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FAA AD on General Electric Company CF6-80C2 series and CF6-80E1 series turbofan engines (2008-21-11)
Washington, Usa - To prevent loss of the mount system structural integrity could result in the engine separating from the airplane
Airworthiness Directive Federal Register Information [Federal Register: (Volume 73, Number 207)] [Page 63354-63357] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-28367; Directorate Identifier 2007-NE-19-AD; Amendment 39-15695; AD 2008-21-11] RIN 2120-AA64 Airworthiness Directives; General Electric Company...
fra/pec - 1095767
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency