Skip to Content

Rule

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

Document Details

Information about this document as published in the Federal Register.

Published Document

This document has been published in the Federal Register. Use the PDF linked in the document sidebar for the official electronic format.

Start Preamble

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.

Start Further Info

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.

End Further Info End Preamble Start Supplemental Information

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:

[Corrected]
Start Amendment Part

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”.

End Amendment Part Start Signature

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

Jay J. Pardee,

Manager, Engine and Propeller Directorate, Aircraft Certification Service.

End Signature End Supplemental Information

[FR Doc. 04-10429 Filed 5-6-04; 8:45 am]

BILLING CODE 4910-13-P