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FAA AD on Airbus model A-320 series airplanes (2004-25-02)

Washington, Usa - To detect and correct fatigue cracking of the fuselage, which could result in reduced structural integrity of the airplane

Airworthiness Directive Federal Register Information [Federal Register: January 6, 2005 (Volume 70, Number 4)] [Page 1184-1186] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2004-18773; Directorate Identifier 2002-NM-312-AD; Amendment 39-13889; AD 2004-25-02] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 111594
Rome, Italy, 01/10/2005 14:18
AVIONEWS - World Aeronautical Press Agency

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