# Airworthiness Directives; General Electric Company CF34-8C1 Turbofan Engines, Correction
**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- 02 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.
**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.
**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”.
Issued in Burlington, MA, on December 12, 2002.
Francis A. Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.