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FAA AD on Boeing model 737-100, -200, -200C, - 300, -400, and -500 series airplanes (2005-19-25)
Washington, Usa - To detect and correct fatigue cracks of the countersunk rivet holes, which could result in cracks of the fuselage skin of the lower lobe, and consequent rapid depressurization of the cabin
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Airworthiness Directive Federal Register Information [Federal Register: September 27, 2005 (Volume 70, Number 186)] [Page 56351-56355] Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2005-20627; Directorate Identifier 2004-NM-39-AD; Amendment 39-14290; AD 2005-19-25] RIN 2120-AA64 Airworthiness Directives;...
fra/pec - 127900
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency