# Airworthiness Directives; Airbus Model A318, A319, A320, and A321 Airplanes
> **Rule** · Final rule. · Published 2006-09-06 · Effective 2006-10-11 · 71 FR 52421
## Document
- **Document number:** E6-14623
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 52421
- **Publication date:** 2006-09-06
- **Effective date:** 2006-10-11
- **FAA docket:** Docket No. FAA-2006-24199
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Airbus Model A318, A319, A320, and A321 airplanes. This AD requires revising the Limitations section of the airplane flight manual (AFM); performing a one-time hardness test of certain ribs of the left- and right-hand engine pylons, as applicable, which would terminate the AFM limitations; and performing related corrective actions if necessary. This AD results from a report that certain stainless steel ribs installed in the engine pylon may not have been heat-treated during manufacture, which could result in significantly reduced structural integrity of the pylon. We are issuing this AD to detect and correct reduced structural integrity of the engine pylon, which could lead to separation of the engine from the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/09/06/E6-14623/airworthiness-directives-airbus-model-a318-a319-a320-and-a321-airplanes)
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