Statements (15)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aero engine variant
|
| gptkbp:application |
commercial aviation
|
| gptkbp:certification |
2011
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:engineType |
high-bypass turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trent 1000 Package C
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:numberOfIssues |
durability problems with intermediate pressure turbine blades
|
| gptkbp:partOf |
gptkb:Rolls-Royce_Trent_1000
|
| gptkbp:predecessor |
gptkb:Trent_1000_Package_B
|
| gptkbp:successor |
gptkb:Trent_1000_TEN
|
| gptkbp:thrust |
around 74,000 lbf
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:bfsParent |
gptkb:Trent_1000_family
|
| gptkbp:bfsLayer |
7
|