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FAA AD on Boeing model 747-200B, -200C, -200F, and -400F series airplanes (2005-08-09)
Washington, Usa - To find and fix fatigue cracking of the fuselage frame, which could result in reduced structural integrity of the frame and consequent rapid decompression of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: April 19, 2005 (Volume 70, Number 74)] [Page 20273-20275] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20136; Directorate Identifier 2004-NM-185-AD; Amendment 39-14061; AD 2005-08-09] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 118965
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency