Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_172S
|
| gptkbp:bore |
5.125 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:configuration |
horizontally opposed
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
360 cubic inches
|
| gptkbp:engineType |
four-cylinder
|
| gptkbp:family |
gptkb:Lycoming_IO-360_series
|
| gptkbp:firstFlight |
1996
|
| gptkbp:fuelType |
100LL avgas
fuel injected |
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming IO-360-L2A
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
180 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
4.375 in
|
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:weight |
285 lbs
|
| gptkbp:bfsParent |
gptkb:Cessna_172SP_Skyhawk
gptkb:Textron_Aviation_Cessna_172_Skyhawk gptkb:Cessna_172_Skyhawk |
| gptkbp:bfsLayer |
6
|