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FAA AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-200C, 747-300, 747-400, 747-400D, and 747SR series airplanes (2006-12-12)
Washington, Usa - To detect and correct fatigue cracks that could extend and fully sever the frame, which could result in development of skin cracks that could lead to rapid depressurization of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: June 12, 2006 (Volume 71, Number 112)] [Page 33595-33598] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-24102; Directorate Identifier 2005-NM-244-AD; Amendment 39-14638; AD 2006-12-12] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 142662
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency