Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
business jet
|
| gptkbp:bypassRatio |
4.2:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:diameter |
34.2 in
|
| gptkbp:family |
gptkb:Honeywell_TFE731
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell TFE731-60 (900LX)
|
| gptkbp:introducedIn |
2008
|
| gptkbp:length |
78.5 in
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:thrust |
5000 lbf
|
| gptkbp:usedIn |
gptkb:Dassault_Falcon_900LX
|
| gptkbp:weight |
1,520 lb
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_900
|
| gptkbp:bfsLayer |
6
|