Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
4.875 in
|
| gptkbp:compressionRatio |
7.5:1
6.5:1 |
| gptkbp:configuration |
horizontally opposed
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
290 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1942
|
| gptkbp:fuelType |
aviation gasoline
carbureted |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:numberOfEngines |
4
|
| gptkbp:powerOutput |
125 hp to 140 hp
|
| gptkbp:status |
out of production
|
| gptkbp:stroke |
3.125 in
|
| gptkbp:usedIn |
gptkb:Cessna_170
gptkb:Stinson_108 gptkb:Piper_PA-18_Super_Cub |
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:variant |
O-290-A
O-290-B O-290-C O-290-D O-290-G |
| gptkbp:weight |
244 lb
|
| gptkbp:bfsParent |
gptkb:Lycoming_Engines
gptkb:Lycoming_aircraft_engines gptkb:Piper_PA-20_Pacer |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming O-290
|