Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:Airbus_A300 gptkb:McDonnell_Douglas_DC-10 |
| gptkbp:bypassRatio |
4.26:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:compressor_stages |
16
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
86.4 in
|
| gptkbp:family |
gptkb:General_Electric_CF6
|
| gptkbp:firstRun |
1974
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF6-50C2
|
| gptkbp:length |
183 in
|
| gptkbp:mainRotorDiameter |
86.4 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:thrust |
52,500 lbf
|
| gptkbp:used_in |
Boeing KC-10 Extender
|
| gptkbp:weight |
8,850 lb
|
| gptkbp:bfsParent |
gptkb:Airbus_A300B2-203
|
| gptkbp:bfsLayer |
6
|