Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.0 in
|
| gptkbp:category |
gptkb:aircraft_piston_engine
|
| gptkbp:compressionRatio |
7.0:1
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
470 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:ignition |
dual magneto
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
213 hp
|
| gptkbp:stroke |
4.0 in
|
| gptkbp:usedIn |
gptkb:Cessna_310
gptkb:Cessna_182 gptkb:Cessna_180 |
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:weight |
393 lb
|
| gptkbp:bfsParent |
gptkb:U-3A
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental O-470-M
|