CF6-80 E1 F

URI: https://gptkb.org/entity/CF6-80_E1_F
GPTKB entity
Statements (37)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application commercial aviation
gptkbp:average_temperature 1,500 ° F
gptkbp:bypass_ratio 5.5:1
gptkbp:certification Stage 3
gptkbp:compressor_type gptkb:10
axial
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:diameter 68 in
112 in
gptkbp:engine gptkb:CF6
gptkbp:engine_configuration twin spool
gptkbp:engine_type high bypass turbofan
gptkbp:first_flight gptkb:1982
gptkbp:fuel_capacity 4,000 lb
112 in
150 in
gptkbp:fuel_economy 0.5 lb/lbf/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label CF6-80 E1 F
gptkbp:launch_platform electric starter
gptkbp:length 150 in
gptkbp:maintenance 6,000 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:notable_users gptkb:Airbus
gptkb:Boeing
gptkb:Mc_Donnell_Douglas_MD-11
gptkbp:number_of_stages_in_low_pressure_compressor gptkb:6
gptkbp:propulsion 60,000 lbf
gptkbp:service_ceiling 40,000 ft
gptkbp:turbine_type gptkb:4
2
high bypass turbofan
gptkbp:weight 4,000 lb
gptkbp:bfsParent gptkb:GE_CF6-80_E1
gptkbp:bfsLayer 6