Airworthiness Directives; International Aero Engines AG (IAE) V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines; Correction, 9140-9141 [2010-4114]
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9140
Federal Register / Vol. 75, No. 39 / Monday, March 1, 2010 / Proposed Rules
(1) The maximum deposition rate of the
nickel plating in any one plating/baking
cycle must not exceed 0.002-inches-per-hour.
(2) Begin the hydrogen embrittlement relief
bake within 10 hours after application of the
plating, or less than 24 hours after the current
was first applied to the part, whichever is
first.
Exception to Reporting Recommendations in
Certain Service Bulletins
(n) Although Boeing Alert Service Bulletin
737–57A1277, Revision 1, dated November
25, 2003, recommends that operators report
inspection findings to the manufacturer, this
AD does not contain such a reporting
requirement.
New Actions Required by This AD
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Inspections, Measurements, and Overhauls of
the Carriage Spindle
(o) At the applicable times specified in
paragraph (o)(1) or (o)(2) of this AD: Do the
detailed inspection for corrosion, pitting, and
cracking of the carriage spindle, the magnetic
particle inspection for cracking of the
carriage spindle, measurements of the
spindle to determine if it meets the allowable
minimum diameter, and overhauls, and
applicable corrective actions by
accomplishing all the applicable actions
specified in the Accomplishment
Instructions of Boeing Alert Service Bulletin
737–57A1218, Revision 5, dated February 9,
2009. The applicable corrective actions must
be done before further flight. Repeat these
actions thereafter at intervals not to exceed
12,000 flight cycles on the carriage spindle or
8 years, whichever comes first.
(1) For Model 737–100, –200, –200C
airplanes, at the later of the times specified
in paragraph (o)(1)(i) or (o)(1)(ii) of this AD:
(i) Before the accumulation of 12,000 total
flight cycles on the carriage spindle since
new or overhauled, or within 8 years after the
installation of the new or overhauled part,
whichever comes first.
(ii) Within 1 year after the effective date of
this AD.
(2) For Model –300, –400, and –500 series
airplanes, at the later of the times specified
in paragraph (o)(2)(i) or (o)(2)(ii) of this AD:
(i) Before the accumulation of 12,000 total
flight cycles on the carriage spindle since
new or overhauled, or within 8 years after the
installation of the new or overhauled part,
whichever comes first.
(ii) Within 2 years after the effective date
of this AD.
Replacement of the Carriage Spindle
(p) For Model 737–100, –200, –200C
airplanes: Replace the carriage spindle with
a new or documented (for which the service
life, in flight cycles, is known) carriage
spindle, in accordance with Boeing Alert
Service Bulletin 737–57A1218, Revision 5,
dated February 9, 2009, at the later of the
times specified in paragraphs (p)(1) and
(p)(2) of this AD, except as required by
paragraph (r) of this AD. Overhauling the
carriage spindles does not zero-out the flight
cycles. Total flight cycles accumulate since
new.
(1) Before the accumulation of 48,000 total
flight cycles on the new or overhauled
carriage.
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16:32 Feb 26, 2010
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(2) Within three years or 7,500 flight cycles
after the effective date of this AD, whichever
occurs first.
(q) For Model 737–300, –400, and –500
series airplanes: Replace the carriage spindle
with a new or documented (for which the
service life, in flight cycles, is known)
carriage spindle, in accordance with Boeing
Alert Service Bulletin 737–57A1218,
Revision 5, dated February 9, 2009, at the
later of the times specified in paragraphs
(q)(1) and (q)(2) of this AD, except as
required by paragraph (r) of this AD.
Overhauling the carriage spindles does not
zero-out the flight cycles. Total flight cycles
accumulate since new.
(1) Before the accumulation of 48,000 total
flight cycles on the new or overhauled
carriage.
(2) Within six years or 15,000 flight cycles
after the effective date of this AD, whichever
occurs first.
(r) For airplanes with an undocumented
carriage: Do the applicable actions specified
in paragraph (p) or (q) of this AD at the
applicable time specified in paragraph (r)(1)
or (r)(2) of this AD.
(1) For Model 737–100, –200, –200C series
airplanes: Do the actions specified in
paragraph (p) of this AD at the time specified
in paragraph (p)(2) of this AD.
(2) For Model –300, –400, and –500 series
airplanes: Do the actions specified in
paragraph (q) of this AD at the time specified
in paragraph (q)(2) of this AD.
Repetitive Replacements of Carriage Spindle
(s) For all airplanes: Repeat the
replacement of the carriage spindle specified
by paragraph (p) or (q) of this AD, as
applicable, thereafter at intervals not to
exceed 48,000 total flight cycles on the new
or overhauled carriage spindle.
Alternative Methods of Compliance
(AMOCs)
(t)(1) The Manager, Seattle Aircraft
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19. Send information to ATTN:
Nancy Marsh, Aerospace Engineer, Airframe
Branch, ANM–120S, FAA, Seattle Aircraft
Certification Office, 1601 Lind Avenue, SW.,
Renton, Washington 98057–3356; telephone
(425) 917–6440; fax (425) 917–6590. Or,
e-mail information to 9-ANM-Seattle-ACOAMOC-Requests@faa.gov.
(2) To request a different method of
compliance or a different compliance time
for this AD, follow the procedures in 14 CFR
39.19. Before using any approved AMOC on
any airplane to which the AMOC applies,
notify your principal maintenance inspector
(PMI) or principal avionics inspector (PAI),
as appropriate, or lacking a principal
inspector, your local Flight Standards District
Office. The AMOC approval letter must
specifically reference this AD.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair
required by this AD, if it is approved by the
Boeing Commercial Airplanes Organization
Designation Authorization (ODA) that has
been authorized by the Manager, Seattle
ACO, to make those findings. For a repair
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Fmt 4702
Sfmt 4702
method to be approved, the repair must meet
the certification basis of the airplane, and the
approval must specifically refer to this AD.
Issued in Renton, Washington, on February
17, 2010.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2010–4167 Filed 2–26–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2009–1100; Directorate
Identifier 2009–NE–37–AD]
RIN 2120–AA64
Airworthiness Directives; International
Aero Engines AG (IAE) V2500–A1,
V2522–A5, V2524–A5, V2525–D5,
V2527–A5, V2527E–A5, V2527M–A5,
V2528–D5, V2530–A5, and V2533–A5
Turbofan Engines; Correction
AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM); correction.
SUMMARY: The FAA is correcting an
NPRM, which published in the Federal
Register. That NPRM applies to IAE
V2500–A1, V2522–A5, V2524–A5,
V2525–D5, V2527–A5, V2527E–A5,
V2527M–A5, V2528–D5, V2530–A5,
and V2533–A5 turbofan engines. The
docket number is incorrect in three
locations. This document corrects the
docket number in those three locations.
In all other respects, the original
document remains the same.
DATES: The NPRM is corrected as of
March 1, 2010.
FOR FURTHER INFORMATION CONTACT:
Kevin Dickert, Aerospace Engineer,
Engine Certification Office, FAA, 12
New England Executive Park,
Burlington, MA 01803; e-mail:
kevin.dickert@faa.gov; phone: (781)
238–7117, fax: (781) 238–7199.
SUPPLEMENTARY INFORMATION: On
February 12, 2010 (75 FR 6860), we
published a proposed AD, FR Doc.
2010–2999, in the Federal Register.
That AD applies to IAE V2500–A1,
V2522–A5, V2524–A5, V2525–D5,
V2527–A5, V2527E–A5, V2527M–A5,
V2528–D5, V2530–A5, and V2533–A5
turbofan engines. We need to make the
following corrections:
§ 39.13
[Corrected]
On page 6860, in the first column,
under 14 CFR Part 39, ‘‘Docket No.
E:\FR\FM\01MRP1.SGM
01MRP1
Federal Register / Vol. 75, No. 39 / Monday, March 1, 2010 / Proposed Rules
FAA–2009–0544’’ is corrected to read
‘‘Docket No. FAA–2009–1100’’.
On page 6860, in the second column,
under Comments Invited, in the fifth
and sixth line, ‘‘Docket No. FAA–2009–
0544’’ is corrected to read ‘‘Docket No.
FAA–2009–1100’’.
On page 6861, in the third column,
after International Aero Engines AG,
‘‘Docket No. FAA–2009–0544’’ is
corrected to read ‘‘Docket No. FAA–
2009–1100’’.
Issued in Burlington, Massachusetts, on
February 19, 2010.
Francis A. Favara,
Manager, Engine and Propeller Directorate,
Aircraft Certification Service.
[FR Doc. 2010–4114 Filed 2–26–10; 8:45 am]
may be hand-delivered Monday through
Friday between the hours of 8 a.m. and
4 p.m. to: CC:PA:LPD:PR (REG–117501–
09), Courier’s Desk, Internal Revenue
Service, 1111 Constitution Avenue,
NW., Washington, DC, or sent
electronically via the Federal
eRulemaking Portal at https://
www.regulations.gov/ (IRS REG–
117501–09).
FOR FURTHER INFORMATION CONTACT:
Concerning the proposed regulations,
Adrienne Mikolashek at (202) 622–4940;
concerning submission of comments
and a request for a public hearing,
Regina Johnson at (202) 622–7180 (not
toll-free numbers).
SUPPLEMENTARY INFORMATION:
BILLING CODE 4910–13–P
Background
DEPARTMENT OF THE TREASURY
Internal Revenue Service
26 CFR Part 1
[REG–117501–09]
RIN 1545–BI67
Reduced 2009 Estimated Income Tax
Payments for Individuals With Small
Business Income
Internal Revenue Service (IRS),
Treasury.
ACTION: Notice of proposed rulemaking
by cross-reference to temporary
regulations.
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AGENCY:
SUMMARY: In the Rules and Regulations
section of this issue of the Federal
Register, the IRS is issuing temporary
regulations that provide guidance as to
qualified individuals with small
business income who certify that they
satisfy the gross income requirement for
purposes of claiming a reduction in
their required 2009 estimated income
tax payments. The temporary
regulations implement section 1212 of
the American Recovery and
Reinvestment Act of 2009, which
amended section 6654(d) of the Internal
Revenue Code (Code) to provide for
reduced 2009 estimated income tax
payments for certain qualified
individuals. The text of the temporary
regulations also serves as the text of
these proposed regulations.
DATES: Written or electronic comments
and requests for a public hearing must
be received by June 1, 2010.
ADDRESSES: Send submissions to:
CC:PA:LPD:PR (REG–117501–09), Room
5203, Internal Revenue Service, P.O.
Box 7604, Ben Franklin Station,
Washington, DC 20044. Submissions
VerDate Nov<24>2008
16:32 Feb 26, 2010
Jkt 220001
Temporary regulations in the Rules
and Regulations section of this issue of
the Federal Register amend the Income
Tax Regulations (26 CFR part 1) relating
to section 6654. Section 6654 imposes
an addition to tax in the case of an
individual taxpayer’s underpayment of
estimated tax. The temporary
regulations provide guidance on
reduced estimated income tax payments
for qualified individuals with small
business income for any taxable year
beginning in 2009. The text of those
regulations also serves as the text of
these proposed regulations. The
preamble to the temporary regulations
explains the temporary regulations and
these proposed regulations.
Proposed Effective Date
The regulations, as proposed, apply to
any taxable year that begins in 2009 or
after the date of publication of the
Treasury decision adopting these rules
as final regulations in the Federal
Register.
Special Analyses
It has been determined that this notice
of proposed rulemaking is not a
significant regulatory action as defined
in Executive Order 12866. Therefore, a
regulatory assessment is not required. It
also has been determined that section
553(b) of the Administrative Procedure
Act (5 U.S.C. chapter 5) does not apply
to these regulations, and because the
regulations do not impose a collection
of information on small entities, the
Regulatory Flexibility Act (5 U.S.C.
chapter 6) does not apply. Pursuant to
section 7805(f) of the Code, these
regulations have been submitted to the
Chief Counsel for Advocacy of the Small
Business Administration for comment
on its impact on small business.
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Frm 00022
Fmt 4702
Sfmt 4702
9141
Comments and Requests for a Public
Hearing
Before these proposed regulations are
adopted as final regulations,
consideration will be given to any
written (a signed original and eight (8)
copies) or electronic comments that are
submitted timely to the IRS. The IRS
and the Treasury Department request
comments on the substance of the
proposed regulations, as well as on the
clarity of the proposed rules and how
they can be made easier to understand.
All comments will be available for
public inspection and copying. A public
hearing will be scheduled if requested
in writing by any person that timely
submits comments. If a public hearing is
scheduled, notice of the date, time and
place for the public hearing will be
published in the Federal Register.
Drafting Information
The principal author of these
proposed regulations is Adrienne
Mikolashek, Office of the Associate
Chief Counsel, Procedure and
Administration.
List of Subjects in 26 CFR Part 1
Income taxes, Reporting and
recordkeeping requirements.
Proposed Amendments to the
Regulations
Accordingly, 26 CFR part 1 is
proposed to be amended as follows:
PART 1—INCOME TAXES
Paragraph 1. The authority citation
for part 1 continues to read in part as
follows:
Authority: 26 U.S.C. 7805 * * *
Section 1.6654–2 also issued under 26
U.S.C. 6654(d) * * *
Par. 2. Section 1.6654–2 is amended
by revising paragraph (a) introductory
text, and paragraphs (a)(1)(ii) and (f) to
read as follows:
§ 1.6654–2 Exceptions to imposition of the
addition to the tax in the case of
individuals.
(a) [The text of the proposed
amendment to § 1.6654–2(a) is the same
as the text of § 1.6654–2T(a) published
elsewhere in this issue of the Federal
Register].
(1)(i) * * *
(ii) [The text of the proposed
amendment to § 1.6654–2(a)(1)(ii) is the
same as the text of § 1.6654–2T(a)(1)(ii)
published elsewhere in this issue of the
Federal Register].
*
*
*
*
*
(f) [The text of the proposed
amendment to § 1.6654–2(f) is the same
E:\FR\FM\01MRP1.SGM
01MRP1
]]>Agencies
[Federal Register Volume 75, Number 39 (Monday, March 1, 2010)]
[Proposed Rules]
[Pages 9140-9141]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-4114]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-1100; Directorate Identifier 2009-NE-37-AD]
RIN 2120-AA64
Airworthiness Directives; International Aero Engines AG (IAE)
V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5,
V2528-D5, V2530-A5, and V2533-A5 Turbofan Engines; Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM); correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an NPRM, which published in the Federal
Register. That NPRM applies to IAE V2500-A1, V2522-A5, V2524-A5, V2525-
D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5
turbofan engines. The docket number is incorrect in three locations.
This document corrects the docket number in those three locations. In
all other respects, the original document remains the same.
DATES: The NPRM is corrected as of March 1, 2010.
FOR FURTHER INFORMATION CONTACT: Kevin Dickert, Aerospace Engineer,
Engine Certification Office, FAA, 12 New England Executive Park,
Burlington, MA 01803; e-mail: kevin.dickert@faa.gov; phone: (781) 238-
7117, fax: (781) 238-7199.
SUPPLEMENTARY INFORMATION: On February 12, 2010 (75 FR 6860), we
published a proposed AD, FR Doc. 2010-2999, in the Federal Register.
That AD applies to IAE V2500-A1, V2522-A5, V2524-A5, V2525-D5, V2527-
A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan
engines. We need to make the following corrections:
Sec. 39.13 [Corrected]
On page 6860, in the first column, under 14 CFR Part 39, ``Docket
No.
[[Page 9141]]
FAA-2009-0544'' is corrected to read ``Docket No. FAA-2009-1100''.
On page 6860, in the second column, under Comments Invited, in the
fifth and sixth line, ``Docket No. FAA-2009-0544'' is corrected to read
``Docket No. FAA-2009-1100''.
On page 6861, in the third column, after International Aero Engines
AG, ``Docket No. FAA-2009-0544'' is corrected to read ``Docket No. FAA-
2009-1100''.
Issued in Burlington, Massachusetts, on February 19, 2010.
Francis A. Favara,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2010-4114 Filed 2-26-10; 8:45 am]
BILLING CODE 4910-13-P
