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FAA AD on Boeing model 747 airplanes (2009-12-08)
Washington, Usa - To detect and correct fatigue cracking of the longeron, which can propagate and cause damage to the adjacent horizontal stabilizer pivot bulkhead and could result in loss of structural integrity
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Airworthiness Directive Federal Register Information [Federal Register: (Volume 74, Number 111)] [Page 27693-27695] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2008-0612; Directorate Identifier 2008-NM-059-AD; Amendment 39-15931; AD 2009-12-08] RIN 2120-AA64 Airworthiness Directives; Boeing Model 747 Airplanes...
fra/pec - 1106008
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency