Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.25 in
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
520 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:family |
gptkb:Continental_IO-520
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
avgas
fuel-injected |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:powerOutput |
285 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
4.00 in
|
| gptkbp:usedIn |
gptkb:Cessna_210
gptkb:Beechcraft_Bonanza |
| gptkbp:weight |
approx 430 lbs
|
| gptkbp:bfsParent |
gptkb:Cessna_210
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-520-L
|