|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
up to 1,500 ° C
|
|
gptkbp:bypass_ratio
|
5.1:1
|
|
gptkbp:certification
|
FAA and EASA certified
|
|
gptkbp:combustor_type
|
Annular combustor
|
|
gptkbp:compressor_type
|
gptkb:3
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
30,000 hours
|
|
gptkbp:diameter
|
2.5 m
1.5 m
1.5:1
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
gptkb:CFM56_family
Pneumatic start
|
|
gptkbp:engine_configuration
|
twin-spool
Pylon-mounted
|
|
gptkbp:engine_type
|
high bypass turbofan
|
|
gptkbp:environmental_impact
|
Low emissions and noise levels
|
|
gptkbp:fan_art
|
Wide-chord fan blades
|
|
gptkbp:first_flight
|
gptkb:1993
|
|
gptkbp:fuel_capacity
|
30 liters
|
|
gptkbp:fuel_economy
|
0.5 kg/k N/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
Electronic fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM56-5 C engine
|
|
gptkbp:is_tested_for
|
Static and flight testing
|
|
gptkbp:length
|
3.4 m
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:market_position
|
widely available
|
|
gptkbp:market_share
|
dominant in its class
|
|
gptkbp:max_speed
|
10,000 RPM
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:operational_use
|
worldwide
|
|
gptkbp:produces
|
over 1,000
|
|
gptkbp:propulsion
|
115 k N
38.3 k N/kg
Clamshell type
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_entry
|
gptkb:1994
|
|
gptkbp:services_provided
|
Comprehensive support services offered
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:upgrades
|
Performance upgrades available
|
|
gptkbp:used_in
|
gptkb:Airbus_A340-200
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:bfsParent
|
gptkb:CFM56-5_B_engine
|
|
gptkbp:bfsLayer
|
7
|