Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
5.25 inches
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:configuration |
flat-six
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:directDrive |
yes
|
| gptkbp:displacement |
552 cubic inches
|
| gptkbp:engineType |
piston engine
|
| gptkbp:family |
gptkb:Continental_550_series
|
| gptkbp:firstFlight |
1983
|
| gptkbp:fuelType |
100LL avgas
fuel-injected |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-550
|
| gptkbp:ignition |
dual magnetos
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:numberOfEngines |
6
|
| gptkbp:powerOutput |
280 to 360 horsepower
|
| gptkbp:propulsion |
constant-speed propeller
|
| gptkbp:stroke |
4.00 inches
|
| gptkbp:usedIn |
gptkb:Mooney_M20
gptkb:Cessna_206 gptkb:Cessna_210 gptkb:Cirrus_SR22 gptkb:Beechcraft_Bonanza |
| gptkbp:weight |
approx. 430 lbs
|
| gptkbp:bfsParent |
gptkb:Beechcraft_Baron
gptkb:Beechcraft_Baron_58 |
| gptkbp:bfsLayer |
6
|