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FAA AD on Airbus model A-318/111 and A-318/112 airplanes and model A-319, A-320, and A-321 airplanes (2007-20-05)
Washington, Usa - To detect and correct fatigue cracking, accidental damage, or corrosion in principal structural elements and to prevent failure of certain life limited parts, which could result in reduced structural integrity
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Airworthiness Directive Federal Register Information [Federal Register: October 3, 2007 (Volume 72, Number 191)] [Page 56262-56265] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27015; Directorate Identifier 2006-NM-169-AD; Amendment 39-15215; AD 2007-20-05] RIN 2120-AA64 Airworthiness Directives; Airbus...
fra/pec - 1080308
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency