Pratt & Whitney Canada PW307D
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_8X
|
| gptkbp:bypassRatio |
5.4:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
two-spool
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
0.97 m
|
| gptkbp:family |
gptkb:PW300
|
| gptkbp:firstFlight |
2015
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW307D
|
| gptkbp:intendedUse |
business jet
|
| gptkbp:length |
2.1 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:thrust |
6,722 lbf
|
| gptkbp:weight |
650 kg
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_8X
gptkb:Falcon_8X |
| gptkbp:bfsLayer |
7
|