Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
7.5:1
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
520 cubic inches
|
| gptkbp:engineType |
turbocharged
|
| gptkbp:family |
gptkb:Continental_O-520_family
|
| gptkbp:fuelType |
aviation gasoline
fuel injection |
| gptkbp:ignition |
dual magneto
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:powerOutput |
310 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:usedIn |
gptkb:Cessna_414A_Chancellor
|
| gptkbp:bfsParent |
gptkb:Piper_PA-46_Malibu
|
| gptkbp:bfsLayer |
7
|
| http://www.w3.org/2000/01/rdf-schema#label |
Continental TSIO-520-BE
|