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FAA AD on Boeing model 777 airplanes (2006-25-05)

Washington, Usa - To detect and correct corrosion, and prevent subsequent fatigue cracks, on the fuselage skin under the forward and aft wing-to-body fairings, which could result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: December 7, 2006 (Volume 71, Number 235)] [Page 70860-70862] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2006-23817; Directorate Identifier 2005-NM-176-AD; Amendment 39-14846; AD 2006-25-05] RIN 2120-AA64 Airworthiness Directives; Boeing...

fra/pec - 71088

AVIONEWS - World Aeronautical Press Agency
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