# Airworthiness Directives; Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, and 230 Helicopters
> **Rule** · Final rule. · Published 2000-05-22 · 65 FR 32021
## Document
- **Document number:** 00-12818
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 32021
- **Publication date:** 2000-05-22
- **FAA docket:** Docket No. 99-SW-43-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) for BHTC Model 222, 222B, 222U, and 230 helicopters that requires inspecting each flapping bearing to yoke attachment bolt (bolt) and replacing each bolt that shows thread damage, shank wear, or corrosion pitting with an airworthy bolt. This amendment is prompted by the discovery of a fractured bolt during a post-flight inspection. The actions specified by this AD are intended to prevent a fracture of a bolt, failure of the bearing and yoke interface, and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/05/22/00-12818/airworthiness-directives-bell-helicopter-textron-canada-bhtc-model-222-222b-222u-and-230-helicopters)
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