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FAA AD on McDonnell Douglas model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43; DC-8F-54, DC-8F-55; DC-8-50, -60, - 60F, -70, and -70F and other airplanes
Washington, Usa - To prevent failure of the rudder pedal bracket assembly, which could result in the loss of rudder and braking control at either the captain’s or first officer’s position
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Airworthiness Directive Federal Register Information [Federal Register: April 11, 2006 (Volume 71, Number 69)] [Page 18201-18205] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20797; Directorate Identifier 2004-NM-256-AD; Amendment 39-14552; AD 2006-07-25] RIN 2120-AA64 Airworthiness Directives; McDonnell...
fra/pec - 139126
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency