Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:Cessna_180
gptkb:Mooney_M20 gptkb:Piper_PA-24_Comanche gptkb:Beechcraft_Musketeer |
| gptkbp:bore |
5.125 inches
|
| gptkbp:ceo |
1800 hours
|
| gptkbp:compression_ratio |
8.5:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
435 cubic inches
|
| gptkbp:engine |
gptkb:Lycoming_O-series
smooth operation four-stroke high power-to-weight ratio easy installation low noise levels reliable performance inline engine long service life low vibration levels versatile applications dual ignition system robust construction low maintenance requirements good fuel efficiency overhead valve design good acceleration good altitude performance proven reliability good throttle response O-400 series constant speed propeller capability horizontally opposed design |
| gptkbp:engine_type |
reciprocating engine
|
| gptkbp:first_introduced |
1950s
|
| gptkbp:fuel_capacity |
8 quarts
12 gallons per hour |
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lycoming O-435
|
| gptkbp:ignition_system |
dual ignition
Champion RE M40 E |
| gptkbp:manufacturer |
gptkb:Lycoming_Engines
|
| gptkbp:power_output |
200 horsepower
|
| gptkbp:propulsion |
constant speed propeller
|
| gptkbp:setting |
horizontally opposed
|
| gptkbp:stroke |
4.0 inches
|
| gptkbp:type |
four-cylinder engine
|
| gptkbp:used_in |
general aviation aircraft
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
approximately 300 pounds
|
| gptkbp:bfsParent |
gptkb:Sikorsky_S-55
gptkb:Fairchild_24 gptkb:Sikorsky_R-4 gptkb:Waco_YKS-6 |
| gptkbp:bfsLayer |
5
|