[Federal Register Volume 77, Number 37 (Friday, February 24, 2012)]
[Rules and Regulations]
[Pages 10952-10953]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-4285]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2008-1245; Directorate Identifier 2008-NE-27-AD;
Amendment 39-15912; AD 2009-11-02]
RIN 2120-AA64
Airworthiness Directives; CFM International S.A. Model CFM56
Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
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SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to CFM International
S.A. CFM56-2, CFM56-3, CFM56-5A, CFM56-5B, CFM56-5C, and CFM56-7B
series turbofan engines with certain part number (P/N) and serial
number (SN) high-pressure compressor (HPC) 4-9 spools installed. In
Table 1 of the AD, the HPC 4-9 spool SN GWN05AMO in the 2nd column of
the Table is incorrect. This document corrects that error. In all other
respects, the original document remains the same.
DATES: This final rule is effective February 24, 2012. The effective
date for AD 2009-11-02 (74 FR 23305, May 19, 2009) remains June 23,
2009.
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: Martin Adler, Aerospace Engineer,
Engine Certification Office, FAA, Engine & Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; phone: 781-238-7157;
fax: 781-238-7199; email: [email protected].
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2009-11-02,
Amendment 39-15912 (74 FR 23305, May 19, 2009), currently requires
removing certain HPC 4-9 spools listed by P/N and SN in the AD.
As published, in Table 1 of the AD, the HPC 4-9 spool SN GWN05AMO
in the 2nd column of the Table 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 remains June 23, 2009.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register of May 19, 2009, on page 23306, in the 3rd
column, in Table 1, under the HPC 4-9 Spool SN heading, in the
twentieth line of AD
[[Page 10953]]
2009-11-02; Amendment 39-15912 is corrected as follows:
* * * * *
GWN05AM0
* * * * *
Issued in Burlington, Massachusetts, on February 13, 2012.
Peter A. White,
Manager, Engine & Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2012-4285 Filed 2-23-12; 8:45 am]
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