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FAA AD on McDonnell Douglas model DC-9-81, DC-9-82, DC-9-83, DC-9-87, MD-88, and MD- 90-30 airplanes (2006-07-11)
Washington, Usa - To prevent fatigue cracking of the aft attach fitting of the spoiler link and consequent reduced controllability of the airplane
Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16208-16211] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22062; Directorate Identifier 2003-NM-219-AD; Amendment 39-14538; AD 2006-07-11] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 138763
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency