CF6-80A
E558265
The CF6-80A is an early, high-bypass turbofan variant in General Electric’s CF6 engine family, developed primarily to power wide-body commercial airliners.
Statements (40)
| Predicate | Object |
|---|---|
| instanceOf | turbofan engine ⓘ |
| application |
Airbus A310
NERFINISHED
ⓘ
Boeing 767-200 NERFINISHED ⓘ |
| bypassRatio | high bypass ⓘ |
| certificationAuthority | FAA NERFINISHED ⓘ |
| configuration |
axial-flow
ⓘ
twin-spool ⓘ |
| coolingMethod | air-cooled turbine blades ⓘ |
| countryOfOrigin |
United States of America
ⓘ
surface form:
United States
|
| designFeature |
annular combustor
ⓘ
high overall pressure ratio ⓘ multi-stage high-pressure compressor ⓘ multi-stage low-pressure turbine ⓘ single-stage fan ⓘ |
| developedFor | wide-body commercial airliners ⓘ |
| emissionsStandard | civil aviation turbofan regulations ⓘ |
| engineControl | hydromechanical control system ⓘ |
| familyPosition | predecessor to CF6-80C2 series ⓘ |
| familyRole | first CF6-80 series variant ⓘ |
| fuelType | Jet-A kerosene-based aviation fuel ⓘ |
| generation | early CF6-80 series variant ⓘ |
| intendedMounting | underwing pylon ⓘ |
| intendedUse | commercial transport ⓘ |
| manufacturer | General Electric NERFINISHED ⓘ |
| marketSegment | wide-body medium- to long-haul aircraft ⓘ |
| noiseCompliance | ICAO Chapter 3 capable ⓘ |
| operatorType | commercial airlines ⓘ |
| partOfFamily | General Electric CF6 NERFINISHED ⓘ |
| primaryCustomerSegment |
airlines operating Airbus A310
ⓘ
airlines operating early Boeing 767 variants ⓘ |
| relatedModel |
CF6-50
NERFINISHED
ⓘ
CF6-80A1 NERFINISHED ⓘ CF6-80A2 ⓘ CF6-80A3 NERFINISHED ⓘ |
| status | in service on legacy fleets ⓘ |
| successor |
CF6-80C
NERFINISHED
ⓘ
CF6-80C2 NERFINISHED ⓘ |
| thrustClass | approximately 48,000 lbf to 52,000 lbf ⓘ |
| thrustReverserCompatibility | target-type thrust reverser systems ⓘ |
| useCase | twin-engine wide-body aircraft ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.