Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:aircraft_operated |
gptkb:aircraft
gptkb:Mooney_M20 Piper PA-28 |
| gptkbp:application |
general aviation aircraft
|
| gptkbp:ceo |
1800 hours
|
| gptkbp:certification |
FAA certified
|
| gptkbp:color |
Continental blue
|
| gptkbp:compression_ratio |
8.5:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
360 cubic inches
|
| gptkbp:engine |
gptkb:4
lightweight construction smooth operation durable construction high reliability four-stroke high power-to-weight ratio easy maintenance inline engine versatile applications low vibration proven technology aircraft engine design low fuel consumption good climb performance popular among flight schools O-300 series good throttle response major overhaul required every 1800 hours widely supported by parts suppliers |
| gptkbp:engine_type |
reciprocating engine
|
| gptkbp:first_introduced |
1960s
|
| gptkbp:fuel_capacity |
8 quarts
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental O-360
|
| gptkbp:ignition_system |
removable
dual ignition |
| gptkbp:issues |
oil leaks
carburetor icing valve sticking |
| gptkbp:maintenance |
100 hours
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:market_segment |
gptkb:aircraft
|
| gptkbp:modifications |
turbocharging
fuel injection |
| gptkbp:operational_range |
up to 15,000 feet
|
| gptkbp:power_output |
180 horsepower
|
| gptkbp:propulsion |
fixed-pitch or constant-speed
|
| gptkbp:setting |
horizontally opposed
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 300 lbs
|
| gptkbp:bfsParent |
gptkb:Piper_J-3_C-180
|
| gptkbp:bfsLayer |
6
|