Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
3.00 inches
|
| gptkbp:certification |
gptkb:Civil_Aeronautics_Administration
|
| gptkbp:compressionRatio |
6.3:1
|
| gptkbp:configuration |
horizontally opposed
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
171 cubic inches
|
| gptkbp:engineType |
piston engine
|
| gptkbp:firstFlight |
1939
|
| gptkbp:fuelType |
carbureted
|
| https://www.w3.org/2000/01/rdf-schema#label |
Continental A-65
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:powerOutput |
65 horsepower
|
| gptkbp:stroke |
3.625 inches
|
| gptkbp:successor |
gptkb:Continental_C-85
|
| gptkbp:usedIn |
gptkb:Aeronca_Champ
gptkb:Taylorcraft_BC-12 gptkb:Piper_J-3_Cub |
| gptkbp:weight |
170 lbs (dry)
|
| gptkbp:bfsParent |
gptkb:Aeronca_Chief
gptkb:Aeronca_Defender gptkb:Continental_Motors gptkb:Piper_Cub gptkb:Piper_PA-2_Cub_Coupe gptkb:Piper_PA-4_Cub_Coupe |
| gptkbp:bfsLayer |
7
|