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FAA AD on McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F airplanes
Washington, Usa - To prevent corrosion and subsequent cracking of studbolts, which could result in failure of the flap hinge fittings and their possible separation from the wing rear spar, and consequent reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: February 9, 2006 (Volume 71, Number 27)] [Page 6669-6673] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22503; Directorate Identifier 2005-NM-062-AD; Amendment 39-14477; AD 2006-03-13] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 135835
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency