Airworthiness Directives; General Electric Company CF6-45A, CF6-50A, CF6-50C, and CF6-50E Series Turbofan Engines; Correction, 33692 [05-11442]

Download as PDF 33692 Federal Register / Vol. 70, No. 110 / Thursday, June 9, 2005 / Rules and Regulations Regulatory Flexibility Act A regulatory flexibility analysis is required only when the agency must publish a notice of proposed rulemaking. See 5 U.S.C. 603, 604. Because the amendment to part 330 is being published in interim final form without a notice of proposed rulemaking, no regulatory flexibility analysis is required. of the United States or a state or but for sections 2(b), 3(c)(1), or 6(a)(1) of that act shall be deemed to be a corporation for purposes of determining deposit insurance coverage. An exception to this paragraph (a)(2) shall exist for any trust or other business arrangement established by a state or that is a state agency or state public instrumentality as part of a qualified tuition savings program under section 529 of the Internal Revenue Code (26 U.S.C. 529)). A deposit account of such a trust or business arrangement shall not be deemed to be the deposit of a corporation provided that: The funds in the account may be traced to one or more particular investors or participants; and the existence of the trust relationships are disclosed in accordance with the requirements of § 330.5. If these conditions are satisfied, each participant’s funds shall be insured to the participant. * * * * * Small Business Regulatory Enforcement Fairness Act In accordance with the Small Business Regulatory Enforcement Fairness Act, the FDIC will report this rule to Congress so that the rule may be reviewed. See 5 U.S.C. 801 et seq. By order of the Board of Directors. Federal Deposit Insurance Corporation. Dated at Washington, DC, this 16th day of May, 2005. Valerie J. Best, Assistant Executive Secretary. [FR Doc. 05–11212 Filed 6–8–05; 8:45 am] List of Subjects in 12 CFR Part 330 Bank deposit insurance, Banks, Banking, Reporting and recordkeeping requirements, Savings and loan associations, Trust and trustees. I For the reasons set forth in the preamble, the Board of Directors of the Federal Deposit Insurance Corporation hereby amends part 330 of title 12 of the Code of Federal Regulations as follows: BILLING CODE 6714–01–P interested in receiving comments as to how the rule might be improved. Therefore, comments are requested. Following the comment period, the FDIC will make needed changes, if any. Paperwork Reduction Act This rule contains no new collections of information as defined by the Paperwork Reduction Act. See 44 U.S.C. 3501 et seq. Consequently, no information has been submitted to the Office of Management and Budget for review. PART 330—DEPOSIT INSURANCE COVERAGE 1. The authority citation for part 330 continues to read as follows: Authority: 12 U.S.C. 1813(l), 1813(m), 1817(i), 1818(q), 1819(Tenth), 1820(f), 1821(a), 1822(c). [Docket No. FAA–2004–19463; Directorate Identifier 2004–NE–14–AD; Amendment 39– 14029; AD 2005–07–05] [Corrected] On page 16098, in the first column, in compliance paragraph (f), the third line, ‘‘cycles-since-new (CSN), or 3,000 cycles-’’ is corrected to read ‘‘cyclessince-new (CSN) on the TMF assembly, or 3,000 cycles-’’. I Issued in Burlington, MA, on June 2, 2005. Francis A. Favara, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 05–11442 Filed 6–8–05; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Airworthiness Directives; General Electric Company CF6–45A, CF6–50A, CF6–50C, and CF6–50E Series Turbofan Engines; Correction Federal Aviation Administration Federal Aviation Administration, DOT. ACTION: Final rule; correction. 2. Section 330.11(a)(2) is revised to read as follows: § 330.11 Accounts of a corporation, partnership or unincorporated association. (a) * * * (2) Notwithstanding any other provision of this part, any trust or other business arrangement which has filed or is required to file a registration statement with the Securities and Exchange Commission pursuant to section 8 of the Investment Company Act of 1940 (15 U.S.C. 80a–8) or that would be required so to register but for the fact it is not created under the laws Jkt 205001 14 CFR Part 39 AGENCY: I 14:57 Jun 08, 2005 Federal Aviation Administration § 39.13 RIN 2120–AA64 I VerDate jul<14>2003 DEPARTMENT OF TRANSPORTATION Federal Register on March 30, 2005, (70 FR 16096). A descriptive phrase was inadvertently left out of compliance paragraph (f). This document corrects compliance paragraph (f). In all other respects, the original document remains the same. DATES: Effective June 9, 2005. FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer, Engine Certification Office, FAA, Engine and Propeller Directorate, 12 New England Executive Park, Burlington, MA 01803; telephone (781) 238–7192; fax (781) 238–7199. SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 05–6107, that applies to (GE) CF6–45A, CF6–50A, CF6–50C, and CF6–50E series turbofan engines that have not incorporated GE Service Bulletin (SB) No. CF6–50 S/B 72–1239, Revision 1, dated September 24, 2003, or that have not incorporated paragraph 3.B. of GE SB No. CF6–50 S/B 72–1239, original issue, dated May 29, 2003, was published in the Federal Register on March 30, 2005, (70 FR 16096). The following correction is needed: This document makes a correction to Airworthiness Directive (AD) 2005–07–05. That AD applies to General Electric Company (GE) CF6– 45A, CF6–50A, CF6–50C, and CF6–50E series turbofan engines that have not incorporated GE Service Bulletin (SB) No. CF6–50 S/B 72–1239, Revision 1, dated September 24, 2003, or that have not incorporated paragraph 3.B. of GE SB No. CF6–50 S/B 72–1239, original issue, dated May 29, 2003. We published AD 2005–07–05 in the SUMMARY: PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 14 CFR Part 73 [Docket No. FAA–2004–17773; Airspace Docket No. 04–ASW–11] RIN 2120–AA66 Modification of Restricted Areas 5103A, 5103B, and 5103C and Revocation of Restricted Area 5103D; McGregor, NM Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: SUMMARY: This action corrects a final rule (Airspace Docket No. 04–ASW–11) published in the Federal Register on December 13, 2004 (69 FR 72113). That action modified Restricted Areas 5103A E:\FR\FM\09JNR1.SGM 09JNR1

Agencies

[Federal Register Volume 70, Number 110 (Thursday, June 9, 2005)]
[Rules and Regulations]
[Page 33692]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-11442]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2004-19463; Directorate Identifier 2004-NE-14-AD; 
Amendment 39-14029; AD 2005-07-05]
RIN 2120-AA64


Airworthiness Directives; General Electric Company CF6-45A, CF6-
50A, CF6-50C, and CF6-50E Series Turbofan Engines; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2005-07-05. That AD applies to General Electric Company (GE) CF6-
45A, CF6-50A, CF6-50C, and CF6-50E series turbofan engines that have 
not incorporated GE Service Bulletin (SB) No. CF6-50 S/B 72-1239, 
Revision 1, dated September 24, 2003, or that have not incorporated 
paragraph 3.B. of GE SB No. CF6-50 S/B 72-1239, original issue, dated 
May 29, 2003. We published AD 2005-07-05 in the Federal Register on 
March 30, 2005, (70 FR 16096). A descriptive phrase was inadvertently 
left out of compliance paragraph (f). This document corrects compliance 
paragraph (f). In all other respects, the original document remains the 
same.

DATES: Effective June 9, 2005.

FOR FURTHER INFORMATION CONTACT: Karen Curtis, Aerospace Engineer, 
Engine Certification Office, FAA, Engine and Propeller Directorate, 12 
New England Executive Park, Burlington, MA 01803; telephone (781) 238-
7192; fax (781) 238-7199.

SUPPLEMENTARY INFORMATION: A final rule AD, FR Doc. 05-6107, that 
applies to (GE) CF6-45A, CF6-50A, CF6-50C, and CF6-50E series turbofan 
engines that have not incorporated GE Service Bulletin (SB) No. CF6-50 
S/B 72-1239, Revision 1, dated September 24, 2003, or that have not 
incorporated paragraph 3.B. of GE SB No. CF6-50 S/B 72-1239, original 
issue, dated May 29, 2003, was published in the Federal Register on 
March 30, 2005, (70 FR 16096). The following correction is needed:


Sec.  39.13  [Corrected]

0
On page 16098, in the first column, in compliance paragraph (f), the 
third line, ``cycles-since-new (CSN), or 3,000 cycles-'' is corrected 
to read ``cycles-since-new (CSN) on the TMF assembly, or 3,000 cycles-
''.

    Issued in Burlington, MA, on June 2, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 05-11442 Filed 6-8-05; 8:45 am]
BILLING CODE 4910-13-P