Summary
The FAA is adopting a new airworthiness directive (AD) for GE CF6-80C2D1F turbofan engines, installed on, but not limited to, McDonnell Douglas Corporation MD-11 series airplanes. This AD requires removing previous software versions from the engine electronic control unit (ECU). Engines with new version software will have increased margin to flameout. This AD results from reports of engine flameout events during flight, including reports of events where all engines simultaneously experienced a flameout or other adverse operation. Although the root cause investigation is not yet complete, we believe that exposure to ice crystals during flight is associated with these flameout events. We are issuing this AD to minimize engine flameout caused by ice accretion and shedding during flight.
Directive Details
AD Number
FAA-2007-28319
Document Number
E7-20813
Type
Rule
Publication Date
October 24, 2007
Effective Date
November 28, 2007
Affected Manufacturer
General Electric Company (GE) CF6-80C2D1F Turbofan
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2007-28319
Topics
Official Documents
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