Pratt & Whitney Canada PW535B
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Cessna_Citation_Encore+
|
| gptkbp:bypassRatio |
2.9:1
|
| gptkbp:certification |
gptkb:FAA
gptkb:Transport_Canada |
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
two-stage fan, two axial, one centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:diameter |
24.2 in
|
| gptkbp:family |
gptkb:PW500_series
|
| gptkbp:firstFlight |
2006
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW535B
|
| gptkbp:length |
63.6 in
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:thrust |
3,400 lbf
|
| gptkbp:turbineType |
two-stage high-pressure, two-stage low-pressure
|
| gptkbp:usedOn |
gptkb:Cessna_Citation_Encore+
|
| gptkbp:weight |
1,020 lb
|
| gptkbp:bfsParent |
gptkb:Cessna_Citation_Encore+
|
| gptkbp:bfsLayer |
7
|