|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
business jets
|
|
gptkbp:certifications
|
EASA_certified
FAA_certified
|
|
gptkbp:climate
|
up to 1,500 °F
|
|
gptkbp:compressionRatio
|
3.5:1
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital electronic control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
advanced materials
high bypass ratio
low specific fuel consumption
|
|
gptkbp:developer
|
derived_from_PW535E
|
|
gptkbp:diameter
|
24 in
28 in
|
|
gptkbp:emissionsStandard
|
CAEP/6
|
|
gptkbp:engine
|
rear-mounted
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
2
5
turbofan
turbojet
axial
air start
single-stage high-pressure turbine
|
|
gptkbp:firstFlight
|
2000
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuelType
|
Jet A
electronic fuel control system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pratt & Whitney Canada PW617F
|
|
gptkbp:length
|
48 in
|
|
gptkbp:maintenance
|
3,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:market_segment
|
light jets
very light jets
|
|
gptkbp:noise_level
|
Stage 4
|
|
gptkbp:notableUsers
|
gptkb:Bombardier_Learjet_75
gptkb:Cessna_Citation_M2
Embraer Phenom 100
|
|
gptkbp:operationalRange
|
up to 41,000 ft
|
|
gptkbp:performances
|
scheduled maintenance required
optimized for short takeoff and landing
|
|
gptkbp:propulsion
|
5:1
1,500 lbf
|
|
gptkbp:related_engine
|
gptkb:PW600_series
Brayton_cycle
|
|
gptkbp:reliability
|
high
|
|
gptkbp:services
|
up to 20,000 hours
|
|
gptkbp:weight
|
approximately 300 lb
|