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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
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