|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:aircraft_type
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:application
|
wide-body aircraft
|
|
gptkbp:average_temperature
|
high
|
|
gptkbp:bypass_ratio
|
8.5:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:competitors
|
gptkb:Rolls-Royce_Trent_800
gptkb:GE90
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:configuration
|
dual-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
global network
|
|
gptkbp:design
|
30,000 hours
|
|
gptkbp:diameter
|
2.7 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:East_Hartford,_Connecticut
gptkb:PW4000_family
advanced materials
|
|
gptkbp:engine_configuration
|
customizable
pylon-mounted
|
|
gptkbp:engine_disassembly_location
|
gptkb:East_Hartford,_Connecticut
|
|
gptkbp:engine_repair_facility
|
Pratt & Whitney repair facility
|
|
gptkbp:engine_starting_system
|
electric starter
|
|
gptkbp:engine_upgrade_options
|
available
|
|
gptkbp:first_flight
|
gptkb:1995
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW4000-113 J
|
|
gptkbp:is_tested_for
|
Pratt & Whitney test facility
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
moderate
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_position
|
high
|
|
gptkbp:noise_level
|
low
yes
|
|
gptkbp:number_of_engines
|
over 1,000
|
|
gptkbp:operational_range
|
long-haul flights
|
|
gptkbp:propulsion
|
25:1
113,000 lbf
|
|
gptkbp:rating
|
excellent
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_entry
|
gptkb:1995
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:weight
|
4,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW4000
|
|
gptkbp:bfsLayer
|
5
|