# Airworthiness Directives; Airbus Model A300-600 Series Airplanes
> **Rule** · Final rule. · Published 1998-12-10 · Effective 1999-01-14 · 63 FR 68167
## Document
- **Document number:** 98-32623
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A300-600 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 68167
- **Publication date:** 1998-12-10
- **Effective date:** 1999-01-14
- **FAA docket:** Docket No. 97-NM-153-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 cracks in the angle fitting at frame 40 of the center wing box, and corrective actions, if necessary; and eventual modification of that angle fitting, which terminates the repetitive inspections. 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 cracks in the center wing box angle fitting, which could result in the failure of the center wing box at frame 40, and consequent reduced structural integrity of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/12/10/98-32623/airworthiness-directives-airbus-model-a300-600-series-airplanes)
---
*AI Analytics · CC0 1.0*