Properties (44)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:application |
General aviation aircraft
|
| gptkbp:bore |
5.125 inches
|
| gptkbp:certifications |
FAA_certified
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:controls |
Throttle_control
|
| gptkbp:coolingSystem |
Air-cooled
|
| gptkbp:displacement |
550 cubic inches
|
| gptkbp:drivetrain |
Pushrod
|
| gptkbp:engine |
High reliability
Detailed specifications available Used in various aircraft models Air-cooled engine Aviation use Engine mount type IO-550 family |
| gptkbp:engineConfiguration |
Inline engine
|
| gptkbp:engineType |
Regular maintenance required
Reciprocating engine Multiple variants exist Optimized for performance Widely used in general aviation |
| gptkbp:exhaustSystem |
Dual exhaust
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuelType |
Aviation gasoline
Wet sump Fuel injection Dual magneto Champion_REM40E |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-550-U
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:marketSegment |
Light aircraft
|
| gptkbp:mayHave |
1,700 hours
|
| gptkbp:operationalHistory |
Developed in the late 1980s
|
| gptkbp:performance |
High performance
|
| gptkbp:performances |
2700 RPM
|
| gptkbp:powerOutput |
300 horsepower
|
| gptkbp:propulsion |
Constant speed propeller
|
| gptkbp:relatedPatent |
gptkb:Continental_IO-550-G
gptkb:Continental_IO-550-N |
| gptkbp:setting |
Horizontally_opposed
|
| gptkbp:stroke |
4.0 inches
|
| gptkbp:type |
Six-cylinder engine
|
| gptkbp:weight |
approximately 360 lbs
|