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FAA AD on Airbus model A-318/100 and A-319/100; A-320/111; and A-320/200, A-321/100, A-321/200 (2006-07-09)
Washington, Usa - To ensure the integrity of the THSA's primary load path, which if failed, could result in an eventual failure of the THSA's secondary load path and consequent uncontrolled movement of the horizontal stabilizer and loss of control
Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16203-16206] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22794; Directorate Identifier 2005-NM-097-AD; Amendment 39-14536; AD 2006-07-09] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 138762
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency