Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.25 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
520 cubic inches
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
avgas
fuel injected |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-520-C
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:powerOutput |
285 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
4.00 in
|
| gptkbp:usedInAircraft |
gptkb:Cessna_210
gptkb:Beechcraft_Baron gptkb:Beechcraft_Bonanza |
| gptkbp:weight |
406 lbs
|
| gptkbp:bfsParent |
gptkb:Beechcraft_Model_58_Baron
gptkb:Beechcraft_Model_58 |
| gptkbp:bfsLayer |
6
|