Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:armament |
composite
|
| gptkbp:bypass_ratio |
5.5:1
|
| gptkbp:certification |
CAEP/6
|
| gptkbp:compressor_type |
fan, 3 low-pressure, 10 high-pressure
|
| gptkbp:control_system |
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
| gptkbp:diameter |
68 inches
|
| gptkbp:engine |
gptkb:CF6_family
|
| gptkbp:first_flight |
gptkb:1982
|
| gptkbp:fuel_type |
gptkb:Jet_A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF6-80 C5
|
| gptkbp:maintenance |
6,000 hours
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:noise_level |
Stage 3
|
| gptkbp:propulsion |
22,000 to 34,000 lbf
|
| gptkbp:turbine_type |
2 high-pressure, 1 low-pressure
|
| gptkbp:type |
high bypass turbofan
|
| gptkbp:uses |
gptkb:Boeing_707
gptkb:Airbus gptkb:Mc_Donnell_Douglas_MD-11 |
| gptkbp:weight |
3,800 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF6-80_C2
|
| gptkbp:bfsLayer |
5
|