CFM56-2 P4

GPTKB entity

Statements (66)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application commercial aviation
gptkbp:average_temperature 1,500 ° F
gptkbp:bypass_ratio 5.1:1
gptkbp:certification FAA certified
gptkbp:combustor_type annular
low emissions combustor
gptkbp:compressor_type gptkb:9
gptkbp:control_system gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
gptkbp:diameter 68 in
60 in
gptkbp:emissions_standard CAEP/6
gptkbp:engine gptkb:CFM56
gptkb:CFM56_family
advanced aerodynamics
scheduled maintenance
narrow-body aircraft
global network
modern materials
continuous improvements
gptkbp:engine_certification_body gptkb:EASA
gptkbp:engine_compressor_design high pressure ratio compressor
gptkbp:engine_configuration twin-engine
22,000 lbf
high bypass ratio
gptkbp:engine_fan_design wide chord fan blades
gptkbp:engine_inlet_design advanced design
gptkbp:engine_noise_certification Stage 4 compliant
gptkbp:engine_operational_flexibility versatile use
gptkbp:engine_power high
efficient
20,000 hours
proven track record
gptkbp:engine_thrust_reverser yes
gptkbp:engine_turbine_design high efficiency turbine
gptkbp:engine_type gptkb:CFM56-2
gptkb:CFM56-2_P4
turbofan
gptkbp:first_flight gptkb:1982
gptkbp:first_introduced gptkb:1982
gptkbp:fuel_capacity 1.7 m
4.0 m
1,360 kg
gptkbp:fuel_economy 0.5 lb/lbf/hr
gptkbp:fuel_type gptkb:Jet_A
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label CFM56-2 P4
gptkbp:is_tested_for extensive testing
gptkbp:length 156 in
gptkbp:maintenance cost-effective
4,000 hours
gptkbp:manufacturer gptkb:CFM_International
gptkbp:noise_level low
gptkbp:notable_users gptkb:Airbus
gptkb:Boeing_737
gptkbp:number_of_engines 2
gptkbp:produces over 30,000 engines
gptkbp:propulsion 7.3:1
22,000 lbf
gptkbp:reliability high
gptkbp:service_ceiling 40,000 ft
gptkbp:turbine_type 2
gptkbp:water_requirement 1,200 lb/hr
gptkbp:weight 3,000 lb
gptkbp:bfsParent gptkb:CFM56-2_P
gptkbp:bfsLayer 7