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FAA AD on Boeing model 747 airplanes (2006-22-15)
Washington, Usa - To prevent fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid decompression of the airplane
Airworthiness Directive Federal Register Information [Federal Register: November 6, 2006 (Volume 71, Number 214)] [Page 64884-64887] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23921; Directorate Identifier 2005-NM-205-AD; Amendment 39-14812; AD 2006-22-15] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 68505
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency