AD 2002-23-02

[Federal Register Volume 67, Number 244 (Thursday, December 19, 2002)]
[Rules and Regulations]
[Pages 77666-77667]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 02-31999]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2002-NE-13-AD; Amendment 39-12946; AD 2002-23-02]
RIN 2120-AA64


Airworthiness Directives; General Electric Company CF34-8C1 
Turbofan Engines, Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to a previous correction to 
Airworthiness Directive (AD) 2002-23-

[[Page 77667]]

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.
[FR Doc. 02-31999 Filed 12-18-02; 8:45 am]
BILLING CODE 4910-13-P