Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
3.00 inches
|
| gptkbp:certification |
Civil Aeronautics Administration Type Certificate E-165
|
| gptkbp:compressionRatio |
6.3:1
|
| gptkbp:configuration |
horizontally opposed
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
171 cubic inches
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1939
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental A-65-8 engine
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:powerOutput |
65 horsepower
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
3.625 inches
|
| gptkbp:usedIn |
gptkb:Aeronca_Champ
gptkb:Luscombe_8 gptkb:Piper_J-3_Cub gptkb:Taylorcraft_BC-12D |
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:weight |
approximately 170 lbs
|
| gptkbp:bfsParent |
gptkb:Aeronca_Champ
|
| gptkbp:bfsLayer |
7
|