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FAA AD on Airbus model A-310 series airplanes (2007-11-12)

Washington, Usa - To prevent corrosion between the scuff plates at exit and cargo doors and fatigue cracks originating from certain fastener holes located in adjacent structure, which could result in reduced structural integrity

Airworthiness Directive Federal Register Information [Federal Register: May 30, 2007 (Volume 72, Number 103)] [Page 29874-29879] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-26857; Directorate Identifier 2006-NM-126-AD; Amendment 39-15069; AD 2007-11-12] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 1074846
Rome, Italy, 06/04/2007 15:11
AVIONEWS - World Aeronautical Press Agency

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