# Airworthiness Directives; Airbus Model A320-111 Airplanes, and Model A320-200 Series Airplanes
> **Rule** · Final rule; correction. · Published 2005-12-29 · Effective 2005-12-05 · 70 FR 76973
## Document
- **Document number:** 05-24525
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A320-111
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 70 FR 76973
- **Publication date:** 2005-12-29
- **Effective date:** 2005-12-05
- **FAA docket:** Docket No. 2002-NM-298-AD
## Abstract

This document corrects information in an existing airworthiness directive (AD) that applies to certain Airbus Model A320- 111 airplanes, and Model A320-200 series airplanes. That AD currently requires a detailed inspection of the tail cone triangle to determine its position, and corrective actions if necessary. This document corrects the applicability by specifying that the AD affects only airplanes identified in Airbus Service Bulletin A320-27-1132, Revision 01, dated June 19, 2002. This correction is necessary to ensure that only affected airplanes are subject to the requirements of the AD.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/12/29/05-24525/airworthiness-directives-airbus-model-a320-111-airplanes-and-model-a320-200-series-airplanes)
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