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FAA AD on General Electric Company (GE) CF6- 80C2B5F turbofan engines (2009-14-08)

Washington, Usa - To prevent HPCR stages 11-14 spool/shaft fatigue cracks caused by exceeding the life limit, which could result in a possible uncontained failure of the HPCR spool/shaft and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 125)] [Page 31350-31351] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2009-0121; Directorate Identifier 2008-NE-36-AD; Amendment 39-15958; AD 2009-14-08] RIN 2120-AA64 Airworthiness Directives; General Electric Company...

fra/pec - 1106661
Rome, Italy, 07/03/2009 11:50
AVIONEWS - World Aeronautical Press Agency

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