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FAA AD on Airbus model A-300B4-600, B4-600R, and F4-600R series airplanes, and model C4-605R Variant F airplanes (2007-12-04)

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: June 5, 2007 (Volume 72, Number 107)] [Page 30961-30966] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-26856; Directorate Identifier 2006-NM-125-AD; Amendment 39-15082; AD 2007-12-04] RIN 2120-AA64 Airworthiness Directives; Airbus...

fra/pec - 1074958
Rome, Italy, 06/06/2007 15:09
AVIONEWS - World Aeronautical Press Agency

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