Airworthiness Directives; General Electric Company (GE) Turbofan Engines
airworthiness · Rule · Final rule. · Published 2012-02-24 · Effective 2012-03-30 · 77 FR 10950
Document
Document number
2012-4284
Federal Register citation
77 FR 10950
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
General Electric Company (GE) Turbofan
Publication date
2012-02-24
Effective date
2012-03-30
FAA docket
Docket No. FAA-2006-25738
Abstract
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.