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FAA AD on Airbus model A-310/200 and -300 series airplanes (2006-10-11)
Washington, Usa - To detect and correct cracking of the flap transmission shaft, which could compromise shaft structural integrity and lead to a disabled flap transmission shaft and reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: May 16, 2006 (Volume 71, Number 94)] [Page 28254-28256] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24104; Directorate Identifier 2005-NM-231-AD; Amendment 39-14595; AD 2006-10-11] RIN 2120-AA64 Airworthiness Directives; Airbus...
fra/pec - 141099
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency