Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:light_sport_aircraft gyrocopters powered parachutes |
| gptkbp:bore |
72 mm
|
| gptkbp:compressionRatio |
6.6:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Austria
|
| gptkbp:displacement |
496 cc
|
| gptkbp:fuelType |
gptkb:gasoline
carbureted |
| gptkbp:ignition |
dual independent breakerless, magneto CDI
|
| gptkbp:manufacturer |
gptkb:Rotax
|
| gptkbp:max_RPM |
6800
|
| gptkbp:numberOfEngines |
2
|
| gptkbp:oil_system |
pre-mix or oil injection
|
| gptkbp:powerOutput |
50 hp
|
| gptkbp:productionEndYear |
2011
|
| gptkbp:reduction_drive |
optional
|
| gptkbp:starter_system |
manual or electric
|
| gptkbp:status |
discontinued
|
| gptkbp:stroke |
64 mm
|
| gptkbp:type |
gptkb:two-stroke_engine
|
| gptkbp:weight |
approx. 70 lbs (basic configuration)
|
| gptkbp:bfsParent |
gptkb:Rotax
gptkb:Rotax_engines |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rotax 503
|