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FAA AD on Airbus model A-320 series airplanes (2004-25-03)
Washington, Usa - To detect and correct fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: January 6, 2005 (Volume 70, Number 4)] [Page 1182-1184] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18771; Directorate Identifier 2002-NM-313-AD; Amendment 39-13890; AD 2004-25-03] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 111591
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency