Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:aspiration |
normally aspirated
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
541.5 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:family |
gptkb:Lycoming_O-540
|
| gptkbp:features |
fuel injection
dual magnetos inverted oil system |
| gptkbp:firstFlight |
1960s
|
| gptkbp:fuelType |
avgas
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
260 hp
|
| gptkbp:usedIn |
gptkb:Pitts_Model_12
gptkb:Extra_300 |
| gptkbp:bfsParent |
gptkb:Pacific_Aerospace_CT-4E_Airtrainer
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming AEIO-540-L1B5D
|