb:FAA
|
gptkbp:compressionRatio |
8.5:1
7.5:1 |
gptkbp:configuration |
flat-six
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:displacement |
520 cubic inches
|
gptkbp:fuelType |
avgas
fuel-injected |
https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-520 series
|
gptkbp:ignition |
dual magnetos
|
gptkbp:introducedIn |
1964
|
gptkbp:manufacturer |
gptkb:Continental_Motors
|
gptkbp:numberOfEngines |
6
|
gptkbp:powerOutput |
300 hp
285 hp |
gptkbp:primaryUse |
general aviation
|
gptkbp:relatedTo |
Continental IO-550 series
Continental IO-470 series |
gptkbp:stroke |
4.00 in
|
gptkbp:superchargedVariant |
TSIO-520
|
gptkbp:turbochargedVariant |
TSIO-520
|
gptkbp:usedIn |
gptkb:Cessna_206
gptkb:Cessna_210 gptkb:Cessna_310 gptkb:Beechcraft_Baron gptkb:Beechcraft_Bonanza gptkb:Cessna_185 |
gptkbp:valvetrain |
overhead valve
|
gptkbp:weight |
406 lb
|
gptkbp:bfsParent |
gptkb:Continental_IO-520-D
|
gptkbp:bfsLayer |
7
|