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FAA AD on Airbus model A-330/301, -321, -322, - 341, and -342 airplanes; A-340/200 and A-340/300 series airplanes

Washington, Usa - To detect and correct fatigue cracking in the vertical web of the wing rear spar, which could result in reduced structural integrity of the wing

Airworthiness Directive Federal Register Information [Federal Register: October 3, 2005 (Volume 70, Number 190)] [Page 57493-57497] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22485; Directorate Identifier 2001-NM-337-AD; Amendment 39-14293; AD 2005-19-28] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 128190
Rome, Italy, 10/04/2005 13:18
AVIONEWS - World Aeronautical Press Agency

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