Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:application |
regional aircraft
|
| gptkbp:compressor_type |
axial
|
| gptkbp:configuration |
twin-shaft
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design_feature |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
36 in
|
| gptkbp:emissions_standard |
ICAO Chapter 4
|
| gptkbp:first_flight |
gptkb:1998
|
| gptkbp:fuel_economy |
high
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
PW150
|
| gptkbp:length |
54 in
|
| gptkbp:maintenance |
3,600 hours
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:market_segment |
regional aviation
|
| gptkbp:noise_level |
low
|
| gptkbp:power_output |
1,800 to 2,000 shp
|
| gptkbp:propulsion |
up to 5,000 lbf
|
| gptkbp:turbine_type |
free turbine
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Bombardier_Q400
|
| gptkbp:weight |
1,200 lb
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_Canada_PW117
gptkb:Pratt_&_Whitney_Canada_PW100 |
| gptkbp:bfsLayer |
6
|