Statements (13)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:compressor_type |
axial
|
| gptkbp:diameter |
68 in
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-80 C2 B1 F3
|
| gptkbp:length |
156 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:propulsion |
18,500 lbf
|
| gptkbp:weight |
4,000 lb
|
| gptkbp:bfsParent |
gptkb:CF6
|
| gptkbp:bfsLayer |
5
|