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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 (2007-16-08)

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

Airworthiness Directive Federal Register Information [Federal Register: August 9, 2007 (Volume 72, Number 153)] [Page 44728-44731] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2007-28015; Directorate Identifier 2006-NM-210-AD; Amendment 39-15147; AD 2007-16-08] RIN 2120-AA64 Airworthiness Directives; Boeing...

fra/pec - 1078084
Rome, Italy, 08/10/2007 15:14
AVIONEWS - World Aeronautical Press Agency

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