E8-23140. Airworthiness Standards; Aircraft Engine Standards for Pressurized Engine Static Parts; Correction  

  • Start Preamble

    AGENCY:

    Federal Aviation Administration (FAA), DOT.

    ACTION:

    Final rule; correction.

    SUMMARY:

    This document corrects the amendment number to a final rule published in the Federal Register of Thursday, September 25, 2008, regarding requirements for pressurized engine static parts.

    DATES:

    This amendment becomes effective November 24, 2008.

    Start Further Info

    FOR FURTHER INFORMATION CONTACT:

    Tim Mouzakis, Engine and Propeller Directorate Standards Staff, ANE-111, Federal Aviation Administration, 12 New England Executive Park, Burlington, Massachusetts 01803-5299; telephone (781) 238-7114, fax (781) 238-7199, e-mail timoleon.mouzakis@faa.gov.

    Correction

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    In final rule Aircraft Engine Standards for Pressurized Engine Static Parts beginning on page 55435 in the Federal Register issue of Thursday, September 25, 2008, (73 FR 55435) make the following correction.

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    1. On page 55435, in the first column, beginning on the fourth line of the heading, “Amendment No. 33-26” is corrected to read “Amendment No. 33-27.”

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    Issued in Washington, DC on September 26, 2008.

    Pamela Hamilton-Powell,

    Director, Office of Rulemaking.

    End Signature End Further Info End Preamble

    [FR Doc. E8-23140 Filed 10-1-08; 8:45 am]

    BILLING CODE 4910-13-P

Document Information

Comments Received:
0 Comments
Effective Date:
11/24/2008
Published:
10/02/2008
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; correction.
Document Number:
E8-23140
Dates:
This amendment becomes effective November 24, 2008.
Pages:
57235-57235 (1 pages)
Docket Numbers:
Docket No. FAA-2007-28501, Amendment No. 33-27
RINs:
2120-AJ05: Airworthiness Standards: Aircraft Engine Standards for Pressurized Engine Static Parts
RIN Links:
https://www.federalregister.gov/regulations/2120-AJ05/airworthiness-standards-aircraft-engine-standards-for-pressurized-engine-static-parts
PDF File:
e8-23140.pdf
CFR: (1)
14 CFR 33