Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:certifications |
FAA_certified
|
| gptkbp:compressionRatio |
5.5:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
68 in
|
| gptkbp:engineType |
axial
high bypass ratio |
| gptkbp:firstFlight |
1982
|
| gptkbp:fuel_capacity |
0.5 lb/lbf/hr
|
| gptkbp:fuelType |
Jet A
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-80C2B6E14
|
| gptkbp:length |
158 in
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableUsers |
gptkb:Airbus_A330
gptkb:Boeing_767 |
| gptkbp:propulsion |
60,000 lbf
|
| gptkbp:related_engine |
gptkb:CF6_family
|
| gptkbp:weight |
4,000 lb
|