BELL 205A-1, 205B, 210 and 212 helicopters [Docket No. FAA-2011-1182; Directorate Identifier 2010-SW-010-AD; Amendment 39-16853; AD 2011-23-02] – Conduct repetitive inspections of certain main-rotor blades for edge voids, corrosion or cracks. This new AD supersedes an existing directive (AD 2010-03-03), retaining the same requirements but increasing the scope and frequency of the inspections and expanding the applicability to include Model 205A-1 and 210 helicopters, additional blades, and ...
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