Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.25 in
|
| gptkbp:certification |
FAA certified
|
| 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 |
piston engine
|
| gptkbp:firstFlight |
1970s
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental TSIO-520-VB
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:inductionSystem |
turbocharged
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:powerOutput |
310 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
4.00 in
|
| gptkbp:usedIn |
gptkb:Cessna_414A_Chancellor
gptkb:Cessna_421C_Golden_Eagle |
| gptkbp:weight |
approx 430 lbs
|
| gptkbp:bfsParent |
gptkb:Cessna_402
|
| gptkbp:bfsLayer |
6
|