# Airworthiness Directives; Airbus Model A320 and A321 Series Airplanes
> **Rule** · Final rule. · Published 1999-01-15 · Effective 1999-02-19 · 64 FR 2551
## Document
- **Document number:** 99-813
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A320 and A321 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 64 FR 2551
- **Publication date:** 1999-01-15
- **Effective date:** 1999-02-19
- **FAA docket:** Docket No. 98-NM-67-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A320 and A321 series airplanes. This amendment requires modification of the slat and flap control computer (SFCC) in the aft electronics rack. 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 failure of the SFCC caused by computer software anomalies or contamination by conductive dust. This condition, if not corrected, could result in uncommanded slat retraction during takeoff and consequent insufficient wing lift available to complete a successful takeoff.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/01/15/99-813/airworthiness-directives-airbus-model-a320-and-a321-series-airplanes)
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