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Airworthiness Directives; General Electric Company CF34-8C1 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 a previous correction to Airworthiness Directive (AD) 2002-23-Start Printed Page 7766702 applicable to General Electric Company CF34-8C1 turbofan engines that was published in the Federal Register on December 11, 2002 (67 FR 76111). A typographical error was made in the AD number in line three of the Summary. This document corrects that number. In all other respects, the original document remains the same.

EFFECTIVE DATE:

December 26, 2002.

Start Further Info

FOR FURTHER INFORMATION CONTACT:

Keith Mead, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803-5299; telephone (781) 238-7744; fax (781) 238-7199.

End Further Info End Preamble Start Supplemental Information

SUPPLEMENTARY INFORMATION:

A final rule correction AD, FR Doc. 02-31173 applicable to General Electric Company CF34-8C1 turbofan engines was published in the Federal Register on December 11, 2002 (67 FR 76111). The following correction is needed:

On page 76111, in the third column, in the third line of the Summary, remove the AD number “(AD) 2002-23-09” and add in its place “(AD) 2002-23-02”.

Start Signature

Issued in Burlington, MA, on December 12, 2002.

Francis A. Favara,

Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.

End Signature End Supplemental Information

[FR Doc. 02-31999 Filed 12-18-02; 8:45 am]

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