[Federal Register Volume 67, Number 238 (Wednesday, December 11, 2002)]
[Rules and Regulations]
[Pages 76111-76112]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-31173]


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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 Airworthiness Directive 
(AD) 2002-23-09 applicable to General Electric Company CF34-8C1 
turbofan engines that was published in the Federal Register on November 
20, 2002 (67 FR 70004). Table 801 was incorrectly numbered in three 
locations in the AD. 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

[[Page 76112]]

01803-5299; telephone (781) 238-7744; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc, 02-29355 applicable 
to General Electric Company CF34-8C1 turbofan engines was published in 
the Federal Register on November 20, 2002 (67 FR 70004). The following 
correction is needed:


Sec.  39.13  [Corrected]

    On page 70005, in the first column, in the Comments Section, in the 
fourth paragraph, in the eighth and again in the thirteenth lines, 
``Table 805'' is corrected to read ``Table 801''. Also on page 70005, 
in the third column in the ninth paragraph, ``Table 805'' is corrected 
to read ``Table 801''.

    Dated: Issued in Burlington, MA, on December 4, 2002.
Francis A. Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-31173 Filed 12-10-02; 8:45 am]
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