Statements (64)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:aircraft_operated |
gptkb:Beechcraft_Bonanza
gptkb:Mooney_M20 gptkb:Piper_PA-46 gptkb:Cessna_182 |
| gptkbp:application |
General aviation aircraft
|
| gptkbp:ceo |
1800 hours
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compression_ratio |
8.5:1
|
| gptkbp:configuration |
6-cylinder
|
| gptkbp:control_system |
Electronic engine control
|
| gptkbp:cooling_system |
Air-cooled
Air-cooled engine |
| gptkbp:displacement |
550 cubic inches
|
| gptkbp:enforces |
Meets aviation regulations
|
| gptkbp:engine |
Active user community
Used in various applications Electric start Innovative engineering solutions Developed in the 1990s Manufacturer support available Used in various aircraft models Fuel efficiency features Available aftermarket parts IO-500 series Comprehensive documentation provided Advanced features for efficiency High output for its class |
| gptkbp:engine_awards |
Awards for design excellence
|
| gptkbp:engine_configuration |
Inline engine
Positive reviews from users Detailed specifications available Modern design principles Engine mount type |
| gptkbp:engine_performance_data |
Performance data published
|
| gptkbp:engine_power |
Reliable performance
Known for reliability Popular among general aviation pilots |
| gptkbp:engine_type |
Compatible with various aircraft systems
Fuel-injected Variants available |
| gptkbp:first_introduced |
1990s
|
| gptkbp:fuel_capacity |
Wet sump
|
| gptkbp:fuel_type |
gptkb:Avgas
Fuel injection system |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental IO-550
|
| gptkbp:ignition_system |
Dual ignition
|
| gptkbp:is_tested_for |
Extensively tested before release
|
| gptkbp:maintenance |
Regular maintenance required
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:market_segment |
Light aircraft
|
| gptkbp:number_of_engines |
Horizontally opposed
|
| gptkbp:performance |
High performance
|
| gptkbp:power_output |
300 horsepower
|
| gptkbp:propeller |
Constant speed propeller
|
| gptkbp:service_entry |
1990s
|
| gptkbp:training |
Training available for mechanics
|
| gptkbp:type |
Horizontally opposed engine
|
| gptkbp:valve_configuration |
Overhead valve
|
| gptkbp:weight |
approximately 360 lbs
|
| gptkbp:bfsParent |
gptkb:T-34_Mentor
gptkb:Beechcraft_Baron gptkb:Cessna_206_H |
| gptkbp:bfsLayer |
5
|