# Proposed AD FAA-2016-9498: Airbus Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2017-14-14
- Products: Airbus
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: December 16, 2016, 81 FR 91060
- Comments due: January 30, 2017
- Became: [AD 2017-14-14](https://openairdocs.org/ad/2017-14-14)
- Docket: FAA-2016-9498 (https://www.regulations.gov/docket/FAA-2016-9498, where comments are filed)
- Project: 2016-NM-105-AD
- FR document: 2016-29676
- Official PDF: https://openairdocs.org/files/sha256/54/cf/54cf9926b3c75592a29874cb929a155e69d0469e055974e2c017ca412fcac5f9 (from https://www.govinfo.gov/content/pkg/FR-2016-12-16/pdf/2016-29676.pdf)
- Federal Register: https://www.federalregister.gov/documents/2016/12/16/2016-29676/airworthiness-directives-airbus-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BF5A4E959E5B85858625808B005494FC.0001
- Page: https://openairdocs.org/proposed/FAA-2016-9498

## Summary

We propose to adopt a new airworthiness directive (AD) for all Airbus Model A321 series airplanes. This proposed AD was prompted by a determination from fatigue testing on the Model A321 airframe that cracks could develop in the cabin floor beam junction at certain fuselage frame locations. This proposed AD would require repetitive inspections for cracking in the cabin floor beam junction at certain fuselage frame locations, and repair if necessary. We are proposing this AD to address the unsafe condition on these products.

## Notices in this docket

- Dec 16, 2016: Notice of proposed rulemaking (NPRM). (first notice), FR document 2016-29676, comments due Jan 30, 2017 (https://www.federalregister.gov/documents/2016/12/16/2016-29676/airworthiness-directives-airbus-airplanes)

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