# Airworthiness Directives; General Electric Company (GE) CF6-80E1A2 and -80E1A4 Turbofan Engines; Correction
> **Rule** · Final rule; request for comments correction. · Published 2004-01-14 · Effective 2004-01-14 · 69 FR 2062
## Document
- **Document number:** 04-760
- **Category:** airworthiness
- **Manufacturer:** General Electric Company (GE) CF6-80E1A2 and -80E1A4 Turbofan
- **Type:** Rule
- **Action:** Final rule; request for comments correction.
- **Citation:** 69 FR 2062
- **Publication date:** 2004-01-14
- **Effective date:** 2004-01-14
- **FAA docket:** Docket No. 2003-NE-26-AD
## Abstract

This document makes a correction to Airworthiness Directive (AD) 2003-26-11 applicable to GE CF6-80E1A2 and -80E1A4 turbofan engines with left vertical link bolts part number (P/N) 1304M26P02 installed, and pylon attachment bolts originally torqued to 450-500 lb ft. That AD was published in the Federal Register on January 6, 2004 (69 FR 494). The SUPPLEMENTARY INFORMATION paragraph title, first sentence, and first three words of the second sentence of that paragraph were inadvertently omitted. This document corrects that omission. In all other respects, the original document remains the same.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2004/01/14/04-760/airworthiness-directives-general-electric-company-ge-cf6-80e1a2-and--80e1a4-turbofan-engines)
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