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 ...

THIS CONTENT REQUIRES SUBSCRIPTION ACCESS

You must be a paid subscriber to access "BELL".

 

Current Aviation Week Intelligence Network (AWIN) enterprise and individual members: please go to http://awin.aviationweek.com for access.

 

Not currently a subscriber? Click on the "Learn More" button below to view subscription offers.

Already registered? here.