Pratt & Whitney Canada PW150 A

URI: https://gptkb.org/entity/Pratt_%26_Whitney_Canada_PW150_A
GPTKB entity
Statements (42)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Bombardier_Q400
gptkbp:certification gptkb:Transport_Canada
gptkbp:compressor_type axial
gptkbp:configuration twin-shaft
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:design_features high bypass ratio
gptkbp:diameter 1,100 mm
gptkbp:emissions_standard ICAO Chapter 4
gptkbp:engine gptkb:PW100
gptkb:PW100_family
gptkb:PW100_series
gptkb:PW127
PW121
gptkbp:engine_configuration 1,500 shp
twin-shaft
gptkbp:engine_type gptkb:turbofan_engine
turboprop
gptkbp:first_flight gptkb:1996
gptkbp:fuel_capacity 1,500 mm
1,100 mm
gptkbp:fuel_economy 0.5 lb/hp/hr
gptkbp:fuel_type gptkb:Jet_A
gptkbp:has_programs PW100 development
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney Canada PW150 A
gptkbp:length 1,500 mm
gptkbp:maintenance 4,000 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney_Canada
gptkbp:market_segment regional aircraft
gptkbp:noise_level gptkb:Stage_4
gptkbp:number_of_engines 2
gptkbp:number_of_stages gptkb:6
gptkbp:operational_use commercial aviation
gptkbp:power_output 1,800 k W
gptkbp:propulsion 5,000 lbf
gptkbp:service_ceiling 25,000 ft
gptkbp:turbine_type free turbine
gptkbp:weight 1,200 kg
1,500 kg
gptkbp:bfsParent gptkb:Bombardier_Q400
gptkbp:bfsLayer 5