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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

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
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