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FAA AD on Airbus model A-300 airplanes; and A-300B4-600, B4-600R, and F4-600R series airplanes, and C4-605R Variant F airplanes (2007-26-14)
Washington, USA - To detect and correct fatigue cracking of the left and right upper radius at frame 47, which could propagate and result in reduced structural integrity of the airplane
Airworthiness Directive Federal Register Information [Federal Register: January 16, 2008 (Volume 73, Number 11)] [Page 2803-2807] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-27926; Directorate Identifier 2006-NM-050-AD; Amendment 39-15316; AD 2007-26-14] RIN 2120-AA64To Airworthiness Directives; Airbus...
fra/pec - 1084627
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency