CFM56-2 N8

URI: https://gptkb.org/entity/CFM56-2_N8
GPTKB entity
Statements (40)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application commercial aviation
gptkbp:average_temperature up to 1,500 ° F
gptkbp:bypass_ratio 5.1:1
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 68 in
60 in
gptkbp:emissions_standard CAEP/6
gptkbp:engine gptkb:CFM56
gptkbp:engine_configuration twin spool
gptkbp:engine_type gptkb:CFM56-2
N8
gptkbp:first_flight gptkb:1982
gptkbp:fuel_capacity 1.68 m
1.73 m
4.0 m
gptkbp:fuel_economy 0.5 lb/lbf/hr
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label CFM56-2 N8
gptkbp:launch_platform electric starter
gptkbp:length 156 in
gptkbp:maintenance 4,000 hours
gptkbp:manufacturer gptkb:CFM_International
gptkbp:noise_level Stage 3
gptkbp:number_of_stages gptkb:10
gptkbp:operational_range 30,000 to 40,000 ft
gptkbp:produces over 8,000 engines
gptkbp:propulsion 22,000 lbf
7.33:1
gptkbp:related_aircraft gptkb:Airbus
gptkb:Boeing_737
gptkbp:revenue over 30 years
gptkbp:service_entry gptkb:1982
gptkbp:turbine_type high bypass
gptkbp:weight 3,000 lb
gptkbp:bfsParent gptkb:CFM56-2_N
gptkbp:bfsLayer 7