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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
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