# Airworthiness Directives; Airbus Model A300, A310, A300-600 Series Airplanes
> **Rule** · Final rule. · Published 1998-07-08 · Effective 1998-08-12 · 63 FR 36832
## Document
- **Document number:** 98-17912
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 36832
- **Publication date:** 1998-07-08
- **Effective date:** 1998-08-12
- **FAA docket:** Docket No. 98-NM-132-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A300, A310, and A300-600 series airplanes. This amendment requires a one-time operational test and repetitive functional tests of the free fall control mechanism of the landing gear to ensure proper release of the main landing gear (MLG), and corrective action, if necessary. This amendment also requires eventual modification of the free fall control mechanism of the landing gear, which constitutes terminating action for the repetitive functional tests. 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 malfunction of the free fall control mechanism of the landing gear, which could result in the inability to extend the MLG in the event of failure of the hydraulic extension system.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/07/08/98-17912/airworthiness-directives-airbus-model-a300-a310-a300-600-series-airplanes)
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