Pratt & Whitney Canada PW120A turboprop
GPTKB entity
Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
gptkb:Xian_MA60
gptkb:ATR_42 |
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:family |
gptkb:Pratt_&_Whitney_Canada_PW100
|
| gptkbp:firstFlight |
1983
|
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:introducedIn |
1984
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:powerOutput |
1800 shp
|
| gptkbp:relatedTo |
gptkb:Pratt_&_Whitney_Canada_PW118
Pratt & Whitney Canada PW121 |
| gptkbp:usedIn |
regional airliners
|
| gptkbp:bfsParent |
gptkb:De_Havilland_Canada_Dash_8-100
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW120A turboprop
|