Airworthiness Directives; CFM International S.A. Model CFM56 Turbofan Engines, 10952-10953 [2012-4285]

Download as PDF 10952 Federal Register / Vol. 77, No. 37 / Friday, February 24, 2012 / Rules and Regulations TABLE 1—AFFECTED ECU P/NS—Continued 1471M63P25 1471M63P30 1471M63P35 1519M89P04 1519M89P09 1519M89P16 1519M89P21 1519M89P26 1820M33P05 1471M63P26 1471M63P31 1471M63P36 1519M89P05 1519M89P10 1519M89P17 1519M89P22 1820M33P01 1820M33P06 (2) Remove from service ECUs with P/Ns 2121M37P01, 2121M37P02, 2121M38P01, 2121M38P02, 2121M41P01 and 2121M41P02 within 14 months or 1,050 engine flight 1471M63P27 1471M63P32 1519M89P01 1519M89P06 1519M89P13 1519M89P18 1519M89P23 1820M33P02 1820M33P07 1471M63P28 1471M63P33 1519M89P02 1519M89P07 1519M89P14 1519M89P19 1519M89P24 1820M33P03 1820M33P08 cycles after the effective date of this AD, whichever occurs first. (3) Remove from service ECUs with P/Ns listed in Table 2 of this AD within 60 months 1471M63P29 1471M63P34 1519M89P03 1519M89P08 1519M89P15 1519M89P20 1519M89P25 1820M33P04 1820M33P09 or 4,500 engine flight cycles after the effective date of this AD, whichever occurs first. TABLE 2—AFFECTED ECU P/NS 1471M63P37 1519M89P27 1820M33P10 2121M25P01 2121M29P02 1471M63P38 1519M89P28 1820M33P11 2121M25P02 2121M37P03 (h) Installation Prohibition The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures in 14 CFR 39.19 to make your request. (j) Related Information For more information about this AD, contact Tomasz Rakowski, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; phone: 781–238–7735; fax: 781–238– 7199; email: tomasz.rakowski@faa.gov. (k) Material Incorporated by Reference None. Issued in Burlington, Massachusetts, on February 17, 2012. Peter A. White, Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2012–4284 Filed 2–23–12; 8:45 am] rmajette on DSK2TPTVN1PROD with RULES BILLING CODE 4910–13–P Jkt 226001 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 (i) Alternative Methods of Compliance (AMOCs) 14:50 Feb 23, 2012 1471M63P40 1519M89P30 1820M33P13 2121M26P02 2121M41P03 DEPARTMENT OF TRANSPORTATION (1) After the effective date of this AD, do not install any ECU P/N listed in Table 1 of this AD onto any airplane. (2) After the effective date of this AD, do not operate any airplane with more than one ECU P/N 2121M37P02, 2121M38P02, or 2121M41P02 installed. VerDate Mar<15>2010 1471M63P39 1519M89P29 1820M33P12 2121M26P01 2121M38P03 Airworthiness Directives; CFM International S.A. Model CFM56 Turbofan Engines Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: 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 https:// 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 SUMMARY: PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 1471M63P42 1519M89P32 1820M33P15 2121M29P01 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: martin.adler@faa.gov. 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 § 39.13 [Corrected] 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 ■ E:\FR\FM\24FER1.SGM 24FER1 Federal Register / Vol. 77, No. 37 / Friday, February 24, 2012 / Rules and Regulations 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] BILLING CODE 4910–13–P DEPARTMENT OF COMMERCE Bureau of Industry and Security 15 CFR Part 748 [Docket No. 110525297–1476–01] RIN 0694–AF26 Amendment to Existing Validated EndUser Authorizations for Applied Materials (China), Inc., Boeing Tianjin Composites Co. Ltd., CSMC Technologies Corporation, Lam Research Corporation, and Semiconductor Manufacturing International Corporation in the People’s Republic of China, and for GE India Industrial Pvt. Ltd. in India Bureau of Industry and Security, Commerce. ACTION: Final rule. AGENCY: In this rule, the Bureau of Industry and Security (BIS) amends the Export Administration Regulations (EAR) to revise the existing Authorization Validated End-User (VEU) listings for five VEUs in the People’s Republic of China (PRC) and one VEU in India. For Applied Materials (China), Inc. (AMAT), this rule amends the eligible items AMAT may receive under Authorization VEU. For Boeing Tianjin Composites Co., Ltd. (BTC), this rule amends the eligible items the company may receive under Authorization VEU and revises the address of the eligible destination (i.e., facility) to which items may be exported, reexported, or transferred (incountry) under Authorization VEU. For CSMC Technologies Corporation (CSMC), this rule revises the address of one eligible destination. For Lam Research Corporation (Lam), this rule revises the list of facilities to which eligible items may be exported, reexported, or transferred (in-country) under Authorization VEU. For Semiconductor Manufacturing International Corporation (SMIC), this rule revises the list of eligible items that rmajette on DSK2TPTVN1PROD with RULES SUMMARY: VerDate Mar<15>2010 14:50 Feb 23, 2012 Jkt 226001 may be exported, reexported, or transferred (in-country) to SMIC under Authorization VEU. Finally, this rule revises the listed name for GE India to GE India Industrial Pvt Ltd. (GE India), amends the list of eligible items that may be exported, reexported, or transferred (in-country) to GE India under Authorization VEU, and removes one of the company’s eligible destinations. DATES: This rule is effective February 24, 2012. FOR FURTHER INFORMATION CONTACT: Karen Nies-Vogel, Chair, End-User Review Committee, Bureau of Industry and Security, U.S. Department of Commerce, 14th Street & Pennsylvania Avenue NW., Washington, DC 20230; by telephone: (202) 482–5991, by fax: (202) 482–3991 or email: ERC@bis.doc.gov. SUPPLEMENTARY INFORMATION: Background Authorization Validated End-User BIS amended the EAR in a final rule on June 19, 2007 (72 FR 33646), creating a new authorization for ‘‘validated endusers’’ (VEUs) located in eligible destinations to which eligible items may be exported, reexported, or transferred (in-country) under a general authorization instead of a license, in conformance with section 748.15 of the EAR. VEUs may obtain eligible items that are on the Commerce Control List, set forth in Supplement No. 1 to Part 774 of the EAR, without having to wait for their suppliers to obtain export licenses from BIS. Eligible items may include commodities, software, and technology, except those controlled for missile technology or crime control reasons. The VEUs listed in Supplement No. 7 to Part 748 of the EAR were reviewed and approved by the U.S. Government in accordance with the provisions of section 748.15 and Supplement Nos. 8 and 9 to Part 748 of the EAR. The revisions to Supplement No. 7 to Part 748 set forth in this rule are being made either at the request of the VEUs or pursuant to the U.S. Government’s periodic review of VEU authorizations, and were approved by the End-User Review Committee (ERC) following the process set forth in Section 748.15 and Supplement No. 9 to Part 748 of the EAR. Amendment to Existing Validated EndUser Authorizations in the PRC Revision to the List of ‘‘Eligible Items’’ for Applied Materials (China), Inc. Applied Materials (China), Inc. (AMAT) was designated as a VEU on PO 00000 Frm 00011 Fmt 4700 Sfmt 4700 10953 October 19, 2007 (72 FR 59164). Subsequently, AMAT’s VEU authorization listing has been amended to add additional facilities, modify the items it is eligible to receive, and change the company’s name (74 FR 19382 (Apr. 29, 2009) and 75 FR 27185 (May 14, 2010)). In this rule, BIS amends Supplement No. 7 to Part 748 of the EAR to add an additional Export Control Classification Number (ECCN) paragraph, ECCN 3B001.a, as an eligible item for all eligible AMAT destinations. Correction of Facility Address and Revision to the List of ‘‘Eligible Items’’ for Boeing Tianjin Composites Co. Ltd. BIS designated BHA Aero Composite Parts Co. as a VEU on October 19, 2007 (72 FR 59164). On April 29, 2009, BIS amended the authorization by changing the name of the VEU to Boeing Tianjin Composites Co., Ltd. (BTC) (74 FR 19382). In this rule, BIS amends Supplement No. 7 to Part 748 of the EAR to correct the spelling of the name of the road on which BTC’s ‘‘Eligible Destination’’ (i.e., facility) is located: ‘‘Heibei Road’’ will be revised to read ‘‘Hebei Road.’’ BIS also revises the list of ‘‘Eligible Items (By ECCN)’’ that may be exported, reexported, and transferred (in-country) to BTC by removing ECCN 2B001.a from the parenthetical limiting statement for ECCN 1E001. Pursuant to the latter revision, the export, reexport or transfer (in-country) of 1E001 ‘‘technology,’’ according to the General Technology Note, for the ‘‘development’’ or ‘‘production’’ of items controlled by ECCN 2B001.a is no longer authorized to BTC under Authorization VEU. This amendment is not the result of activities of concern by BTC. Revisions to the List of ‘‘Eligible Destinations’’ for CSMC Technologies Corporation BIS designated CSMC Technologies Corporation (CSMC) as a VEU on January 18, 2011 (76 FR 2802). Thereafter, on June 28, 2011, BIS amended the list of CSMC’s eligible items (76 FR 37364). This rule amends Supplement No. 7 to Part 748 by updating the address of CSMC Technologies Fab 2 Co., Ltd., a CSMC ‘‘Eligible Destination.’’ Revisions to the List of ‘‘Eligible Destinations’’ for Lam Research Corporation BIS designated Lam Research Corporation (Lam) as a VEU on October 12, 2010 (75 FR 62462). This rule amends Supplement No. 7 to Part 748 by adding three and updating six addresses of the company’s list of E:\FR\FM\24FER1.SGM 24FER1

Agencies

[Federal Register Volume 77, Number 37 (Friday, February 24, 2012)]
[Rules and Regulations]
[Pages 10952-10953]
From the Federal Register Online via the Government Printing 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.

-----------------------------------------------------------------------

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 https://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: martin.adler@faa.gov.

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]
BILLING CODE 4910-13-P

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