Summary
We are superseding an existing airworthiness directive (AD) for all GE CF6-80C2B series turbofan engines. That AD currently requires installing software version 8.2.Q1 to the engine electronic control unit (ECU), which increases the engine's margin to flameout. This new AD requires the removal of the affected ECUs from service. This AD was prompted by two reports of engine flameout events during flight in inclement weather conditions, eight reports of engine in- flight shutdown (IFSD) events caused by dual-channel central processing unit (CPU) faults in the ECU, and four reports of engine flameout ground events. We are issuing this AD to prevent engine flameout or un- commanded engine IFSD of one or more engines, leading to an emergency or forced landing of the airplane.
Directive Details
AD Number
FAA-2006-25738
Document Number
2012-4284
Type
Rule
Publication Date
February 24, 2012
Effective Date
March 30, 2012
Affected Manufacturer
General Electric Company (GE) Turbofan
Criticality
critical
Emergency
Yes
Docket ID
Docket No. FAA-2006-25738
Topics
Official Documents
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