Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.125 in
|
| gptkbp:certification |
FAA Type Certificate 1E12
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
320 cubic inches
|
| gptkbp:engineType |
horizontally opposed
four-cylinder |
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming O-320-H2AD
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:introducedIn |
1977
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:notableFeature |
unique camshaft and lifter design
|
| gptkbp:numberOfIssues |
premature cam and lifter wear
|
| gptkbp:powerOutput |
160 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:stroke |
3.875 in
|
| gptkbp:usedIn |
gptkb:Cessna_172N
|
| gptkbp:valveConfiguration |
overhead valve
|
| gptkbp:weight |
244 lbs
|
| gptkbp:bfsParent |
gptkb:Cessna_172N
|
| gptkbp:bfsLayer |
7
|