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FAA AD on General Electric Company CF6-80C2 series turbofan engines
Washington, Usa - To prevent LCF cracking and failure of the HPT stage 1 disk due to exceeding the life limit, which could result in an uncontained engine failure and damage to the airplane
Airworthiness Directive Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NE-46-AD; Amendment 39-13557; AD 2004-07-13] RIN 2120-AA64 Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines PDF Copy (If Available): Preamble Information AGENCY:...
fra/pec - 61212
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency