# Airworthiness Directives; Airbus Model A320 Series Airplanes
> **Rule** · Final rule. · Published 1998-03-20 · Effective 1998-04-24 · 63 FR 13489
## Document
- **Document number:** 98-6758
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A320 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 63 FR 13489
- **Publication date:** 1998-03-20
- **Effective date:** 1998-04-24
- **FAA docket:** Docket No. 95-NM-216-AD
## Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Airbus Model A320 series airplanes, that currently requires inspections to detect cracking of certain floor beams and side box-beams, and repair of cracks; and modification of the pressure floor. That AD was prompted by results of a full-scale fatigue test. This amendment adds a one-time inspection to verify proper clearance between the fasteners of the reinforcement bracket and the bellcrank of the free-fall extension system of the main landing gear (MLG) and its associated tie rod attachment nut. This amendment also adds a requirement for a new improved modification of the pressure floor. The actions specified by this AD are intended to prevent reduced structural integrity of the fuselage, restricted operation of the MLG free-fall system and, consequently, reduced ability to use the MLG during an emergency.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1998/03/20/98-6758/airworthiness-directives-airbus-model-a320-series-airplanes)
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