# Airworthiness Directives; Airbus Model A310 Series Airplanes
> **Rule** · Final rule. · Published 1998-04-29 · Effective 1998-06-03 · 63 FR 23377
## Document
- **Document number:** 98-11070
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A310 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 23377
- **Publication date:** 1998-04-29
- **Effective date:** 1998-06-03
- **FAA docket:** Docket No. 96-NM-248-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A310 series airplanes, that requires repetitive inspections of the fuselage skin to detect corrosion or fatigue cracking around and under the chafing plates of the wing root; and corrective actions, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to detect and correct fatigue cracks and corrosion around and under chafing plates of the wing root, which could result in reduced structural integrity of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/04/29/98-11070/airworthiness-directives-airbus-model-a310-series-airplanes)
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