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Home » 2009 Issues » 74 FR (12/31/2009) » E9-30978. Airworthiness Directives; General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B Series Turbofan Engines; Delay of Effective Date

  E9-30978. Airworthiness Directives; General Electric Company (GE) CF34-1A, CF34-3A, and CF34-3B Series Turbofan Engines; Delay of Effective Date  

  • Start Preamble

    AGENCY:

    Federal Aviation Administration (FAA), Department of Transportation (DOT).

    ACTION:

    Final rule; delay of effective date.

    SUMMARY:

    The FAA is delaying the effective date of the final rule airworthiness directive (AD) 2009-24-11, which published in the Federal Register, for an additional 30 days, from January 4, 2010 to February 3, 2010. The FAA is delaying the effective date to allow us a sufficient amount of time to make corrections to the compliance text of the final rule.

    DATES:

    The effective date for the final rule published in the Federal Register on November 30, 2009 (74 FR 62481) is delayed until February 3, 2010.

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    FOR FURTHER INFORMATION CONTACT:

    John Frost, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; e-mail: john.frost@faa.gov; telephone (781) 238-7756; fax (781) 238-7199.

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    SUPPLEMENTARY INFORMATION:

    On November 30, 2009 (74 FR 62481), we published a final rule AD, FR Doc. E9-28236, in the Federal Register. That AD applies to GE CF34-1A, CF34-3A, and CF34-3B series turbofan engines. We are delaying the effective date to allow us a sufficient amount of time to make corrections to the compliance text of the final rule. Since AD 2009-24-11 was issued, we discovered that when we recodified the compliance section as part of our response to a comment received on the proposed AD, we inadvertently left out of the AD certain fan blade effectivity information from paragraphs (f) and (g) and (j). Paragraphs (f) and (g) are missing information on fan blades, P/Ns 6018T30P14 or 4923T56G08, that have any fan blade S/Ns listed in Appendix A of General Electric Aircraft Engines (GEAE) Service Bulletin (SB) No. CF34-AL S/B 72-0245, Revision 01, dated July 30, 2008. Also, paragraph (j) is missing Start Printed Page 69260information on fan blades, P/N 6018T30P14 or P/N 4923T56G08, that have any fan blade S/Ns listed in Appendix A of GEAE SB No. CF34-BJ S/B 72-0229, Revision 01, dated July 30, 2008.

    Start Signature

    Issued in Burlington, Massachusetts, on December 23, 2009.

    Francis A. Favara,

    Manager, Engine and Propeller Directorate, Aircraft Certification Service.

    End Signature End Supplemental Information

    [FR Doc. E9-30978 Filed 12-30-09; 8:45 am]

    BILLING CODE 4910-13-P

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Document Information

Comments Received:
0 Comments
Effective Date:
11/30/2009
Published:
12/31/2009
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; delay of effective date.
Document Number:
E9-30978
Dates:
The effective date for the final rule published in the Federal Register on November 30, 2009 (74 FR 62481) is delayed until February 3, 2010.
Pages:
69259-69260 (2 pages)
Docket Numbers:
Docket No. FAA-2009-0328, Directorate Identifier 2008-NE-44-AD, Amendment 39-16103, AD 2009-24-11
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
e9-30978.pdf
CFR: (1)
14 CFR 39