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FAA AD on McDonnell Douglas model DC-10-10 and DC-10-10F; DC-10-15; DC-10-30 and DC- 10-30F; DC-10-40 and DC-10-40F; MD-10-10F and MD-10-30F; MD-11 and MD-11F airplanes
Washington, Usa - To prevent failure of a rudder pedal torque tube, which could result in loss of rudder control and nose wheel steering controlled by the rudder pedal, and consequent reduced controllability of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: October 6, 2005 (Volume 70, Number 193)] [Page 58305-58307] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21594; Directorate Identifier 2005-NM-067-AD; Amendment 39-14309; AD 2005-20-15] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 128516
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency