# Airworthiness Directives; Airbus Airplanes
> **Rule** · Final rule. · Published 2017-06-06 · Effective 2017-07-11 · 82 FR 25936
## Document
- **Document number:** 2017-11129
- **Category:** airworthiness
- **Manufacturer:** Airbus
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 82 FR 25936
- **Publication date:** 2017-06-06
- **Effective date:** 2017-07-11
- **FAA docket:** Docket No. FAA-2016-8182
## Abstract

We are adopting a new airworthiness directive (AD) for all Airbus Model A318-111 and -112 airplanes; Model A319-111, -112, -113, - 114, and -115 airplanes; Model A320-211, -212, and -214 airplanes; and Model A321-111, -112, -211, -212, and -213 airplanes. This AD was prompted by reports of cracks in certain pivot fittings of a CFM56 engine's thrust reverser (T/R). This AD requires repetitive inspections for cracking and corrosion of certain pivot fittings of a CFM56 engine's T/R, and corrective actions if necessary. We are issuing this AD to address the unsafe condition on these products.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2017/06/06/2017-11129/airworthiness-directives-airbus-airplanes)
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