# Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines
> **Rule** · Final rule; request for comments. · Published 2002-05-23 · Effective 2002-06-27 · 67 FR 36090
## Document
- **Document number:** 02-12631
- **Category:** airworthiness
- **Manufacturer:** General Electric Company CF6-80E1 Series Turbofan
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 67 FR 36090
- **Publication date:** 2002-05-23
- **Effective date:** 2002-06-27
- **FAA docket:** Docket No. 2002-NE-04-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to General Electric Company (GE) CF6-80E1 series turbofan engines installed on Airbus Industrie A330 series airplanes. This action requires initial and repetitive thrust reverser inspections and checks, and allows extended threshold and repetitive inspection intervals for certain inspections if an optional double p-seal configuration is installed. This amendment is prompted by reports of service-induced hardware deterioration that reduces the overall thrust reverser system protection against inadvertent deployment, which can result in loss of control of the airplane. The actions specified in this AD are intended to prevent inadvertent in-flight thrust reverser deployment, which can result in loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2002/05/23/02-12631/airworthiness-directives-general-electric-company-cf6-80e1-series-turbofan-engines)
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