Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
general aviation aircraft
|
| gptkbp:bore |
5.125 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.70:1
|
| gptkbp:configuration |
direct-drive
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
360 cubic inches
|
| gptkbp:engineType |
horizontally opposed
four-cylinder |
| gptkbp:family |
gptkb:Lycoming_IO-360_series
|
| gptkbp:fuelType |
fuel-injected
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:notableAircraft |
gptkb:Beechcraft_Musketeer
gptkb:Piper_Arrow |
| gptkbp:powerOutput |
200 horsepower
|
| gptkbp:propulsion |
constant-speed
|
| gptkbp:stroke |
4.375 in
|
| gptkbp:weight |
285 lbs
|
| gptkbp:bfsParent |
gptkb:Lycoming_IO-360
gptkb:Textron_Lycoming_IO-360 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
IO-360-A1A
|