|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:Bombardier_Learjet_75
gptkb:Cessna_Citation_CJ4
Embraer Phenom 300
|
|
gptkbp:application
|
business jets
|
|
gptkbp:compressionRatio
|
4.5:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
CAEP/6
|
|
gptkbp:engine
|
modular design
high bypass ratio
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
turbojet
axial
bleed air
PW535A
PW535E
high-pressure and low-pressure
PW535C
PW535D
PW535U
PW535F
PW535H
PW535I
PW535J
PW535K
PW535L
PW535O
PW535P
PW535Q
PW535R
PW535S
PW535T
PW535V
PW535W
PW535X
PW535Y
PW535Z
PW535G
PW535M
PW535N
|
|
gptkbp:exhaustSystem
|
subsonic
|
|
gptkbp:firstFlight
|
1997
|
|
gptkbp:fuel_capacity
|
0.5 lb/hp/hr
|
|
gptkbp:fuelType
|
Jet A
annular
electronic fuel control
|
|
gptkbp:hasArea
|
FAA_certified
Pratt_&_Whitney_Canada_facilities
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PW535B
|
|
gptkbp:length
|
1,500 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:noise_level
|
Stage 4
|
|
gptkbp:number_of_stages
|
10
|
|
gptkbp:operationalRange
|
0 to 100% N1
|
|
gptkbp:propulsion
|
3,500 lbf
|
|
gptkbp:related_engine
|
PW500 series
|
|
gptkbp:reviews
|
3,500 lbf
|
|
gptkbp:service_ceiling
|
41,000 ft
|
|
gptkbp:setting
|
twin-spool
|
|
gptkbp:weight
|
300 kg
|