# Airworthiness Directives; Airbus Model A300 B2-203 and A300 B4-203 Airplanes; Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series Airplanes); and Model A310-200 and -300 Series Airplanes
> **Rule** · Final rule. · Published 2006-07-20 · Effective 2006-08-24 · 71 FR 41118
## Document
- **Document number:** E6-11414
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A300 B2-203 and A300 B4-203
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 41118
- **Publication date:** 2006-07-20
- **Effective date:** 2006-08-24
- **FAA docket:** Docket No. FAA-2006-23675
## Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Airbus Model A300 series airplanes and all Model A300-600 and A310 series airplanes. That AD currently requires repetitive inspections of the pitch trim system to detect continuity defects in the autotrim function, and follow-on corrective actions if necessary. For certain airplanes, this new AD requires replacing the flight augmentation computers (FACs) with new improved FACs. This AD also revises the applicability of the existing AD. This AD results from the development of a final action intended to address the unsafe condition. We are issuing this AD to prevent a sudden change in pitch due to an out-of-trim condition combined with an autopilot disconnect, which could result in reduced controllability of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/07/20/E6-11414/airworthiness-directives-airbus-model-a300-b2-203-and-a300-b4-203-airplanes-model-a300-b4-600)
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