# Airworthiness Directives; Airbus Model A330, A340-200, and A340-300 Series Airplanes
> **Rule** · Final rule; correction. · Published 2005-03-11 · Effective 2005-03-21 · 70 FR 12119
## Document
- **Document number:** 05-4824
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 70 FR 12119
- **Publication date:** 2005-03-11
- **Effective date:** 2005-03-21
- **FAA docket:** Docket No. 2003-NM-256-AD
## Abstract

This document corrects a typographical error that appeared in airworthiness directive (AD) 2005-03-12 that was published in the Federal Register on February 14, 2005 (70 FR 7386). The typographical error resulted in an incorrect AD number. This AD is applicable to certain Airbus Model A330, A340-200, and A340-300 series airplanes. This AD requires initial and repetitive inspections of certain frame stiffeners to detect cracking and replacement of any cracked stiffener with a new, reinforced stiffener. Replacement of the stiffener constitutes terminating action for certain inspections. This AD also requires a one-time inspection of any new, reinforced stiffener; and repair or replacement of the new, reinforced stiffener if any cracking is found during the one-time inspection. This AD also provides for an optional terminating action for certain requirements of this AD.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/03/11/05-4824/airworthiness-directives-airbus-model-a330-a340-200-and-a340-300-series-airplanes)
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