# Airworthiness Directives; Agusta S.p.A. Model A109A and A109A II Helicopters
> **Rule** · Final rule. · Published 2008-11-25 · Effective 2008-12-30 · 73 FR 71526
## Document
- **Document number:** E8-27611
- **Category:** airworthiness
- **Manufacturer:** Agusta S.p.A. Model A109A and A109A II
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 73 FR 71526
- **Publication date:** 2008-11-25
- **Effective date:** 2008-12-30
- **FAA docket:** Docket No. FAA-2008-0834
## Abstract

This amendment supersedes an existing airworthiness directive (AD) for the specified Agusta S.p.A. (Agusta) model helicopters. This AD results from a revised mandatory continuing airworthiness information (MCAI) issued by an aviation authority to identify and correct an unsafe condition on an aviation product. The aviation authority of Italy, with which we have a bilateral agreement, reports that the previous MCAI should not apply to newly redesigned and improved tail rotor blades. This AD requires the same inspections as the current AD but limits the applicability to only three part-numbered tail rotor blades. This AD requires actions that are intended to prevent fatigue failure of a tail rotor blade (blade), loss of a tail rotor, and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2008/11/25/E8-27611/airworthiness-directives-agusta-spa-model-a109a-and-a109a-ii-helicopters)
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