# Airworthiness Directives; General Electric Company (GE) CF6-80C2 Turbofan Engines; Correction
> **Rule** · Final rule; correction. · Published 2005-03-04 · Effective 2005-03-04 · 70 FR 10485
## Document
- **Document number:** 05-4072
- **Category:** airworthiness
- **Manufacturer:** General Electric Company (GE) CF6-80C2 Turbofan
- **Type:** Rule
- **Action:** Final rule; correction.
- **Citation:** 70 FR 10485
- **Publication date:** 2005-03-04
- **Effective date:** 2005-03-04
- **FAA docket:** Docket No. 2003-NE-43-AD
## Abstract

This document makes a correction to Airworthiness Directive (AD) 2004-22-07. That AD applies to GE CF6-80C2 turbofan engines with certain part number (P/N) high pressure turbine stage 2 nozzle guide vanes (HPT S2 NGVs) installed. That AD was published in the Federal Register on October 27, 2004 (69 FR 62571). The phrase "5.0 or more cycles per flight leg" in the Compliance section is incorrect. This document corrects that phrase. In all other respects, the original document remains the same.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/03/04/05-4072/airworthiness-directives-general-electric-company-ge-cf6-80c2-turbofan-engines-correction)
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