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###### Department of Transportation

###### Federal Aviation Administration

          - 14 CFR Part 39
          - [Docket No. FAA-2007-27687; Directorate Identifier 2000-NE-42-AD; Amendment 39-16144; AD 2009-26-09]
          - RIN 2120-AA64

# 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.

# 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.                    

# 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:                

§ 39.13 

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”.

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

Peter A. White,

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

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

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