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FAA AD on McDonnell Douglas model DC-9-81, DC-9-82, DC-9-83, DC-9-87, and MD-88 airplanes (2008-13-29)
Washington, Usa - To detect and correct such cracking, which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplane
Airworthiness Directive Federal Register Information Federal Register: July 8, 2008 [Page 38883-38885] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-29335; Directorate Identifier 2007-NM-045-AD; Amendment 39-15592; AD 2008-13-29] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model DC-9-81...
fra/pec - 1092102
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency