# Proposed AD FAA-2012-1034: Airbus Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2013-05-11
- Products: Airbus
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: October 2, 2012, 77 FR 60064
- Comments due: November 16, 2012
- Became: [AD 2013-05-11](https://openairdocs.org/ad/2013-05-11)
- Docket: FAA-2012-1034 (https://www.regulations.gov/docket/FAA-2012-1034, where comments are filed)
- Project: 2011-NM-051-AD
- FR document: 2012-24175
- Official PDF: https://openairdocs.org/files/sha256/86/4a/864af1114eb22f5313facbbf7d67c747def174c990493cd81aa5af63964d94da (from https://www.govinfo.gov/content/pkg/FR-2012-10-02/pdf/2012-24175.pdf)
- Federal Register: https://www.federalregister.gov/documents/2012/10/02/2012-24175/airworthiness-directives-airbus-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2EE81FE90966883286257A8B0052FB52.0001
- Page: https://openairdocs.org/proposed/FAA-2012-1034

## Summary

We propose to supersede an existing airworthiness directive (AD) that applies to certain Airbus Model A318, A319, A320, and A321 series airplanes. The existing AD currently requires one-time and repetitive inspections of specific areas and, when necessary, corrective actions for those rudders where production rework has been identified. Since we issued that AD, we have determined that additional inspections and corrective actions are necessary to address the identified unsafe condition, and that additional airplanes with certain rudders are subject to the identified unsafe condition. This proposed AD would add airplanes with certain rudders to the AD applicability; change an inspection type for certain reinforced rudder areas; require pre-inspections and repairs if needed; and require permanent restoration of vacuum loss holes. This proposed AD would also require additional inspections for certain rudders and repair if needed; and require replacement of certain rudders with new rudders. We are proposing this AD to detect and correct extended de-bonding, which might degrade the structural integrity of the rudder. The loss of the rudder leads to degradation of the handling qualities and reduces the controllability of the airplane.

## Notices in this docket

- Oct 2, 2012: Notice of proposed rulemaking (NPRM). (first notice), FR document 2012-24175, comments due Nov 16, 2012 (https://www.federalregister.gov/documents/2012/10/02/2012-24175/airworthiness-directives-airbus-airplanes)

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