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FAA AD (Correction) on Airbus model A-330, A-340/200, and A-340/300 series airplanes (2005-03-12)
Washington, Usa - To prevent fatigue failure of certain frame stiffener fittings, which could result in reduced structural integrity of the airplane
Airworthiness Directive Federal Register Information [Federal Register: February 14, 2005 (Volume 70, Number 29)] [Page 7386-7389] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-256-AD; Amendment 39-13968; AD 2005-03-12] RIN 2120-AA64 Airworthiness Directives; Airbus Model A330, A340-200, and...
fra/pec - 114288
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency