Properties (48)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:application |
general aviation aircraft
|
| gptkbp:bore |
5.125 inches
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:controls |
throttle control
|
| gptkbp:coolingSystem |
air-cooled
air-cooled design integrated cooling fins |
| gptkbp:cylinderCount |
6
|
| gptkbp:displacement |
540 cubic inches
|
| gptkbp:drivetrain |
overhead valves
|
| gptkbp:engine |
inline engine
used in various aircraft models O-540-J |
| gptkbp:engineConfiguration |
mechanical fuel pump
|
| gptkbp:engineType |
high power-to-weight ratio
multiple variants available horizontally opposed engine |
| gptkbp:exhaustSystem |
exhaust stacks
|
| gptkbp:fuel_capacity |
12 quarts
12-15 gallons per hour |
| gptkbp:fuelCapacity |
not applicable
|
| gptkbp:fuelType |
aviation gasoline
carbureted dual ignition Champion RHM-40 |
| gptkbp:hasArea |
extensively tested for performance
FAA_certified_engine |
| https://www.w3.org/2000/01/rdf-schema#label |
O-540-J engine
|
| gptkbp:introduced |
1960s
|
| gptkbp:lensType |
engine_mount
|
| gptkbp:maintenance |
regular inspections required
|
| gptkbp:manufacturer |
Lycoming
|
| gptkbp:mayHave |
2000 hours
|
| gptkbp:operationalHistory |
long history in aviation
|
| gptkbp:operationalRange |
2000 to 2700 RPM
|
| gptkbp:performance |
high reliability
|
| gptkbp:performances |
detailed specifications available
proven track record major overhaul required at TBO |
| gptkbp:powers |
250 horsepower
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:related_engine |
Lycoming O series
O-540 series |
| gptkbp:setting |
V-type engine
|
| gptkbp:stroke |
4.00 inches
|
| gptkbp:type |
reciprocating engine
|
| gptkbp:weight |
approximately 300 lbs
|