Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
5.72:1
|
| gptkbp:certification |
1971
|
| gptkbp:compressionStages |
16
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
86.4 in
|
| gptkbp:family |
gptkb:CF6_engine_family
|
| gptkbp:firstRun |
1971
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
high-bypass turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
CF6-6
|
| gptkbp:length |
163 in
|
| gptkbp:mainRotorDiameter |
86.4 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:CF6-50
|
| gptkbp:thrust |
41,000 lbf
|
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:McDonnell_Douglas_DC-10 |
| gptkbp:weight |
8,650 lb
|
| gptkbp:bfsParent |
gptkb:General_Electric_CF6
|
| gptkbp:bfsLayer |
5
|