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FAA AD on Airbus model A-310/203, -204, and -222 airplanes, and A-310/300 series airplanes

Washington, Usa - To prevent fatigue cracking of the frame foot run-outs, which could lead to rupture of the frame foot and cracking in adjacent frames and skin, and result in reduced structural integrity of the fuselage

Airworthiness Directive Federal Register Information [Federal Register: January 20, 2006 (Volume 71, Number 13)] [Page 3214-3215] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22810; Directorate Identifier 2005-NM-143-AD; Amendment 39-14458; AD 2006-02-06] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 134771
Rome, Italy, 01/23/2006 14:51
AVIONEWS - World Aeronautical Press Agency

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