|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:armament
|
composite
|
|
gptkbp:average_temperature
|
1,500 ° F
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CFM56_family
every 20,000 hours
|
|
gptkbp:engine_configuration
|
twin-spool
2 C4 J rating
|
|
gptkbp:engine_power
|
30,000 hours
|
|
gptkbp:engine_type
|
gptkb:CFM56-2_C4_B
gptkb:CFM56-2_C4_E
gptkb:CFM56-2_C4_F
gptkb:CFM56-2_C4_G
gptkb:CFM56-2_C4_H
dual-rotor
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-2 C4 J
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_period
|
high bypass ratio
|
|
gptkbp:propulsion
|
22,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Airbus
gptkb:Boeing_737
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:turbine_type
|
gptkb:Super_GT
high-pressure turbine
low-pressure turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CFM56-2_C4
|
|
gptkbp:bfsLayer
|
7
|