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FAA (Revision) AD on Boeing model 747-100, 747-100B, 747- 100B SUD, 747-200B, 747-300, 747-400, 747-400D, and 747SR series airplanes (2006-09-06 R1)
Washington, Usa - To detect and correct fatigue cracking of certain lower lobe fuselage frames, which could lead to fatigue cracks in the fuselage skin, and consequent rapid decompression of the airplane
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Airworthiness Directive Federal Register Information [Federal Register: December 7, 2006 (Volume 71, Number 235)] [Page 70857-70859] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-25327; Directorate Identifier 2006-NM-116-AD; Amendment 39-14842; AD 2006-09-06 R1] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 71091
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency