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routineRule

AD FAA-2007-28172

Airworthiness Directives; General Electric Company (GE) CF6-80C2A5F Turbofan Engines

Summary

The FAA is adopting a new airworthiness directive (AD) for GE CF6-80C2A5F turbofan engines installed on, but not limited to, Airbus A300F4-605R 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 the potential of an all-engine flameout event caused by ice accretion and shedding during flight.

Directive Details

AD Number

FAA-2007-28172

Document Number

E7-20036

Type

Rule

Publication Date

October 11, 2007

Effective Date

November 15, 2007

Affected Manufacturer

General Electric Company (GE) CF6-80C2A5F Turbofan

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2007-28172

Topics

Air transportationAircraftAviation safetySafety

Official Documents

View all ADs for General Electric Company (GE) CF6-80C2A5F Turbofan →

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