Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
4.06 in
|
| gptkbp:category |
gptkb:piston_engine
|
| gptkbp:certification |
FAA Type Certificate E-253
|
| gptkbp:compressionRatio |
7.0:1
|
| gptkbp:configuration |
naturally aspirated
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
201 cubic inches
|
| gptkbp:engineType |
air-cooled
horizontally opposed four-cylinder |
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
aviation gasoline
carbureted |
| gptkbp:ignition |
dual magneto
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:powerOutput |
100 hp
|
| gptkbp:stroke |
3.88 in
|
| gptkbp:successor |
Continental IO-240
|
| gptkbp:usedIn |
gptkb:Cessna_150
American Champion Citabria |
| gptkbp:variant |
O-200-A
O-200-B O-200-C O-200-D |
| gptkbp:weight |
170 lbs
|
| gptkbp:bfsParent |
gptkb:Auster_J/4_Archer
gptkb:Cessna_150 gptkb:VariEze gptkb:X-28 gptkb:Continental_Motors |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental O-200
|