CFM56-5 B2

URI: https://gptkb.org/entity/CFM56-5_B2
GPTKB entity
Statements (47)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application gptkb:Airbus
gptkbp:armament gptkb:textiles
gptkbp:average_temperature 1,500 ° F
gptkbp:bypass_ratio 5.1:1
gptkbp:combustor_type annular combustor
gptkbp:compression_system axial compressor
gptkbp:compressor_stage_material aluminum alloy
gptkbp:control_system gptkb:FADEC
gptkbp:cooling_system air-cooled
gptkbp:diameter 1.5 m
gptkbp:emissions_standard CAEP/6
gptkbp:engine gptkb:CFM56_family
gptkbp:engine_configuration twin-spool
gptkbp:engine_type gptkb:CFM56-5_B
turbofan
gptkbp:first_flight gptkb:1988
gptkbp:fuel_capacity 1.5 m
3.5 m
1,360 kg
gptkbp:fuel_type gptkb:Jet_A
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label CFM56-5 B2
gptkbp:launched air starter
gptkbp:length 3.5 m
gptkbp:maintenance 6,000 hours
gptkbp:manufacturer gptkb:CFM_International
gptkbp:noise_level Stage 4 compliant
gptkbp:number_of_engines 2
gptkbp:number_of_stages 5 stages
gptkbp:operational_range -54 to 50 ° C
gptkbp:propulsion 7.3:1
22,000 lbf
22,000 to 33,000 lbf
33,000 lbf
gptkbp:related_aircraft gptkb:Boeing_737_Next_Generation
gptkb:Airbus_A319
gptkb:Airbus
gptkb:Boeing_737
gptkb:Mc_Donnell_Douglas_MD-80
gptkbp:service_entry gptkb:1994
gptkbp:total_engine_pressure_ratio 30:1
gptkbp:turbine_stage_material nickel alloy
gptkbp:type high bypass turbofan
gptkbp:weight 3,000 lb
gptkbp:bfsParent gptkb:CFM56-5_B_series
gptkbp:bfsLayer 7