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Airworthiness Directives; General Electric Company CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 Turbofan Engines; Correction

Document Details

Information about this document as published in the Federal Register.

Published Document

This document has been published in the Federal Register. Use the PDF linked in the document sidebar for the official electronic format.

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AGENCY:

Federal Aviation Administration (FAA), DOT.

ACTION:

Final rule; correction.

SUMMARY:

The FAA is correcting airworthiness directive (AD) 2009-26-09, which published in the Federal Register. That AD applies to General Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan engines. The GE alert service bulletin (ASB) numbers CF34-AL S/B 72 A0212, CF34-AL S/B 72 A0234, and CF34-AL S/B 72 A0235 in the regulatory section are incorrect. This document corrects those ASB numbers. In all other respects, the original document remains the same.

DATES:

This correction is May 20, 2010. The compliance date of AD 2009-26-09 remains February 11, 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; phone: (781) 238-7756; fax: (781) 238-7199.

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SUPPLEMENTARY INFORMATION:

On January 7, 2010 (75 FR 910), we published a final rule AD, FR Doc, E9-30471, in the Federal Register. That AD applies to (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan engines. We need to make the following corrections:

[Corrected]

1. On page 914, in the second column, in paragraph (k)(1)(i), in the fifth and eighth lines, “CF34-AL” is corrected to read “CF34-BJ”.

2. On page 914, in the second column, in paragraph (k)(2)(iii), in the fifth line, “CF34-AL” is corrected to read “CF34-BJ”.

3. On page 914, in the second column, in paragraph (l), in the seventh line, “CF34-AL” is corrected to read “CF34-BJ”.

4. On page 914, in the second column, in paragraph (l)(1), in the second line, “CF34-AL” is corrected to read “CF34-BJ”.

5. On page 914, in the third column, in paragraph (l)(1)(i), in the seventh and tenth lines, “CF34-AL” is corrected to read “CF34-BJ”.

6. On page 914, in the third column, in paragraph (m)(1), in the second, ninth, and twelfth lines, “CF34-AL” is corrected to read “CF34-BJ”.

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Issued in Burlington, Massachusetts, on May 10, 2010.

Peter A. White,

Assistant Manager, Engine and Propeller Directorate, Aircraft Certification Service.

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[FR Doc. 2010-11642 Filed 5-19-10; 8:45 am]

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