Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.70:1
|
| gptkbp:displacement |
360 cubic inches
|
| gptkbp:engineType |
air-cooled
horizontally opposed four-cylinder |
| gptkbp:fuelType |
100LL avgas
fuel injected |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:intendedUse |
gptkb:aircraft
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
200 hp
|
| gptkbp:propulsion |
constant-speed propeller
|
| gptkbp:usedIn |
gptkb:CAP_10
gptkb:Pitts_Special gptkb:Extra_300 |
| gptkbp:valveConfiguration |
overhead valve
|
| gptkbp:weight |
approx 295 lbs
|
| gptkbp:bfsParent |
gptkb:Zlín_Z-242
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming AEIO-360-A1B6
|