[Federal Register Volume 67, Number 226 (Friday, November 22, 2002)]
[Rules and Regulations]
[Page 70310]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-29673]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000-NE-57; Amendment 39-12938; AD 2002-22-12]
RIN 2120-AA64


Airworthiness Directives; Titeflex Corporation, Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2002-22-12, applicable to certain Titeflex Corporation high-
pressure and medium-pressure hoses, that was published in the Federal 
Register on November 8, 2002 (67 FR 68024). An engine model referenced 
in the Applicability paragraph in the regulatory information is 
incorrect. This document corrects that reference. In all other 
respects, the original document remains the same.

EFFECTIVE DATE: November 8, 2002.

FOR FURTHER INFORMATION CONTACT: Terry Fahr, Aerospace Engineer, Boston 
Aircraft Certification Office, FAA, Engine and Propeller Directorate, 
12 New England Executive Park, Burlington, MA 01803-5299; telephone 
(781) 238-7155; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule airworthiness directive FR Doc. 
02-28113 applicable to certain Titeflex Corporation high-pressure and 
medium-pressure hoses, was published in the Federal Register on 
November 8, 2002 (67 FR 68024). The following correction is needed:


Sec.  39.13  [Corrected]

    On page 68025, in the Regulatory Information, third column, third 
paragraph, thirteenth line, ``General Electric CF6-80C and CFM-56 
series, * * *.'' is corrected to read ``CF6-80C and CFM56-5C, * * *.''

    Issued in Burlington, MA, on November 14, 2002.
Mark C. Fulmer,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-29673 Filed 11-21-02; 8:45 am]
BILLING CODE 4910-13-P