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FAA AD on Boeing model 747 airplanes (2006-05-06)
Washington, Usa - To prevent fatigue cracking of the BS 2598 bulkhead structure, which could result in inability of the structure to carry horizontal stabilizer flight loads, and loss of controllability of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: March 9, 2006 (Volume 71, Number 46)] [Page 12125-12129] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22715; Directorate Identifier 2005-NM-108-AD; Amendment 39-14503; AD 2006-05-06] RIN 2120-AA64 Airworthiness Directives; Boeing...
fra/pec - 137335
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency