Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:certification |
2011
|
| gptkbp:compressionRatio |
axial-centrifugal
|
| gptkbp:countryOfOrigin |
gptkb:Canada
|
| gptkbp:features |
improved fuel efficiency
FADEC control increased thermodynamic power |
| gptkbp:fuelType |
gptkb:Jet-A
|
| gptkbp:improves |
gptkb:PW127F
|
| gptkbp:length |
approx. 2.1 m
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:market |
civil aviation
|
| gptkbp:numberOfStages |
2 power, 1 gas generator
3 axial, 1 centrifugal |
| gptkbp:partOf |
gptkb:PW100_engine_family
|
| gptkbp:powerOutput |
2750 shp
|
| gptkbp:usedIn |
gptkb:ATR_42-600
gptkb:ATR_72-600 |
| gptkbp:weight |
approx. 350 kg
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_Canada_PW127
gptkb:PW-100 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW127M
|