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FAA AD (Correction) 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
Airworthiness Directive Federal Register Information [Federal Register: March 4, 2005 (Volume 70, Number 42)] [Page 10485] 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 Turbofan...
fra/pec - 115676
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency