Pratt & Whitney Canada PW306D1
GPTKB entity
Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_Citation_Latitude
|
| gptkbp:bypassRatio |
5.2:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:combustorType |
annular
|
| gptkbp:compressionStages |
2 axial + 1 centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
28.4 in
|
| gptkbp:family |
gptkb:PW300
|
| gptkbp:firstFlight |
2014
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW306D1
|
| gptkbp:length |
75.6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:numberOfAxles |
2
|
| gptkbp:thrust |
5,907 lbf
|
| gptkbp:usedOn |
gptkb:Cessna_Citation_Latitude
|
| gptkbp:weight |
1,520 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_Citation_Latitude
|
| gptkbp:bfsLayer |
7
|