# Airworthiness Directives; Airbus Model A300 Series Airplanes
> **Rule** · Final rule. · Published 2000-04-11 · Effective 2000-05-16 · 65 FR 19308
## Document
- **Document number:** 00-8514
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A300 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 19308
- **Publication date:** 2000-04-11
- **Effective date:** 2000-05-16
- **FAA docket:** Docket No. 99-NM-205-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300 series airplanes, that requires modification of wing center box angle fittings at frame 47. 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 prevent reduced structural integrity of the wing center box angle fittings at frame 47 due to fatigue cracking.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/04/11/00-8514/airworthiness-directives-airbus-model-a300-series-airplanes)
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