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FAA AD on General Electric Company (GE) CF6-80A series turbofan engines (2009-08-06)
Washington, Usa - To prevent cracks developing at the aft chamfer of the blade dovetail slots that could propagate to a failure of the disk and cause an uncontained engine failure and damage to the airplane
Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 69)] [Page 16754-16755] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0827; Directorate Identifier 2008-NE-26-AD; Amendment 39-15879; AD 2009-08-06] RIN 2120-AA64 Airworthiness Directives; General Electric Company...
fra/pec - 1103688
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency