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FAA AD on General Electric Company CF34-3A1 turbofan engines

Washington, Usa - To impose life limits on these HPT rotating components to prevent low cycle fatigue (LCF) cracking and failure of those components, which could result in uncontained engine failure and damage to the airplane

Airworthiness Directive Federal Register Information [Federal Register: September 8, 2005 (Volume 70, Number 173)] [Page 53295-53296] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18869; Directorate Identifier 2004-NE-23-AD; Amendment 39-14256; AD 2005-18-16] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 126529
Rome, Italy, 09/09/2005 12:51
AVIONEWS - World Aeronautical Press Agency

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