|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
1,000 mm
1,200 mm
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PW100_family
turboprop aircraft
|
|
gptkbp:engine_configuration
|
twin-engine
high bypass ratio
pylon-mounted
2,000 lbf
|
|
gptkbp:engine_type
|
gptkb:PW100
gptkb:PW127
gptkb:PW150
turbofan
PW121
PW127 G
PW127 M
PW127 F
PW127 E
PW127 H
PW127 N
PW127 R
PW127 S
PW127 T
PW127 U
PW127 V
PW127 W
PW127 X
PW127 Y
PW127 Z
PW152
|
|
gptkbp:first_introduced
|
gptkb:1997
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
hydromechanical
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PW117
|
|
gptkbp:length
|
1,500 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_range
|
30,000 ft
|
|
gptkbp:power_output
|
1,500 k W
|
|
gptkbp:propulsion
|
2,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1998
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:used_in
|
gptkb:Bombardier_Q400
|
|
gptkbp:weight
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:Saab_340
|
|
gptkbp:bfsLayer
|
5
|