Statements (61)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Cessna_195_A
gptkb:IO-540 |
| gptkbp:application |
general aviation aircraft
|
| gptkbp:ceo |
1,700 hours
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compression_ratio |
8.5:1
|
| gptkbp:controls |
throttle control
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
550 cubic inches
9.0 liters |
| gptkbp:engine |
inline
boxer engine engine mount type IO series |
| gptkbp:engine_type |
gptkb:IO-550-B
gptkb:IO-550-G reciprocating engine IO-550-U IO-550-N IO-550-C IO-550-D IO-550-E IO-550-F IO-550-H IO-550-J IO-550-K IO-550-L IO-550-M IO-550-P IO-550-R IO-550-S IO-550-T IO-550-V IO-550-W IO-550-X IO-550-Y IO-550-Z IO-550-Q |
| gptkbp:first_introduced |
1990s
|
| gptkbp:fuel_capacity |
8 quarts
|
| gptkbp:fuel_type |
aviation gasoline
mechanical fuel pump |
| https://www.w3.org/2000/01/rdf-schema#label |
IO-550
|
| gptkbp:ignition_system |
dual ignition
Champion RE M40 E |
| gptkbp:is_often_used_in |
gptkb:aircraft
gptkb:Beechcraft_Bonanza gptkb:Piper_PA-46 |
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:Teledyne_Continental_Motors
|
| gptkbp:power_output |
300 horsepower
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:setting |
horizontally opposed
|
| gptkbp:successor |
IO-550-N
|
| gptkbp:torque |
300 lb-ft
|
| gptkbp:type |
six-cylinder engine
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:water_source |
up to 20 gallons per hour
|
| gptkbp:weight |
approximately 300 pounds
|