Statements (53)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
engine
|
| gptkbp:accessories |
alternator
fuel pump oil pump magnetos starter motor |
| gptkbp:application |
gptkb:Cessna_172
gptkb:Piper_PA-28 Beechcraft Bonanza |
| gptkbp:bore |
5.125 inches
|
| gptkbp:compressionRatio |
8.5:1
|
| gptkbp:controls |
throttle control
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:cylinderCount |
6
|
| gptkbp:displacement |
540 cubic inches
|
| gptkbp:drivetrain |
overhead valve
|
| gptkbp:engine |
front-mounted
|
| gptkbp:engineType |
O-540-U1A
O-540-U2A O-540-U2B O-540-U4A O-540-U5A O-540-U8A O-540-U3A O-540-U6A O-540-U7A O-540-U9A |
| gptkbp:exhaustSystem |
dual exhaust
|
| gptkbp:fuel_capacity |
8 quarts
|
| gptkbp:fuelType |
aviation gasoline
carbureted dual ignition Champion_REM40E |
| https://www.w3.org/2000/01/rdf-schema#label |
O-540-U engine
|
| gptkbp:introduced |
1950s
|
| gptkbp:is_used_in |
general aviation aircraft
|
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
Lycoming
|
| gptkbp:market_segment |
private aircraft
light aircraft training aircraft |
| gptkbp:mayHave |
1800 hours
|
| gptkbp:performance |
smooth operation
high reliability good fuel efficiency |
| gptkbp:powerOutput |
250 horsepower
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:regulatoryCompliance |
FAA_certified
|
| gptkbp:related_engine |
Lycoming O-540
|
| gptkbp:setting |
V-type engine
|
| gptkbp:stroke |
4.00 inches
|
| gptkbp:type |
reciprocating engine
|
| gptkbp:weight |
approximately 300 lbs
|