# Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B, 222U, 230, and 430 Helicopters
> **Rule** · Final rule. · Published 2010-06-11 · Effective 2010-07-16 · 75 FR 33159
## Document
- **Document number:** 2010-11071
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 75 FR 33159
- **Publication date:** 2010-06-11
- **Effective date:** 2010-07-16
- **FAA docket:** Docket No. FAA-2008-0071
## Abstract

This amendment supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) helicopters, that currently requires certain checks and inspections of the tail rotor blades. If a crack is found, the existing AD requires replacing the tail rotor blade (blade) with an airworthy blade before further flight. This amendment requires the same checks and inspections of the blades until they are required to be replaced and removes certain serial numbered and specifically coded blades from the applicability of the AD. This amendment is prompted by the approved rework of certain blades and two newly redesigned blades, which, if installed, constitute terminating action for the inspection requirements. The actions specified by this AD are intended to detect a crack in a blade, and to prevent loss of a blade and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2010/06/11/2010-11071/airworthiness-directives-bell-helicopter-textron-canada-model-222-222b-222u-230-and-430-helicopters)
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