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FAA AD on Boeing model 747 series airplanes (2005-09-02)

Washington, Usa - To detect and correct fatigue cracks in the top and side panel webs and stiffeners of the NWW, which could compromise the structural integrity of the NWW and could lead to the rapid decompression of the airplane

Airworthiness Directive Federal Register Information [Federal Register: April 25, 2005 (Volume 70, Number 78)] [Page 21141-21144] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-21027; Directorate Identifier 2005-NM-048-AD; Amendment 39-14070; AD 2005-09-02] RIN 2120-AA64 Airworthiness Directives;...

fra/pec - 119289
Rome, Italy, 04/26/2005 13:49
AVIONEWS - World Aeronautical Press Agency

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