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FAA AD on Boeing model 777-200 and -300 series airplanes (2005-10-17)
Washington, Usa - To prevent fatigue cracks in the lower t-chord at the bolt holes common to the paddle fittings that could result in fractures of one or more of the t-chord segments, which could lead to detachment of the lower wing panel and consequent
Airworthiness Directive Federal Register Information [Federal Register: May 19, 2005 (Volume 70, Number 96)] [Page 28797-28800] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-214-AD; Amendment 39-14094; AD 2005-10-17] RIN 2120-AA64 Airworthiness Directives; Boeing Model 777-200 and -300 Series...
fra/pec - 120881
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency