Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
general aviation aircraft
|
| gptkbp:bore |
5.125 inches
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:configuration |
flat-four
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
360 cubic inches
|
| gptkbp:engineType |
air-cooled
horizontally opposed four-cylinder |
| gptkbp:family |
gptkb:Lycoming_O-360_family
|
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
avgas
fuel injected |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Textron
gptkb:Lycoming_Engines |
| gptkbp:powerOutput |
180 to 200 horsepower
|
| gptkbp:stroke |
4.375 inches
|
| gptkbp:usedIn |
gptkb:Cessna_172
gptkb:Mooney_M20J gptkb:Beechcraft_Musketeer gptkb:Piper_Arrow Grumman American AA-5B Tiger |
| gptkbp:variant |
gptkb:IO-360-A1A
IO-360-C1C IO-360-B1B |
| gptkbp:weight |
approx 285 lbs (dry)
|
| gptkbp:bfsParent |
gptkb:Zeppelin_NT
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Textron Lycoming IO-360
|