# Proposed AD 99-NM-82-AD: Airbus Model A300-600 and A310 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2000-05-03
- Action: Notice of proposed rulemaking (NPRM).
- Published: January 5, 2000, 65 FR 397
- Comments due: February 4, 2000
- Became: [AD 2000-05-03](https://openairdocs.org/ad/2000-05-03)
- Docket: 99-NM-82-AD
- FR document: 00-137
- Official PDF: https://openairdocs.org/files/sha256/68/ed/68ed96b468d0b07e3d217226c038aa160556ea97e4553552f229cb65613d1b64 (from https://www.govinfo.gov/content/pkg/FR-2000-01-05/pdf/00-137.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/01/05/00-137/airworthiness-directives-airbus-model-a300-600-and-a310-series-airplanes
- Page: https://openairdocs.org/proposed/99-NM-82-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Airbus A300-600 and A310 series airplanes. This proposal would require repetitive high frequency eddy current (HFEC) inspections to detect cracking of the inner flange of fuselage frame FR73A, between beams 5 and 7, and corrective actions, 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 fatigue cracking of the inner flange of fuselage frame FR73A, which could result in reduced structural integrity of the fuselage.

## Notices in this docket

- Jan 5, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-137, comments due Feb 4, 2000 (https://www.federalregister.gov/documents/2000/01/05/00-137/airworthiness-directives-airbus-model-a300-600-and-a310-series-airplanes)

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