Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.125 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
361 cubic inches
|
| gptkbp:engineType |
horizontally opposed
four-cylinder |
| gptkbp:family |
gptkb:Lycoming_O-360_series
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
avgas
carbureted |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
180 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
4.375 in
|
| gptkbp:usedIn |
gptkb:Cessna_172
gptkb:Piper_Cherokee gptkb:Beechcraft_Musketeer |
| gptkbp:valveConfiguration |
overhead valve
|
| gptkbp:weight |
258 lbs
|
| gptkbp:bfsParent |
gptkb:Valmet_L-70_Vinka
gptkb:Beechcraft_Model_95_Travel_Air |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming O-360-A1A
|