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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, DC-10-30F, DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F airplanes
Washington, Usa - To prevent failure of the rudder pedal arm assembly, which, under certain conditions, could result in reduced controllability of the airplane
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-207-AD; Amendment 39-13379; AD 2003-24-10] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC- 10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F (KC10A and KDC-10), DC-10-40, DC-10-40F,...
fra/pec - 55974
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency