Pratt & Whitney PW2040

URI: https://gptkb.org/entity/Pratt_%26_Whitney_PW2040
GPTKB entity
Statements (35)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Flight
gptkb:Mc_Donnell_Douglas_MD-90
gptkbp:bypass_ratio 4.5:1
gptkbp:compressor_type gptkb:6
axial compressor
gptkbp:configuration twin-spool
dual-spool
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:design high bypass ratio
gptkbp:diameter 1.8 m
1.5 m
68 in
3.0 ft
gptkbp:engine_type high bypass turbofan
gptkbp:first_flight gptkb:1993
gptkb:1994
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney PW2040
gptkbp:introduced gptkb:1993
gptkbp:length 3.5 m
11.5 ft
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:notable_users gptkb:Mc_Donnell_Douglas_MD-90
gptkbp:propulsion 20,000 lbf
gptkbp:related_aircraft gptkb:Mc_Donnell_Douglas_MD-95
gptkb:Boeing_717
gptkb:Mc_Donnell_Douglas_MD-80
gptkbp:successor gptkb:PW1500_G
gptkbp:turbine_type 2
high-pressure turbine
gptkbp:weight 1,200 kg
3,800 lb
gptkbp:bfsParent gptkb:Boeing_707
gptkbp:bfsLayer 4