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 

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. 

(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 

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. 

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Federal Register / Vol. 75, No. 39 / Monday, March 1, 2010 / Proposed Rules 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 

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 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Notice of proposed rulemaking 

by cross-reference to temporary 

regulations. 

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 

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 http:// 

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: 

Background 

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. 

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 

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