Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_50
gptkb:Dassault_Falcon_900 |
| gptkbp:bypassRatio |
high bypass
|
| gptkbp:certification |
FAA certified
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:diameter |
approximately 39 inches
|
| gptkbp:family |
gptkb:TFE731
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Garrett TFE731-3R-1H
|
| gptkbp:introduced |
1970s
|
| gptkbp:length |
approximately 80 inches
|
| gptkbp:manufacturer |
gptkb:Garrett_AiResearch
|
| gptkbp:parentCompany |
gptkb:Honeywell_Aerospace
|
| gptkbp:status |
in service
|
| gptkbp:successor |
Honeywell TFE731-5
|
| gptkbp:thrust |
3700 lbf
|
| gptkbp:type |
turbofan
|
| gptkbp:used_in |
business jets
|
| gptkbp:weight |
approximately 950 lbs
|
| gptkbp:bfsParent |
gptkb:BAe_125-400
|
| gptkbp:bfsLayer |
7
|