Teledyne Continental IO-360ES
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
5.125 in
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:displacement |
360 cubic inches
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1990s
|
| gptkbp:fuelType |
aviation gasoline
fuel-injected |
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Teledyne_Continental_Motors
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
210 hp
|
| gptkbp:stroke |
3.875 in
|
| gptkbp:usedIn |
gptkb:Cirrus_SR20
|
| gptkbp:valvetrain |
overhead valve
|
| gptkbp:weight |
295 lb
|
| gptkbp:bfsParent |
gptkb:Ilyushin_Il-103
gptkb:Beriev_Be-103 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Teledyne Continental IO-360ES
|