Editing General Electric CF6 (section)

==== CF6-80C2 ====

For the CF6-80C2-A1, the fan diameter is increased to 93 in (2.36 m), with an airflow of 1750&nbsp;lb/s (790&nbsp;kg/s). Overall pressure ratio is 30.4, with a bypass ratio of 5.15. Static thrust is 59,000&nbsp;lb (263&nbsp;kN). An extra stage is added to the LP compressor, and a 5th to the LP turbine.<ref name=GECF6-80C2>{{cite web |url= http://www.geaviation.com/engines/commercial/cf6/cf6-80c2.html |title= CF6-80C2 Engine |publisher= GE Aviation |url-status= bot: unknown |archive-url= https://web.archive.org/web/20081121124612/http://www.geaviation.com/engines/commercial/cf6/cf6-80c2.html |archive-date= 2008-11-21 }}</ref>

The CF6-80C2 is currently certified on fifteen commercial and military [[widebody aircraft]] models including the [[Boeing 747-400]], and [[McDonnell Douglas MD-11]]. The CF6-80C2 is also certified for [[ETOPS|ETOPS-180]] for the [[Airbus A300]], [[Airbus A310]], [[Boeing 767]], [[Boeing KC-767|KC-767A/J]], [[Boeing E-767|E-767J]], [[Kawasaki C-2]], and (as the F138) the [[Lockheed C-5M Super Galaxy]] and [[VC-25A]].