Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_900DX
gptkb:Dassault_Falcon_900EX gptkb:Dassault_Falcon_900LX |
| gptkbp:bypassRatio |
5.0:1
|
| gptkbp:certification |
gptkb:FAA
|
| gptkbp:compressor_type |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
34.5 in
|
| gptkbp:family |
gptkb:Honeywell_TFE731
|
| gptkbp:firstRun |
1997
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Honeywell TFE731-60
|
| gptkbp:intendedUse |
business jet
|
| gptkbp:length |
80.5 in
|
| gptkbp:manufacturer |
gptkb:Honeywell_Aerospace
|
| gptkbp:number_of_shafts |
2
|
| gptkbp:numberOfStages |
2
1 fan, 4 axial, 1 centrifugal |
| gptkbp:thrust |
5000 lbf
|
| gptkbp:weight |
1,080 lb
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_900DX
gptkb:Dassault_Falcon_900LX gptkb:Falcon_900DX gptkb:Falcon_900LX gptkb:Garrett_TFE731-5AR-1C |
| gptkbp:bfsLayer |
7
|