|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:bypass_ratio
|
8:1
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
68 in
112 in
|
|
gptkbp:emissions_standard
|
NOx standard
|
|
gptkbp:engine
|
gptkb:CF6
gptkb:CF6-80
gptkb:CF6-80_E1_A
gptkb:CF6-80_E1_B
gptkb:CF6-80_E1_D
gptkb:CF6-80_E1_E
gptkb:CF6-80_E1_F
gptkb:CF6-80_E1
CF6-80 C2
CF6-80 E1 C
CF6-80 E1 G
CF6-80 E1 H
|
|
gptkbp:engine_configuration
|
pylon-mounted
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_delivery
|
gptkb:1983
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
dry sump
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80 E1 D4
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
150 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_users
|
gptkb:Boeing_707
gptkb:Airbus
gptkb:Mc_Donnell_Douglas_MD-11
|
|
gptkbp:operational_range
|
3,000 nautical miles
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:propulsion
|
60,000 lbf
cascade
|
|
gptkbp:service_ceiling
|
42,000 ft
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:weight
|
4,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CF6-80_E1_D
|
|
gptkbp:bfsLayer
|
7
|