Pratt & Whitney Canada PW119 B
GPTKB entity
Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:configuration |
twin-spool
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:engine |
Brayton cycle
|
| gptkbp:fan_art |
single-stage fan
|
| gptkbp:first_flight |
gptkb:1998
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW119 B
|
| gptkbp:length |
1,500 mm
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:propulsion |
1,800 lbf
|
| gptkbp:related_aircraft |
gptkb:Dash_8
|
| gptkbp:turbine_type |
high-pressure turbine
|
| gptkbp:type |
turbo-prop engine
|
| gptkbp:used_in |
gptkb:Bombardier_Q400
|
| gptkbp:weight |
1,200 kg
300 kg |
| gptkbp:bfsParent |
gptkb:Fairchild_Dornier_328
|
| gptkbp:bfsLayer |
6
|