Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:Cessna_150 |
| gptkbp:bore |
4.06 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
7.0:1
|
| gptkbp:configuration |
horizontally opposed
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
201 cubic inches
|
| gptkbp:engineType |
four-cylinder
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
O-200A
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:powerOutput |
100 hp
|
| gptkbp:stroke |
3.88 in
|
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:weight |
170 lbs
|
| gptkbp:bfsParent |
gptkb:AD-1_Oblique_Wing
|
| gptkbp:bfsLayer |
7
|