Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.125 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
7.0:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
320 cubic inches
|
| gptkbp:engineType |
horizontally opposed
four-cylinder |
| gptkbp:family |
Lycoming O-320 series
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
aviation gasoline
carbureted |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
150 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
3.875 in
|
| gptkbp:usedIn |
gptkb:Cessna_172
|
| gptkbp:valveConfiguration |
overhead valve
|
| gptkbp:weight |
244 lbs
|
| gptkbp:bfsParent |
gptkb:Cessna_172L
gptkb:Cessna_172M |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming O-320-E2D
|