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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

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
Rome, Italy, 03/10/2006 12:57
AVIONEWS - World Aeronautical Press Agency

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