Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
7.00:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:displacement |
320 cubic inches
|
| gptkbp:engineType |
horizontally opposed
four-cylinder |
| gptkbp:family |
Lycoming IO-320
|
| gptkbp:fuelType |
aviation gasoline
fuel-injected |
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming IO-320-B1A
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:powerOutput |
160 hp
|
| gptkbp:propulsion |
direct drive
|
| gptkbp:usedIn |
Piper Cherokee 140
Grumman American AA-5 Traveler |
| gptkbp:valveConfiguration |
overhead valve
|
| gptkbp:weight |
244 lbs
|
| gptkbp:bfsParent |
gptkb:Piper_PA-30_Twin_Comanche
gptkb:Piper_PA-39_Twin_Comanche_C/R |
| gptkbp:bfsLayer |
6
|