# Airworthiness Directives; Airbus Model A300-600 Series Airplanes
> **Rule** · Final rule. · Published 2000-04-14 · Effective 2000-05-19 · 65 FR 20078
## Document
- **Document number:** 00-8987
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A300-600 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 20078
- **Publication date:** 2000-04-14
- **Effective date:** 2000-05-19
- **FAA docket:** Docket No. 98-NM-78-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300-600 series airplanes, that requires repetitive inspections to detect cracking of the doubler angle and discrepancies of the fasteners that connect the doubler angle and the bottom panel of the center wing box, 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 cracking in the doubler angle and discrepancies of the fasteners that connect the doubler angle and the bottom panel of the center wing box. Such cracking and discrepancies could result in reduced structural integrity of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/04/14/00-8987/airworthiness-directives-airbus-model-a300-600-series-airplanes)
---
*AI Analytics · CC0 1.0*