# Airworthiness Directives; Airbus Airplanes
> **Rule** · Final rule. · Published 2018-07-18 · Effective 2018-08-22 · 83 FR 33821
## Document
- **Document number:** 2018-13220
- **Category:** airworthiness
- **Manufacturer:** Airbus
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 83 FR 33821
- **Publication date:** 2018-07-18
- **Effective date:** 2018-08-22
- **FAA docket:** Docket No. FAA-2018-0111
## Abstract

We are superseding Airworthiness Directive (AD) 2017-07-07, which applied to certain Airbus Model A330-200, A330-300, A340-200, and A340-300 series airplanes. AD 2017-07-07 required repetitive inspections of certain fastener holes, and related investigative and corrective actions if necessary. This AD retains the requirements of AD 2017-07-07 and expands the applicability. This AD was prompted by a report of cracking at fastener holes located at frame (FR) 40 on the lower shell panel junction. We are issuing this AD to address the unsafe condition on these products.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2018/07/18/2018-13220/airworthiness-directives-airbus-airplanes)
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