Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction

---
identifier: "/us/fr/04-10429"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction"
title_number: 0
title_name: "Federal Register"
section_number: "04-10429"
section_name: "Airworthiness Directives; General Electric Company CF6-80C2 Series Turbofan Engines; Correction"
positive_law: false
currency: "2004-05-07"
last_updated: "2004-05-07"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "04-10429"
document_type: "rule"
publication_date: "2004-05-07"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
cfr_references:
  - "14 CFR Part 39"
rin: "2120-AA64"
fr_citation: "69 FR 25488"
fr_volume: 69
docket_ids:
  - "Docket No. 2003-NE-46-AD"
  - "Amendment 39-13557"
  - "AD 2004-07-13"
effective_date: "2004-04-01"
fr_action: "Final rule; correction."
---


#  [Corrected]

**AGENCY:**

Federal Aviation Administration, DOT.

**ACTION:**

Final rule; correction.

**SUMMARY:**

This document makes a correction to Airworthiness Directive (AD) 2004-07-13. That AD applies to General Electric Company (GE) CF6-80C2 series turbofan engines. That AD was published in the *Federal Register* on April 1, 2004 (69 FR 17033). The amendatory text in the Applicability section is incorrect. This document corrects the aircraft models that these engines are installed on. In all other respects, the original document remains the same.

**DATES:**

*Effective Date:* Effective April 1, 2004.

**FOR FURTHER INFORMATION CONTACT:**

Karen Curtis, Aerospace Engineer, Aircraft Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; telephone (781) 238-7192; fax (781) 238-7199.

**SUPPLEMENTARY INFORMATION:**

A final rule AD, FR Doc. 04-7235, that applies to General Electric Company (GE) CF6-80C2 series turbofan engines was published in the *Federal Register* on April 1, 2004 (69 FR 17033). The following correction is needed:

**14 CFR Part 39**

§ 39.13

On page 17034, in the first column, in the Amendatory Section, Applicability paragraph (c), in the eighth line, “A300 and A330” is corrected to read “A300 and A310”.

Issued in Burlington, MA, on May 3, 2004.

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification Service.