|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
twin-spool
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:elevation
|
37,000 ft
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:PW100_family
gptkb:PW100_series
gptkb:PW150
regional aviation
PW120
|
|
gptkbp:engine_configuration
|
twin-engine
twin-engine configuration
twin-spool engine
|
|
gptkbp:engine_power
|
12,500 lbf
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
PW123
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
gptkbp:fuel_capacity
|
1,000 mm
1,200 kg
1,800 mm
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PW123
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Bombardier_CRJ_Series
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:propulsion
|
12,500 lbf
|
|
gptkbp:service_entry
|
gptkb:1992
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Dash_8-300
gptkb:DHC-8-300
|
|
gptkbp:bfsLayer
|
6
|