Statements (64)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:General_Aviation_Aircraft
|
| gptkbp:bore |
5.125 inches
|
| gptkbp:ceo |
1800 hours
|
| gptkbp:certification |
FAA Certified
|
| gptkbp:compression_ratio |
8.5:1
|
| gptkbp:configuration |
6-cylinder
|
| gptkbp:control_system |
Electronic Engine Control
Electronic Ignition |
| gptkbp:cooling_system |
Air-cooled
Efficient Cooling System Air Cooled |
| gptkbp:displacement |
550 cubic inches
|
| gptkbp:durability |
Durable Engine Construction
|
| gptkbp:engine |
Active User Community
High Power-to-Weight Ratio Various Aircraft Models Developed in the 1990s Consistent Power Output Strong Manufacturer Support Easy to Service Advanced Engine Technology Available Upgrades |
| gptkbp:engine_configuration |
Inline Engine
Positive User Reviews Detailed Specifications Available Modern Engine Design |
| gptkbp:engine_power |
Optimized for Performance
Good Fuel Efficiency Fuel Efficient Engine High Reliability Engine Long Life Engine Widely Used in Aviation |
| gptkbp:engine_type |
Reciprocating Engine
Compatible with Various Aircraft Multiple Variants Available |
| gptkbp:exhaust_system |
Dual Exhaust
Dual Intake |
| gptkbp:first_flight |
1990s
|
| gptkbp:fuel_capacity |
12 quarts
|
| gptkbp:fuel_type |
gptkb:Av_Gas
Fuel Injection |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-550-N
|
| gptkbp:ignition_system |
gptkb:Champion_REM40_E
Dual Magneto |
| gptkbp:is_often_used_in |
Piston Aircraft
|
| gptkbp:maintenance |
Regular Maintenance Required
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:mounting_options |
Engine Mount
|
| gptkbp:noise_level |
Moderate Noise Levels
Low Vibration Engine |
| gptkbp:performance |
High Performance Engine
|
| gptkbp:power_output |
300 horsepower
|
| gptkbp:propeller |
Variable Pitch Propeller
|
| gptkbp:related_model |
gptkb:IO-550-B
gptkb:IO-550-G IO-550-U |
| gptkbp:stroke |
4.0 inches
|
| gptkbp:torque |
High Torque Output
|
| gptkbp:type |
gptkb:Horizontally_Opposed_Engine
|
| gptkbp:valve_configuration |
Pushrod
|
| gptkbp:weight |
approximately 360 lbs
|
| gptkbp:bfsParent |
gptkb:Cirrus_SR22
|
| gptkbp:bfsLayer |
5
|