Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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 |
| 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 |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-520 series
|