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FAA AD on General Electric Company CT64-820-4 turboprop engines

Washington, Usa - To prevent uncontained failure of the stage 1 turbine disk and shaft, resulting in damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: June 21, 2005 (Volume 70, Number 118)] [Page 35523-35525] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21586; Directorate Identifier 2005-NE-16-AD; Amendment 39-14148; AD 2005-13-11] RIN 2120-AA64 Airworthiness Directives; General...

fra/pec - 122553
Rome, Italy, 06/22/2005 13:03
AVIONEWS - World Aeronautical Press Agency

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