[Federal Register: December 19, 2002 (Volume 67, Number 244)]
[Rules and Regulations]
[Page 77666-77667]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr19de02-3]
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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