BELL 204B and certain Model 205A-1 helicopters [Docket No. FAA-2013-0379; Directorate Identifier 2009-SW-26-AD; Amendment 39-17580; AD 2013-18-07] – supersedes AD 76-12-07 for affected helicopters with a certain tail rotor pitch control chain installed. AD 76-12-07 required visually inspecting the...

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