|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:airlines
|
1,200 lb/s
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:certifications
|
gptkb:EASA
gptkb:FAA
NOx compliant
|
|
gptkbp:climate
|
1,600 °F
|
|
gptkbp:compressionRatio
|
5.5:1
|
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:developer
|
gptkb:CF6-80C2B1F10
gptkb:CF6-80C2B1F4
gptkb:CF6-80C2B1F16
gptkb:CF6-80C2B1F13
gptkb:CF6-80C2B1F12
gptkb:CF6-80C2B1F
gptkb:CF6-80C2B1F3
gptkb:CF6-80C2B1F14
gptkb:CF6-80C2B1F18
gptkb:CF6-80C2B1F6
gptkb:CF6-80C2B1F1
gptkb:CF6-80C2B1F19
gptkb:CF6-80C2B1F5
gptkb:CF6-80C2B1F20
gptkb:CF6-80C2B1F8
CF6-80C2B1F11
CF6-80C2B1F15
CF6-80C2B1F17
CF6-80C2B1F2
CF6-80C2B1F7
CF6-80C2B1F9
|
|
gptkbp:diameter
|
68 in
60 in
|
|
gptkbp:engine
|
pylon mounted
|
|
gptkbp:engineConfiguration
|
twin_spool
|
|
gptkbp:engineType
|
axial
high bypass ratio
air start
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B6E18
|
|
gptkbp:length
|
156 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
McDonnell Douglas MD-11
|
|
gptkbp:number_of_stages
|
9
|
|
gptkbp:propulsion
|
cascade
18,500 lbf
|
|
gptkbp:related_engine
|
gptkb:CF6-80C2
CF6
|
|
gptkbp:service_ceiling
|
42,000 ft
|
|
gptkbp:weight
|
3,000 lb
|