Teledyne Continental IO-360ES
GPTKB entity
Statements (23)
Predicate | Object |
---|---|
gptkbp:instanceOf |
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 |
piston engine
|
gptkbp:firstFlight |
1990s
|
gptkbp:fuelType |
aviation gasoline
fuel-injected |
https://www.w3.org/2000/01/rdf-schema#label |
Teledyne Continental IO-360ES
|
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
|
gptkbp:bfsLayer |
6
|