GE Aviation's CF34

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application regional jets
gptkbp:certification CAEP/6
gptkbp:compressor_type axial compressor
gptkbp:design_features gptkb:full_authority_digital_engine_control_(FADEC)
advanced aerodynamics
modular design
safety features
reduced maintenance costs
high reliability
environmentally friendly
durable materials
high efficiency
easy installation
quick turnaround times
improved fuel efficiency
global service network
high thrust-to-weight ratio
low operating costs
versatile applications
comprehensive support services
robust performance
advanced materials technology
low noise technology
high bypass ratio fan
state-of-the-art manufacturing processes
modular maintenance approach
advanced engine monitoring systems
gptkbp:diameter 1.5 m
68 in
gptkbp:engine_configuration twin-spool
gptkbp:first_flight gptkb:1982
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label GE Aviation's CF34
gptkbp:length 3.5 m
gptkbp:maintenance 5,000 hours
gptkbp:manufacturer gptkb:General_Electric
gptkbp:noise_level gptkb:Stage_4
gptkbp:produces over 5,000
gptkbp:propulsion up to 34,000 lbf
gptkbp:related_aircraft gptkb:Ilyushin_Il-114
gptkb:Mc_Donnell_Douglas_MD-80_series
gptkb:Bombardier_CRJ_series
gptkb:Sukhoi_Superjet_100
gptkb:Embraer_E-Jet_series
gptkbp:reliability high
gptkbp:service_entry gptkb:1983
gptkbp:turbine_type high bypass ratio
gptkbp:variant gptkb:CF34-10_E
gptkb:CF34-8_C
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:PW1900_G_engine
gptkbp:bfsLayer 8