Document Headings

                    Document headings vary by document type but may contain                    the following:                  
                -                       the agency or agencies that issued and signed a document                    
                -                       the number of the CFR title and the number of each part                      the document amends, proposes to amend, or is directly                      related to                    
                -                       the agency docket number / agency internal file number                    
                -                       the RIN which identifies each regulatory action listed in                      the Unified Agenda of Federal Regulatory and Deregulatory                      Actions                    

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###### Department of Transportation

###### Federal Aviation Administration

          - 14 CFR Part 39
          - [Docket No. FAA-2010-0710; Directorate Identifier 2010-NE-26-AD; Amendment 39-16892; AD 2010-19-06R1]
          - RIN 2120-AA64

# AGENCY:

Federal Aviation Administration (FAA), DOT.

# ACTION:

Final rule; correction.

# SUMMARY:

                        The FAA is correcting an airworthiness directive (AD) that was published in the                         **Federal Register**                        . That AD applies to Turbomeca Arriel 1 series turboshaft engines. The AD number is incorrect in the preamble and in the Regulatory text. This document corrects those errors. In all other respects, the original document remains the same.                    

# DATES:

This final rule revision is effective January 17, 2012.

# ADDRESSES:

                        You may examine the AD docket on the Internet at                         *http://www.regulations.gov;*                         or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The address for the Docket Office (phone: (800) 647-5527) is Document Management Facility, U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.                    

# FOR FURTHER INFORMATION CONTACT:

                        Frederick Zink, Aerospace Engineer, Engine Certification Office, FAA, 12 New England Executive Park, Burlington, MA; phone: (781) 238-7779; fax: (781) 238-7199; email:                         *frederick.zink@faa.gov*.                    

# SUPPLEMENTARY INFORMATION:

Airworthiness Directive 2011-26-02, Amendment 39-16892 (76 FR 77378, December 13, 2011), currently requires removing from service certain gas generator second stage turbine discs, part number (P/N) 0 292 25 040 0, that are not marked with “CFR” before the discs exceed 4,000 cycles-in-service (CIS) since new. That AD also requires removing from service certain gas generator second stage turbine discs, P/N 0 292 25 040 0, that are marked with “CFR” before the discs exceed 6,500 CIS since new.

As published, the AD number 2011-26-02 in the preamble of the AD and under § 39.13 [Amended], is incorrect.

                    No other part of the preamble or regulatory information has been changed; therefore, only the changed portion of the final rule is being published in the                     **Federal Register**                    .                

The effective date of this AD revision remains January 17, 2012.

## Correction of Non-Regulatory Text

                    In the                     **Federal Register**                     of December 13, 2011, AD 2011-26-02; Amendment 39-16892 is corrected as follows:                

On page 77378, in the second column, on line 3 under 14 CFR Part 39, change AD 2011-26-02 to AD 2010-19-06R1.

## Correction of Regulatory Text

§ 39.13 

                        In the                         **Federal Register**                         of December 13, 2011, on page 77379, in the second column, lines 6 and 7 under § 39.13 [Amended] of AD 2011-26-02, are corrected to read as follows:                    

* * * * *

**AD 2010-19-06R1 Turbomeca:**                             Amendment 39-16892; Docket No. FAA-2010-0710;                        

* * * * *

Issued in Burlington, Massachusetts, on December 29, 2011.

Peter A. White,

Manager, Engine & Propeller Directorate, Aircraft Certification Service.

[FR Doc. 2012-79 Filed 1-6-12; 8:45 am]

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