gptkbp:instance_of
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gptkb:turbofan_engine
gptkb:jet_engine
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gptkbp:application
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gptkb:Airbus
gptkb:Airbus_A340-200/300
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gptkbp:armament
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composite
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gptkbp:average_temperature
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up to 1,500 ° C
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gptkbp:bypass_ratio
|
5.1:1
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gptkbp:certification
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CAEP/6
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gptkbp:compressor_type
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gptkb:5
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gptkbp:configuration
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dual-spool
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gptkbp:control_system
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gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
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gptkbp:diameter
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1.68 m
1.54 m
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gptkbp:engine
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gptkb:CFM56_family
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gptkbp:engine_configuration
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high bypass ratio
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gptkbp:engine_type
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gptkb:CFM56-5_A
gptkb:CFM56-5_E
gptkb:CFM56-5_B
turbofan
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gptkbp:first_flight
|
gptkb:1988
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gptkbp:fuel_type
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gptkb:Jet_A
|
https://www.w3.org/2000/01/rdf-schema#label
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CFM56-5 C
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gptkbp:length
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3.4 m
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gptkbp:maintenance
|
6,000 hours
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gptkbp:manufacturer
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gptkb:CFM_International
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gptkbp:noise_level
|
Stage 3
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gptkbp:produces
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over 8,000
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gptkbp:propulsion
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22,000 to 34,000 lbf
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gptkbp:related_aircraft
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gptkb:Airbus_A320neo
gptkb:Airbus_A319
gptkb:Airbus
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gptkbp:service_entry
|
gptkb:1994
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gptkbp:turbine_type
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2
single crystal superalloy
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gptkbp:weight
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3,000 lb
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gptkbp:bfsParent
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gptkb:CFM56
gptkb:CFM56-5_B
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gptkbp:bfsLayer
|
5
|