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FAA AD on McDonnell Douglas model DC-9-14, DC-9- 15, and DC-9-15F airplanes; DC-9-20, DC-9- 30, DC-9-40, and DC-9-50 series airplanes
Washington, Usa - To detect and correct fatigue cracks in the shock strut cylinder of the MLG, which could result in a collapsed MLG during takeoff or landing, and possible reduced structural integrity of the airplane
Airworthiness Directive Federal Register Information [Federal Register: September 16, 2005 (Volume 70, Number 179)] [Page 54616-54618] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21140; Directorate Identifier 2004-NM-274-AD; Amendment 39-14273; AD 2005-19-08] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 127143
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency