|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:certifications
|
gptkb:EASA
gptkb:FAA
Stage 4
|
|
gptkbp:climate
|
1,500 °F
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
68 in
112 in
|
|
gptkbp:engineType
|
2
axial
high bypass ratio
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
gptkbp:historicalEvent
|
derived_from_CF6-50
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B6E5
|
|
gptkbp:length
|
150 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:market_segment
|
wide-body aircraft
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
|
|
gptkbp:number_of_stages
|
10
6
|
|
gptkbp:propulsion
|
15:1
60,000 lbf
|
|
gptkbp:related_engine
|
gptkb:CF6-80C2B1F
gptkb:CF6-80E1
gptkb:CF6-80C2
gptkb:CF6-80C2B1F1
CF6
|
|
gptkbp:reliability
|
high
|
|
gptkbp:serviceType
|
1983
|
|
gptkbp:weight
|
4,000 lb
|