Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
6.2:1
|
| gptkbp:compressionRatio |
30:1
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:family |
gptkb:CFM56
|
| gptkbp:firstFlight |
1991
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:hasConcept |
gptkb:CFM56_core
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM International CFM56-5C
|
| gptkbp:length |
2.47 m
|
| gptkbp:mainRotorDiameter |
1.85 m
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
31,200–34,000 lbf
|
| gptkbp:usedIn |
gptkb:Airbus_A340
|
| gptkbp:weight |
4,850 lb
|
| gptkbp:bfsParent |
gptkb:Airbus_A340-300
|
| gptkbp:bfsLayer |
5
|