# Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction
> **Rule** · Final rule; correction. · Published 2009-12-14 · Effective 2009-12-14 · 74 FR 66042
## Document
- **Document number:** E9-29483
- **Category:** airworthiness
- **Manufacturer:** General Electric Company CF6-80C2 Series Turbofan
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 74 FR 66042
- **Publication date:** 2009-12-14
- **Effective date:** 2009-12-14
- **FAA docket:** Docket No. FAA-2009-0018
## Abstract

The FAA is correcting airworthiness directive (AD) 2009-21-07, which published in the Federal Register. That AD applies to General Electric Company (GE) CF6-80C2 series turbofan engines with certain thrust reverser ballscrew gearbox assembly adjustable-length end actuators installed. The unsafe condition statement of "We are issuing this AD to prevent loss of asymmetric thrust and thrust control", and rod-end part number "MS2124S06" in paragraph (j) are incorrect. This document corrects the unsafe condition statement and the part number. In all other respects, the original document remains the same.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2009/12/14/E9-29483/airworthiness-directives-general-electric-company-cf6-80c2-series-turbofan-engines-correction)
---
*AI Analytics · CC0 1.0*