CFM56-2 C

GPTKB entity

Statements (59)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:aircraft_usage commercial aviation
gptkbp:application gptkb:Boeing_737
gptkbp:armament fan has 24 blades
gptkbp:cancellation_reason quiet engine design
gptkbp:compressor_type axial compressor
gptkbp:configuration dual-spool
gptkbp:control_system gptkb:full_authority_digital_engine_control_(FADEC)
gptkbp:cooling_system air-cooled
gptkbp:diameter 1.5 m
gptkbp:emissions_standard complies with ICAO Chapter 4
gptkbp:engine gptkb:CFM56-2_B
gptkb:CFM56-3
gptkb:CFM56-5
gptkb:CFM56-7
gptkbp:engine_type gptkb:CFM56-2_C1
gptkb:CFM56-2_C2
gptkb:CFM56-2_C25
gptkb:CFM56-2_C26
gptkb:CFM56-2_C27
gptkb:CFM56-2_C28
gptkb:CFM56-2_C29
gptkb:CFM56-2_C3
gptkb:CFM56-2_C30
gptkb:CFM56-2_C4
gptkb:CFM56-2_C10
gptkb:CFM56-2_C11
gptkb:CFM56-2_C12
gptkb:CFM56-2_C13
gptkb:CFM56-2_C14
gptkb:CFM56-2_C15
gptkb:CFM56-2_C16
gptkb:CFM56-2_C17
gptkb:CFM56-2_C18
gptkb:CFM56-2_C19
gptkb:CFM56-2_C20
gptkb:CFM56-2_C21
gptkb:CFM56-2_C22
gptkb:CFM56-2_C23
gptkb:CFM56-2_C24
gptkb:CFM56-2_C5
gptkb:CFM56-2_C6
gptkb:CFM56-2_C7
gptkb:CFM56-2_C8
gptkb:CFM56-2_C9
gptkbp:first_flight gptkb:1982
gptkbp:fuel_type gptkb:Jet_A
https://www.w3.org/2000/01/rdf-schema#label CFM56-2 C
gptkbp:length 3.5 m
gptkbp:maintenance 6,000 hours
gptkbp:manufacturer gptkb:CFM_International
gptkbp:operational_period 3,000 cycles
gptkbp:produces over 8,000 units
gptkbp:propulsion 22,000 lbf
gptkbp:service_entry gptkb:1982
gptkbp:turbine_type high bypass ratio
gptkbp:weight 3,000 lb
gptkbp:bfsParent gptkb:CFM56-2_B
gptkbp:bfsLayer 5