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FAA AD on Airbus model A-320/111 airplanes (2005-20-35)

Washington, Usa - To detect and correct fatigue cracking of the upper stringers of the center wing box, which could lead to loss of structural integrity of the wing

Airworthiness Directive Federal Register Information [Federal Register: October 12, 2005 (Volume 70, Number 196)] [Page 59229-59231] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22626; Directorate Identifier 2002-NM-295-AD; Amendment 39-14332; AD 2005-20-35] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 128885
Rome, Italy, 10/13/2005 14:34
AVIONEWS - World Aeronautical Press Agency

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