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FAA AD on General Electric Company CF6-80E1 model turbofan engines
Usa - To prevent failure of HPT rotor blades from HPT S2 NGV distress, which could result in an uncontained engine failure
Airworthiness Directive Federal Register Information Federal Register Information [Federal Register: May 11, 2004 (Volume 69, Number 91)] [Page 26027-26029] Header Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NE-45-AD; Amendment 39-13625; AD 2004-09-34] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 63182
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency