Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
regional airliner
|
| gptkbp:bypassRatio |
5.3:1
|
| gptkbp:compressor_type |
axial/centrifugal
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:family |
gptkb:CF34
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric CF34-8C1
|
| gptkbp:introducedIn |
1999
|
| gptkbp:length |
2.49 m
|
| gptkbp:mainRotorDiameter |
1.22 m
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:thrust |
13,780 lbf
|
| gptkbp:usedInAircraft |
gptkb:Bombardier_CRJ700
|
| gptkbp:weight |
1,544 kg
|
| gptkbp:bfsParent |
gptkb:CRJ700
|
| gptkbp:bfsLayer |
8
|