Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
8.7:1
|
| gptkbp:certification |
2006
|
| gptkbp:competitor |
gptkb:Rolls-Royce_Trent_900
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:General_Electric
gptkb:Pratt_&_Whitney |
| gptkbp:family |
gptkb:Engine_Alliance_GP7000
|
| gptkbp:firstFlight |
2004
|
| gptkbp:length |
184 in
|
| gptkbp:mainRotorDiameter |
116 in
|
| gptkbp:manufacturer |
gptkb:Engine_Alliance
|
| gptkbp:notableUser |
gptkb:Air_France
gptkb:Emirates gptkb:Etihad_Airways gptkb:Korean_Air |
| gptkbp:numberOfAxles |
two
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
up to 81,500 lbf
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:usedOn |
gptkb:aircraft
|
| gptkbp:weight |
15,000 lb
|
| gptkbp:bfsParent |
gptkb:Engine_Alliance
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
GP7200
|