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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:Boeing_737
|
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gptkbp:armament
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gptkb:textiles
|
|
gptkbp:certification
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gptkb:FAA
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
gptkb:5
axial compressor
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
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gptkbp:cooling_system
|
air-cooled
|
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gptkbp:design
|
modular design
|
|
gptkbp:diameter
|
1.5 m
5.5:1
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|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:CFM56-2_series
gptkb:CFM56_family
|
|
gptkbp:engine_configuration
|
twin-spool
|
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gptkbp:engine_type
|
gptkb:CFM56-2_C
gptkb:CFM56-2_E
gptkb:CFM56-2_B
gptkb:CFM56-2_F
gptkb:CFM56-2_G
gptkb:CFM56-2_H
gptkb:CFM56-2_J
gptkb:CFM56-2_K
gptkb:CFM56-2_L
gptkb:CFM56-2_M
gptkb:CFM56-2_N
gptkb:CFM56-2_O
gptkb:CFM56-2_P
gptkb:CFM56-2_Q
gptkb:CFM56-2_R
gptkb:CFM56-2_S
gptkb:CFM56-2_T
gptkb:CFM56-2_U
gptkb:CFM56-2_V
gptkb:CFM56-2_W
gptkb:CFM56-2_I
CFM56-2 D
|
|
gptkbp:first_flight
|
gptkb:1982
|
|
gptkbp:fuel_capacity
|
1.5 m
3.5 m
1,360 kg
|
|
gptkbp:fuel_economy
|
0.5 lb/lbf/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-2 W
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:noise_level
|
Stage 3 compliant
|
|
gptkbp:notable_users
|
gptkb:Delta_Air_Lines
gptkb:United_Airlines
gptkb:Air_France
|
|
gptkbp:operational_history
|
widely used in commercial aviation
|
|
gptkbp:propulsion
|
22,000 lbf
27,000 lbf
cascade thrust reverser
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service
|
up to 30,000 hours
|
|
gptkbp:turbine_type
|
gptkb:Super_GT
2
axial turbine
|
|
gptkbp:type
|
high-bypass turbofan
|
|
gptkbp:weight
|
3,000 lb
|
|
gptkbp:bfsParent
|
gptkb:CFM56-2
|
|
gptkbp:bfsLayer
|
6
|