# Proposed AD 98-NM-211-AD: Airbus Model A300, A310, and A300-600 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-05-18
- Action: Notice of proposed rulemaking (NPRM).
- Published: January 4, 2000, 65 FR 254
- Comments due: February 3, 2000
- Became: [AD 2000-05-18](https://openairdocs.org/ad/2000-05-18)
- Docket: 98-NM-211-AD
- FR document: 00-48
- Official PDF: https://openairdocs.org/files/sha256/a3/de/a3de9ab4b02b5d1d4d9757a9bb400cbd3eedfecae6e9c5facc086fb5cd23d203 (from https://www.govinfo.gov/content/pkg/FR-2000-01-04/pdf/00-48.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/01/04/00-48/airworthiness-directives-airbus-model-a300-a310-and-a300-600-series-airplanes
- Page: https://openairdocs.org/proposed/98-NM-211-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus Model A300, A310, and A300-600 series airplanes. This proposal would require repetitive eddy current inspections to detect cracking on the door edge frames of the fuselage bulk cargo compartment, and repair, if necessary. This proposal is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by the proposed AD are intended to detect and correct cracks in the door edge frames of the fuselage bulk cargo compartment, which could result in reduced structural integrity of the airframe.

## Notices in this docket

- Jan 4, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-48, comments due Feb 3, 2000 (https://www.federalregister.gov/documents/2000/01/04/00-48/airworthiness-directives-airbus-model-a300-a310-and-a300-600-series-airplanes)

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