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