Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Airbus_A310
gptkb:Boeing_767 gptkb:aircraft gptkb:Airbus_A300 gptkb:Boeing_767-300F gptkb:Boeing_E-4 gptkb:McDonnell_Douglas_MD-11 |
| gptkbp:bypassRatio |
5.0:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:family |
gptkb:General_Electric_CF6
|
| gptkbp:firstRun |
1984
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
high-bypass turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF6-80C2
|
| gptkbp:length |
183 in
|
| gptkbp:mainRotorDiameter |
93 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:notableFeature |
improved fuel efficiency
high reliability |
| gptkbp:status |
in production
|
| gptkbp:thrust |
52,500 to 61,500 lbf
|
| gptkbp:usedBy |
gptkb:aircraft
commercial airlines |
| gptkbp:weight |
9,860 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF6-80E1
|
| gptkbp:bfsLayer |
5
|