# Airworthiness Directives; Eurocopter France Model SA-365C, SA-365C1, SA-365C2, SA-365N, SA-365N1, AS-365N2, AS 365 N3, and SA-366G1 Helicopters
> **Rule** · Final rule; request for comments. · Published 2011-06-17 · Effective 2011-07-05 · 76 FR 35346
## Document
- **Document number:** 2011-14248
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 76 FR 35346
- **Publication date:** 2011-06-17
- **Effective date:** 2011-07-05
- **FAA docket:** Docket No. FAA-2011-0551
## Abstract

This amendment adopts a new airworthiness directive (AD) for the specified Eurocopter France (Eurocopter) helicopters. This action requires visually inspecting the adhesive bead between the bushing and the Starflex star (Starflex) arm for a crack, a gap, or loss of the adhesive bead, inspecting the Starflex arm ends for delamination, and replacing the Starflex if any of these conditions are found. This amendment is prompted by three cases of deterioration of a Starflex arm. In two of these cases, the deterioration caused high amplitude vibrations in flight, compelling the pilot to make a precautionary landing. The actions specified in this AD are intended to prevent failure of the Starflex, high-amplitude vibrations in flight, and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2011/06/17/2011-14248/airworthiness-directives-eurocopter-france-model-sa-365c-sa-365c1-sa-365c2-sa-365n-sa-365n1-as-365n2)
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