# Proposed AD FAA-2014-0574: Airbus Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2015-22-10
- Products: Airbus
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: August 22, 2014, 79 FR 49724
- Comments due: October 6, 2014
- Became: [AD 2015-22-10](https://openairdocs.org/ad/2015-22-10)
- Docket: FAA-2014-0574 (https://www.regulations.gov/docket/FAA-2014-0574, where comments are filed)
- Project: 2013-NM-258-AD
- FR document: 2014-19979
- Official PDF: https://openairdocs.org/files/sha256/f7/59/f7598dfd39ed2e3a456dffefab5a8178ac670d9e8be8956910e1c000cc2f121c (from https://www.govinfo.gov/content/pkg/FR-2014-08-22/pdf/2014-19979.pdf)
- Federal Register: https://www.federalregister.gov/documents/2014/08/22/2014-19979/airworthiness-directives-airbus-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D7093800575894C586257D3C0043E461.0001
- Page: https://openairdocs.org/proposed/FAA-2014-0574

## Summary

We propose to adopt a new airworthiness directive (AD) for all Airbus Model A318 series airplanes, Model A319 series airplanes, Model A320-211, -212, -214, -231, -232, and -233 airplanes, and Model A321 series airplanes. This proposed AD was prompted by a report of skin disbonding on a composite side shell panel of a rudder. This proposed AD would require an inspection to determine if any rudder composite side shell panel has been repaired, a thermography inspection of each rudder that has received this repair, and related investigative and corrective actions if necessary. We are proposing this AD to detect and correct skin disbonding on the rudder, which could affect the structural integrity of the rudder, possibly resulting in reduced control of the airplane.

## Notices in this docket

- Aug 22, 2014: Notice of proposed rulemaking (NPRM). (first notice), FR document 2014-19979, comments due Oct 6, 2014 (https://www.federalregister.gov/documents/2014/08/22/2014-19979/airworthiness-directives-airbus-airplanes)

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