gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Lockheed_Martin_KC-390
|
gptkbp:application
|
gptkb:aircraft
|
gptkbp:armament
|
composite materials
|
gptkbp:bypass_ratio
|
4.5:1
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gptkbp:certification
|
FAA certified
EASA certified
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gptkbp:competitors
|
CF M56
Pratt & Whitney P W1100 G
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
gptkbp:cooling_system
|
advanced cooling technology
|
gptkbp:customer_base
|
airlines worldwide
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gptkbp:customer_support
|
global network
|
gptkbp:design
|
modular design
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gptkbp:developer
|
gptkb:General_Electric
gptkb:Rolls-Royce
gptkb:MTU_Aero_Engines
|
gptkbp:diameter
|
1.5 m
|
gptkbp:emissions_standard
|
CAEP/6
|
gptkbp:engine
|
gptkb:government_agency
gptkb:Japan
gptkb:United_Kingdom
gptkb:United_States
state-of-the-art technology
air start
widely used in commercial aviation
field modifications possible
global repair network
|
gptkbp:engine_type
|
axial compressor
high-pressure and low-pressure turbines
high bypass turbofan
single crystal superalloys
|
gptkbp:first_flight
|
gptkb:1988
|
gptkbp:fuel_capacity
|
improved over predecessors
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label
|
International Aero Engines V2500
|
gptkbp:is_tested_for
|
International Aero Engines test facility
|
gptkbp:length
|
2.8 m
|
gptkbp:maintenance
|
6,000 hours
scheduled maintenance programs
|
gptkbp:manufacturer
|
gptkb:International_Aero_Engines
|
gptkbp:market
|
approximately 30% of the A320 family engines
|
gptkbp:noise_level
|
Stage 3 compliant
advanced design features
|
gptkbp:operational_area
|
competitive
commercial aviation
|
gptkbp:produced_by
|
over 6,000 engines
|
gptkbp:propulsion
|
22,000 to 33,000 lbf
|
gptkbp:rating
|
high performance
|
gptkbp:reliability
|
high
|
gptkbp:services
|
gptkb:1990
|
gptkbp:setting
|
dual-spool
|
gptkbp:upgrades
|
performance upgrades available
|
gptkbp:variant
|
gptkb:V2500-A5
gptkb:V2500-A1
gptkb:V2500-E5
|
gptkbp:weight
|
1,200 kg
|