# Airworthiness Directives; Airbus Model A310 and A300-600 Series Airplanes Equipped With General Electric CF6-80C2 Engines
> **Rule** · Final rule. · Published 1999-03-12 · Effective 1999-04-16 · 64 FR 12244
## Document
- **Document number:** 99-5992
- **Category:** airworthiness
- **Manufacturer:** Airbus Model A310 and A300-600 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 64 FR 12244
- **Publication date:** 1999-03-12
- **Effective date:** 1999-04-16
- **FAA docket:** Docket No. 96-NM-66-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Airbus Model A310 and A300-600 series airplanes, that requires repetitive flow checks of the hydraulic pump drain system to ensure that the system is not clogged, and correction of any discrepancy. This amendment also requires replacement of the existing magnetic seals of the accessory gearbox assembly with new, improved seals. Replacement of certain seals terminates the requirement for repetitive flow checks. This amendment also requires replacement of the engine drain modules with drain manifolds. 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 contamination of the engine accessory gearbox oil with hydraulic fluid, which could result in an in-flight engine shutdown.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/1999/03/12/99-5992/airworthiness-directives-airbus-model-a310-and-a300-600-series-airplanes-equipped-with-general)
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