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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

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
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