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FAA AD on General Electric Company (GE) CF6-80C2 turbofan engines
Washington, Usa - To prevent blade separation from HPT S2 NGV distress, which could result in an uncontained engine failure
![](https://www.avionews.it/layout/elements/default.jpg)
Airworthiness Directive Federal Register Information [Federal Register: October 27, 2004 (Volume 69, Number 207)] [Page 62571-62574] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NE-43-AD; Amendment 39-13835; AD 2004-22-07] RIN 2120-AA64 Airworthiness Directives; General Electric Company (GE) CF6-80C2...
fra/pec - 106289
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency