Pratt & Whitney Canada PW127 G
GPTKB entity
Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
regional aircraft
|
| gptkbp:armament |
gptkb:6
|
| gptkbp:combustor_type |
annular combustion chamber
|
| gptkbp:compression_ratio |
8:1
|
| gptkbp:configuration |
free turbine
|
| gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1,300 mm
|
| gptkbp:elevation |
25,000 ft
|
| gptkbp:engine_configuration |
twin-shaft
|
| gptkbp:engine_type |
turboprop
|
| gptkbp:first_flight |
gptkb:1998
|
| gptkbp:fuel_economy |
0.5 lb/hp/hr
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
Pratt & Whitney Canada PW127 G
|
| gptkbp:length |
1,500 mm
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney_Canada
|
| gptkbp:power_output |
1,850 k W
|
| gptkbp:propulsion |
2,500 lbf
|
| gptkbp:service_entry |
gptkb:2000
|
| gptkbp:type |
turbo-prop engine
|
| gptkbp:used_in |
gptkb:Bombardier_Q400
|
| gptkbp:weight |
400 kg
|
| gptkbp:bfsParent |
gptkb:C295
|
| gptkbp:bfsLayer |
5
|