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FAA AD on Airbus model A-300 F4-600R series airplanes and model A-300 C4-605R Variant F airplanes (2006-14-06)

Washington, Usa - To prevent fatigue cracking of the fuselage skin, which could result in loss of the structural integrity of the fuselage and consequent rapid depressurization of the airplane

Airworthiness Directive Federal Register Information [Federal Register: July 7, 2006 (Volume 71, Number 130)] [Page 38515-38516] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24367; Directorate Identifier 2006-NM-041-AD; Amendment 39-14677; AD 2006-14-06] RIN 2120-AA64 Airworthiness Directives; Airbus...

fra/pec - 144476

AVIONEWS - World Aeronautical Press Agency
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