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FAA AD on Airbus model A-321-100 series airplanes (2006-04-11)
Washington, Usa - To detect and correct fatigue cracking on the inner rear spar of the wings, which could result in reduced structural integrity of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: February 21, 2006 (Volume 71, Number 34)] [Page 8792-8796] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23935; Directorate Identifier 2005-NM-060-AD; Amendment 39-14492; AD 2006-04-11] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 136347
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency