# Proposed AD FAA-2005-22810: Airbus Model A310-203, -204, and -222 Airplanes, and Model A310-300 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-02-06
- Products: Airbus
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: October 27, 2005, 70 FR 61924
- Comments due: November 28, 2005
- Became: [AD 2006-02-06](https://openairdocs.org/ad/2006-02-06)
- Docket: FAA-2005-22810 (https://www.regulations.gov/docket/FAA-2005-22810, where comments are filed)
- Project: 2005-NM-143-AD
- FR document: 05-21428
- Official PDF: https://openairdocs.org/files/sha256/66/d8/66d8d6f92c6eec691aeac377192ee04bc41fe5deb7dd4ad6e5e9bee3642cc1cb (from https://www.govinfo.gov/content/pkg/FR-2005-10-27/pdf/05-21428.pdf)
- Federal Register: https://www.federalregister.gov/documents/2005/10/27/05-21428/airworthiness-directives-airbus-model-a310-203--204-and--222-airplanes-and-model-a310-300-series
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E58C3AADB43B10F0862570A700530D41.0001
- Page: https://openairdocs.org/proposed/FAA-2005-22810

## Summary

The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Model A310-203, -204, and -222 airplanes, and Model A310-300 series airplanes. This proposed AD would require a one-time rototest inspection for cracking of the frame foot and adjacent frames and skin in the area surrounding the frame foot run-outs from fuselage frames (FR) 43 through FR 46, and repair if necessary. The proposed AD also requires modification of certain fastener holes. This proposed AD results from a structural evaluation of Model A310 airplanes for widespread fatigue damage of the frame foot run-outs from FR 43 through FR 46. The evaluation revealed that, on in-service airplanes, undetected cracking in this area can lead to the rupture of the frame foot and subsequent cracking of the adjacent frames and fuselage skin. We are proposing this AD to prevent fatigue cracking of the frame foot run-outs, which could lead to rupture of the frame foot and cracking in adjacent frames and skin, and result in reduced structural integrity of the fuselage.

## Notices in this docket

- Oct 27, 2005: Notice of proposed rulemaking (NPRM). (first notice), FR document 05-21428, comments due Nov 28, 2005 (https://www.federalregister.gov/documents/2005/10/27/05-21428/airworthiness-directives-airbus-model-a310-203--204-and--222-airplanes-and-model-a310-300-series)

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