# Airworthiness Directives; The Boeing Company Model MD-90-30 Airplanes
> **Rule** · Final rule. · Published 2011-01-05 · Effective 2011-02-09 · 76 FR 430
## Document
- **Document number:** 2010-32993
- **Category:** airworthiness
- **Manufacturer:** The Boeing Company Model MD-90-30
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 76 FR 430
- **Publication date:** 2011-01-05
- **Effective date:** 2011-02-09
- **FAA docket:** Docket No. FAA-2010-0953
## Abstract

We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires repetitive high frequency eddy current inspections for cracking on the hinge bearing lugs of the left and right sides of the center section ribs of the horizontal stabilizer, and related investigative and corrective actions if necessary. This AD was prompted by reports of cracks found on either the left or right (or in one case, both) sides of the center section ribs of the horizontal stabilizer. We are issuing this AD to detect and correct cracking in the hinge bearing lugs of the center section of the left and right ribs, which could result in failure of the hinge bearing lugs and consequent inability of the horizontal stabilizer to sustain the required loads.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2011/01/05/2010-32993/airworthiness-directives-the-boeing-company-model-md-90-30-airplanes)
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