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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

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
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