Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine family
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
5:1
|
| gptkbp:certification |
December 2000
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:firstFlight |
2000
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
axial flow
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW6000 series
|
| gptkbp:intendedAircraft |
gptkb:Airbus_A318
|
| gptkbp:length |
2.3 m
|
| gptkbp:mainRotorDiameter |
1.24 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:marketedAs |
efficient, low-cost engine for short-haul aircraft
|
| gptkbp:notableUser |
gptkb:TAME
gptkb:Air_France gptkb:Frontier_Airlines gptkb:LAN_Airlines |
| gptkbp:numberOfSpools |
2
|
| gptkbp:relatedTo |
gptkb:V2500
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
18,000 to 24,000 lbf
|
| gptkbp:weight |
1,200 kg
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_PW6000
|
| gptkbp:bfsLayer |
7
|