# Airworthiness Directives; Airbus SAS Airplanes
> **Rule** · Final rule. · Published 2019-11-13 · Effective 2019-12-18 · 84 FR 61526
## Document
- **Document number:** 2019-24508
- **Category:** airworthiness
- **Manufacturer:** Airbus SAS
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 84 FR 61526
- **Publication date:** 2019-11-13
- **Effective date:** 2019-12-18
- **FAA docket:** Docket No. FAA-2019-0254
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A318 and A319 series airplanes, Model A320- 211, -212, -214, -216, -231, -232, and -233 airplanes, and Model A321- 111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This AD was prompted by a report that cracks were detected on frame (FR) 16 and FR 20 web holes and passenger door intercostal fitting holes at the door stop fitting locations. This AD requires repetitive rototest inspections of the holes at the door stop fittings for any cracking, and corrective actions if necessary, as specified in a European Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2019/11/13/2019-24508/airworthiness-directives-airbus-sas-airplanes)
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