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FAA AD on McDonnell Douglas model DC-9-10, DC-9- 20, DC-9-30, DC-9-40, and DC-9-50 series airplanes (2006-07-08)
Washington, Usa - To detect and correct stress corrosion cracking of the main fuselage frame, which could result in extensive damage to adjacent structure and reduced structural integrity of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: March 31, 2006 (Volume 71, Number 62)] [Page 16201-16203] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-23197; Directorate Identifier 2005-NM-109-AD; Amendment 39-14535; AD 2006-07-08] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 138768
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency