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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:Airbus
|
|
gptkbp:average_temperature
|
1,500 ° C
|
|
gptkbp:bypass_ratio
|
5.1:1
|
|
gptkbp:certification
|
gptkb:FAA
CAEP/6
|
|
gptkbp:compressor_type
|
Fan, 3-stage low-pressure, 5-stage high-pressure
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:diameter
|
1.68 m
|
|
gptkbp:engine
|
gptkb:CFM56_series
gptkb:CFM56_family
|
|
gptkbp:engine_configuration
|
22,000 to 33,000 lbf
twin spool
|
|
gptkbp:engine_type
|
gptkb:CFM56-5_B9
dual rotor
|
|
gptkbp:first_flight
|
gptkb:1988
|
|
gptkbp:fuel_capacity
|
1.68 m
3,000 kg
3.3 m
|
|
gptkbp:fuel_economy
|
0.5 kg/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:high_pressure_compressor_stages
|
gptkb:5
|
|
gptkbp:high_pressure_turbine_stages
|
2
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-5 B9
|
|
gptkbp:length
|
3.3 m
|
|
gptkbp:low_pressure_compressor_stages
|
gptkb:3
|
|
gptkbp:low_pressure_turbine_stages
|
gptkb:1
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_users
|
gptkb:Lufthansa
gptkb:United_Airlines
gptkb:Air_France
gptkb:British_Airways
|
|
gptkbp:produces
|
over 8,000
|
|
gptkbp:propulsion
|
22,000 to 33,000 lbf
|
|
gptkbp:service_entry
|
gptkb:1989
|
|
gptkbp:successor
|
gptkb:CFM_LEAP
|
|
gptkbp:turbine_type
|
2-stage high-pressure, 1-stage low-pressure
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:variant
|
gptkb:CFM56-5_B
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:CFM56-5_B
|
|
gptkbp:bfsLayer
|
5
|