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FAA AD on Airbus model A-330/200 and -300, and A-340/200 and -300 series airplanes
Washington, Usa - To prevent a decrease in the torque limiter function, which could result in degradation and damage to the attachment bolts of the leading edge slat, loss of the slat, and consequent reduced control of the airplane
Airworthiness Directive Federal Register Information [Federal Register: July 17, 2006 (Volume 71, Number 136)] [Page 40387-40389] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24522; Directorate Identifier 2006-NM-002-AD; Amendment 39-14680; AD 2006-14-09] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 145299
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency