# Airworthiness Directives; MD Helicopters, Inc., Model 369, YOH-6A, 369A, OH-6A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, and 369FF Helicopters
> **Rule** · Final rule; request for comments. · Published 2007-06-19 · Effective 2007-07-05 · 72 FR 33642
## Document
- **Document number:** E7-11409
- **Category:** airworthiness
- **Manufacturer:** MD
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 72 FR 33642
- **Publication date:** 2007-06-19
- **Effective date:** 2007-07-05
- **FAA docket:** Docket No. FAA-2007-28449
## Abstract

This document publishes in the Federal Register an amendment adopting Airworthiness Directive (AD) 2007-09-51, sent previously to all known U.S. owners and operators of the specified MD Helicopters, Inc. (MDHI), model helicopters by individual letters. This AD requires, before further flight, removing each affected tail rotor blade assembly and inspecting the bore of the tail rotor blade root fitting. If the blade assembly does not have a smooth radius, the AD requires replacing it. The AD also requires identifying each airworthy tail rotor blade assembly with the applicable helicopter model. This amendment is prompted by a report of an accident after the loss of a tail rotor blade. The actions specified by this AD are intended to prevent the failure of a tail rotor blade and subsequent loss of control of the helicopter.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2007/06/19/E7-11409/airworthiness-directives-md-helicopters-inc-model-369-yoh-6a-369a-oh-6a-369h-369hm-369hs-369he-369d)
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