Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
5.4:1
|
| gptkbp:certification |
2000
|
| gptkbp:competitor |
gptkb:IAE_V2500
gptkb:CFM56-5 |
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
1.18 m
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_PW_series
|
| gptkbp:firstRun |
1998
|
| gptkbp:intendedUse |
narrow-body aircraft
|
| gptkbp:length |
2.2 m
|
| gptkbp:mainRotorDiameter |
1.18 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:notableClient |
gptkb:Air_France
gptkb:Frontier_Airlines gptkb:LAN_Airlines gptkb:Mexicana_de_Aviación |
| gptkbp:numberOfStages |
2-stage high-pressure turbine
5-stage high-pressure compressor |
| gptkbp:thrust |
18,000 to 24,000 lbf
|
| gptkbp:usedOn |
gptkb:Airbus_A318
|
| gptkbp:weight |
1,800 kg
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_Commercial_Engines
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW6000
|