Pratt & Whitney Canada PW120
GPTKB entity
Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:configuration |
twin-shaft
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:first_flight |
gptkb:1984
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW120
|
| gptkbp:length |
1,200 mm
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:notable_users |
gptkb:Bombardier_Dash_8
|
| gptkbp:number_of_stages |
6 stages
|
| gptkbp:power_output |
1,800 shp
|
| gptkbp:propulsion |
4.5:1
|
| gptkbp:turbine_type |
free turbine
|
| gptkbp:weight |
approximately 400 kg
|
| gptkbp:bfsParent |
gptkb:Dash_8-100
gptkb:DHC-8-100 |
| gptkbp:bfsLayer |
6
|