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FAA AD on McDonnell Douglas Model DC-8-33, DC-8- 51, DC-8-53, DC-8-55, DC-8F-54, DC-8F-55, DC-8-63, DC-8-62F, DC-8-63F, DC-8-71, DC-8-73, DC-8-71F, DC-8-72F, and DC-8-73F airplanes

Washington, Usa - To detect and correct fatigue cracks in the fuselage skin, which could result in rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: February 6, 2006 (Volume 71, Number 24)] [Page 5969-5971] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-22425; Directorate Identifier 2005-NM-066-AD; Amendment 39-14468; AD 2006-03-04] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 135508
Rome, Italy, 02/07/2006 12:17
AVIONEWS - World Aeronautical Press Agency

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