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FAA AD on Airbus model A-340/211, -212, -311, and -312 airplanes (2007-12-08)

Washington, Usa - To prevent discrepancies of the fastener holes of the horizontal flange of the keel beam, which could result in reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: June 6, 2007 (Volume 72, Number 108)] [Page 31171-31174] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-28354; Directorate Identifier 2006-NM-245-AD; Amendment 39-15086; AD 2007-12-08] RIN 2120-AA64 Airworthiness Directives; Airbus...

fra/pec - 1075098

AVIONEWS - World Aeronautical Press Agency
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