Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:acrobaticOilSystem |
inverted oil system
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.7:1
|
| gptkbp:displacement |
541.5 cubic inches
|
| gptkbp:engineType |
air-cooled
horizontally opposed |
| gptkbp:family |
gptkb:Lycoming_O-540
|
| gptkbp:fuelType |
100LL avgas
fuel injected |
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming AEIO-540-D4A5
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
260 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:usedIn |
gptkb:Pitts_Special
gptkb:Extra_300 Christen Eagle II |
| gptkbp:weight |
389 lbs
|
| gptkbp:bfsParent |
gptkb:Slingsby_T-67_Firefly
|
| gptkbp:bfsLayer |
7
|