Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.25 in
|
| gptkbp:category |
general aviation engine
|
| 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:family |
gptkb:Continental_O-520_family
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
aviation gasoline
fuel injected |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental TSIO-520
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
285 to 375 hp
|
| gptkbp:stroke |
4.00 in
|
| gptkbp:turbocharged |
yes
|
| gptkbp:usedIn |
gptkb:Piper_Navajo
gptkb:Cessna_421 gptkb:Cessna_414 gptkb:Beechcraft_Baron |
| gptkbp:weight |
430 lbs
|
| gptkbp:bfsParent |
gptkb:Cessna_340
|
| gptkbp:bfsLayer |
6
|