Pratt & Whitney PW4000

GPTKB entity

Statements (65)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkb:jet_engine
gptkbp:application gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
wide-body aircraft
gptkbp:cancellation_reason yes
gptkbp:compressor_type axial compressor
gptkbp:control_system gptkb:FADEC
gptkbp:cooling_system air-cooled
gptkbp:customer_support gptkb:American_Airlines
gptkbp:design high bypass ratio
gptkbp:diameter 94 inches
gptkbp:engine gptkb:Boeing_707
gptkbp:engine_type gptkb:PW4000-112_E
gptkb:PW4000-113_E
gptkb:PW4000-100
gptkb:PW4000-100_D
gptkb:PW4000-100_I
gptkb:PW4000-100_J
gptkb:PW4000-100_R
gptkb:PW4000-112
gptkb:PW4000-112_H
gptkb:PW4000-112_I
gptkb:PW4000-112_J
gptkb:PW4000-112_R
gptkb:PW4000-113_H
gptkb:PW4000-113_I
gptkb:PW4000-113_J
gptkb:PW4000-113_R
gptkb:PW4000-94
gptkb:PW4000-94_D
gptkb:PW4000-94_I
gptkb:PW4000-94_J
gptkb:PW4000-94_R
gptkb:PW4000-100_B
gptkb:PW4000-100_E
gptkb:PW4000-112_B
gptkb:PW4000-113_B
gptkb:PW4000-94_B
gptkb:PW4000-94_E
PW4000-113
PW4000-100 F
PW4000-100 G
PW4000-100 H
PW4000-112 F
PW4000-112 G
PW4000-113 F
PW4000-113 G
PW4000-94 F
PW4000-94 G
PW4000-94 H
gptkbp:first_flight gptkb:1986
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney PW4000
gptkbp:maintenance 4,000 hours
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:number_of_engines two or four
gptkbp:propulsion 18,000 to 52,000 lbf
18,000 to 33,000 lbf
gptkbp:turbine_type high-pressure turbine
gptkbp:weight approximately 8,000 lb
gptkbp:bfsParent gptkb:Boeing_707
gptkb:Airbus
gptkbp:bfsLayer 4