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FAA AD on Airbus model A-321/100 series airplanes (2006-04-11R1)

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

Airworthiness Directive Federal Register Information [Federal Register: June 7, 2006 (Volume 71, Number 109)] [Page 32807-32811] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24953; Directorate Identifier 2006-NM-084-AD; Amendment 39-14628; AD 2006-04-11 R1] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 142380
Rome, Italy, 06/08/2006 15:33
AVIONEWS - World Aeronautical Press Agency

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