|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:airlines
|
2,000 lb/min
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:certifications
|
gptkb:FAA
Stage 4
|
|
gptkbp:climate
|
up to 1,500 °F
|
|
gptkbp:controls
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
68 in
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:engine
|
pylon-mounted
|
|
gptkbp:engineConfiguration
|
twin_spool
|
|
gptkbp:engineType
|
gptkb:CF6-80C2B6F10
gptkb:CF6-80C2B6F1
gptkb:CF6-80C2B6F12
gptkb:CF6-80C2B6F5
gptkb:CF6-80C2B6F14
gptkb:CF6-80C2B6F2
gptkb:CF6-80C2B1F
gptkb:CF6-80C2B6F8
gptkb:CF6-80C2B1F1
gptkb:CF6-80C2B6F4
gptkb:CF6-80C2B6F9
axial
high bypass ratio
1,600 °F
CF6-80C2B6F11
CF6-80C2B6F13
CF6-80C2B6F15
CF6-80C2B6F3
CF6-80C2B6F7
|
|
gptkbp:firstFlight
|
1982
|
|
gptkbp:fuel_capacity
|
0.5 lb/lbf/hr
1,200 lb/hr
|
|
gptkbp:fuelType
|
Jet A
annular
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CF6-80C2B6F16
|
|
gptkbp:length
|
150 in
|
|
gptkbp:maintenance
|
6,000 hours
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:notableUsers
|
gptkb:Airbus_A330
gptkb:Boeing_767
McDonnell Douglas MD-11
|
|
gptkbp:number_of_stages
|
compressor: 10
fan: 3
turbine: 2
|
|
gptkbp:propulsion
|
60,000 lbf
|
|
gptkbp:related_engine
|
CF6
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:weight
|
4,000 lb
|