Pratt & Whitney Canada PW307A
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Dassault_Falcon_7X
|
| gptkbp:bypassRatio |
5.3:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA gptkb:Transport_Canada |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
two-spool
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
0.97 m
|
| gptkbp:family |
gptkb:PW300
|
| gptkbp:firstFlight |
1998
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW307A
|
| gptkbp:intendedUse |
business jet
|
| gptkbp:length |
2.1 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfStages |
2
3 axial, 1 centrifugal |
| gptkbp:thrust |
6,405 lbf
|
| gptkbp:weight |
1,350 lb
|
| gptkbp:bfsParent |
gptkb:Dassault_Falcon_7X
|
| gptkbp:bfsLayer |
6
|