Federal Register / Vol. 77, No. 46 / Thursday, March 8, 2012 / Proposed Rules 13993 

Commodity to be reported Unit of measure to be 

used in reporting 

Beginning of 

marketing year 

End of 

marketing 

year 

Soybean Oil—including: Crude (including degummed), once refined, soybean 

salad oil (including refined and further processed by bleaching, deodorizing or winterizing), hydro-genated, packaged oil.

Metric Tons ..................... Oct. 1 .............................. Sept. 30. 

Flaxseed ............................................................................................................ Metric Tons ..................... June 1 ............................. May 31. 

Linseed Oil—including raw, boiled .................................................................... Metric Tons ..................... June 1 ............................. May 31. 

Cottonseed ......................................................................................................... Metric Tons ..................... Aug. 1 ............................. July 31. 

Cottonseed Cake and Meal ............................................................................... Metric Tons ..................... Oct. 1 .............................. Sept. 30. 

Cottonseed Oil—including crude, once refined, cottonseed salad oil (refined 

and further processed by bleaching, deodorizing or winterizing), hydrogenated.

Metric Tons ..................... Oct. 1 .............................. Sept. 30. 

Sunflowerseed Oil—crude, once refined, sunflowerseed salad oil (refined 

and further processed by bleaching, deodorizing or winterizing), hydrogenated.

Metric Tons ..................... Oct. 1 .............................. Sept. 30. 

Cotton—American Pima—Raw, extra long staple ............................................ Running Bales ................ Aug. 1 ............................. July 31. 

Cotton—Upland—Raw, staple length 11⁄16 inches and over ............................ Running Bales ................ Aug. 1 ............................. July 31. 

Cotton—Upland—Raw, staple length 1 inch up to 11⁄16 inches ....................... Running Bales ................ Aug. 1 ............................. July 31. 

Cotton—Upland—Raw, staple length under 1 inch .......................................... Running Bales ................ Aug. 1 ............................. July 31. 

Rice—Long grain, rough (including parboiled) .................................................. Metric Tons ..................... Aug. 1 ............................. July 31. 

Rice—Medium, short and other classes, rough (including parboiled) .............. Metric Tons ..................... Aug. 1 ............................. July 31. 

Rice—Long grain, brown (including parboiled) ................................................. Metric Tons ..................... Aug. 1 ............................. July 31. 

Rice—Medium, short and other classes, brown (including parboiled) .............. Metric Tons ..................... Aug. 1 ............................. July 31. 

Rice—Long grain, milled (including parboiled) .................................................. Metric Tons ..................... Aug. 1 ............................. July 31. 

Rice—Medium, short and other classes, milled (including parboiled, brewer’s 

rice).

Metric Tons ..................... Aug. 1 ............................. July 31. 

Cattle Hides and Skins—Whole cattle hides, (excluding wet blues) ................ Pieces ............................. Jan. 1 .............................. Dec. 31. 

Cattle Hides and Skins—Whole calf skins (excluding wet blues) ..................... Pieces ............................. Jan. 1 .............................. Dec. 31. 

Cattle Hides and Skins—Whole kip skins, (excluding wet blues) ..................... Pieces ............................. Jan. 1 .............................. Dec. 31. 

Cattle Hides and Skins—Cattle, calf, and kip cut into croupons, crops, 

dossets, sides, butts and butt bend (hide equivalent) (excluding wet blues).

Number ........................... Jan. 1 .............................. Dec. 31. 

Cattle Hides and Skins—Cattle, calf and kip, in cuts not otherwise specified; 

pickled/limed (excluding wet blues).

Pounds ............................ Jan. 1 .............................. Dec. 31. 

Cattle, calf and kip, Wet blues—unsplit (whole or sided) hide equivalent ........ Number ........................... Jan. 1 .............................. Dec. 31. 

Cattle, calf and kip, Wet blues—grain splits (whole or sided) hide equivalent Number ........................... Jan. 1 .............................. Dec. 31. 

Cattle, calf and kip, Wet blues—splits, (excluding grain splits) ........................ Pounds ............................ Jan. 1 .............................. Dec. 31. 

Beef—fresh, chilled or frozen muscle cuts/whether or not boxed .................... Metric tons ...................... Jan. 1 .............................. Dec. 31. 

Pork—fresh, chilled or frozen muscle cuts/whether or not boxed .................... Metric tons ...................... Jan. 1 .............................. Dec. 31. 

Dated: January 10, 2012. 

Suzanne E. Heinen, 

Acting Administrator, Foreign Agricultural 

Service. 

[FR Doc. 2012–5486 Filed 3–7–12; 8:45 am] 

BILLING CODE 3410–10–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0221; Directorate 

Identifier 2010–SW–082–AD] 

RIN 2120–AA64 

Airworthiness Directives; Spectrolab 

Nightsun XP Searchlight 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: We propose to adopt a new 

airworthiness directive (AD) for a 

certain Spectrolab Nightsun XP 

Searchlight Assembly (searchlight) 

installed on, but not limited to, Agusta 

S.p.A. (Agusta) Model AB139 and 

Model AW139 helicopters, Sikorsky 

Aircraft Corporation (Sikorsky) Model 

S–92A helicopters, and Eurocopter 

Deutschland GmbH (Eurocopter) Model 

EC135 and Model MBB–BK 117 C–2 

helicopters. This proposed AD would 

require, before further flight, inserting 

information into the Normal Procedures 

section of the Rotorcraft Flight Manual 

(RFM), a daily check of the searchlight, 

and at a specified time interval or if you 

find certain conditions, modifying any 

affected searchlight gimbal assembly. 

This proposed AD is prompted by a 

report of a searchlight vibrating and an 

investigation that revealed that the 

gimbal azimuth top nut was loose. A 

loose nut, if not detected and corrected, 

could result in a gap between the rubber 

edging of the top shroud and the gimbal 

frame, leading to degredation of 

pointing accuracy and stability 

performance of the searchlight, and 

excessive vibration. If the nut were to 

entirely disengage, the searchlight could 

disconnect partially or totally from the 

helicopter, resulting in damage to the 

helicopter and injury to persons on the 

ground. 

DATES: We must receive comments on 

this proposed AD by May 7, 2012. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Docket: Go to 

http://www.regulations.gov. Follow the 

online instructions for sending your 

comments electronically. 

• Fax: 202–493–2251. 

• Mail: Send comments to the U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590–0001. 

• Hand Delivery: Deliver to the 

‘‘Mail’’ address between 9 a.m. and 

5 p.m., Monday through Friday, except 

Federal holidays. 

Examining the AD Docket: You may 

examine the AD docket on the Internet 

at http://www.regulations.gov or in 

person at the Docket Operations Office 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

The AD docket contains this proposed 

AD, the economic evaluation, any 


wreier-aviles on DSK5TPTVN1PROD with PROPOSALS
13994 Federal Register / Vol. 77, No. 46 / Thursday, March 8, 2012 / Proposed Rules 

comments received, and other 

information. The street address for the 

Docket Operations Office (telephone 

800–647–5527) is in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

For service information identified in 

this proposed AD, contact Spectrolab, 

Inc. ATTN: Saul Vargas, 12500 

Gladstone Ave., Sylmar, CA 91342, 

telephone (818) 365–4611, fax (818) 

361–5102, or on the internet at http:// 

www.spectrolab.com. You may review a 

copy of the referenced service 

information at the FAA, Office of the 

Regional Counsel, Southwest Region, 

2601 Meacham Blvd., Room 663, Fort 

Worth, Texas 76137. 

FOR FURTHER INFORMATION CONTACT: Jim 

Grigg, Manager, Safety Management 

Group, DOT/FAA, 2601 Meacham Blvd., 

Fort Worth, Texas 76137; telephone: 

(817) 222–5126; fax: (817) 222–5961; 

email: jim.grigg@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

We invite you to participate in this 

rulemaking by submitting written 

comments, data, or views. We also 

invite comments relating to the 

economic, environmental, energy, or 

federalism impacts that might result 

from adopting the proposals in this 

document. The most helpful comments 

reference a specific portion of the 

proposal, explain the reason for any 

recommended change, and include 

supporting data. To ensure the docket 

does not contain duplicate comments, 

commenters should send only one copy 

of written comments, or if comments are 

filed electronically, commenters should 

submit only one time. 

We will file in the docket all 

comments that we receive, as well as a 

report summarizing each substantive 

public contact with FAA personnel 

concerning this proposed rulemaking. 

Before acting on this proposal, we will 

consider all comments we receive on or 

before the closing date for comments. 

We will consider comments filed after 

the comment period has closed if it is 

possible to do so without incurring 

expense or delay. We may change this 

proposal in light of the comments we 

receive. 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued AD No.: 2010– 

0237R2, dated December 14, 2010, to 

correct an unsafe condition for the 

Spectrolab Nightsun XP Searchlights 

installed on the following model 

helicopters: Agusta AB139 and AW139, 

Sikorsky S–92A, and Eurocopter MBB– 

BK 117 C2 and EC 135 series, if 

equipped with Spectrolab Nightsun XP 

Gimbal Assembly part number (P/N) 

033295 series, used on Spectrolab 

Nightsun XP Searchlight Assembly 

System P/Ns 033338 series. EASA 

advises that a maintenance organization 

reported an incident where vibration 

was associated with the Spectrolab 

Nightsun XP Searchlight. EASA states 

in its AD that an investigation revealed 

the Gimbal Azimuth Top Hex Nut was 

loose. This condition, if not detected 

and corrected, could lead to a gap 

between the rubber edging of the top 

shroud and the Gimbal frame, resulting 

in degredation of pointing accuracy and 

stability performance, and pose 

excessive vibration. If the nut were to 

entirely disengage, the Searchlight/ 

Gimbal could disconnect from the 

helicopter and remain attached solely 

by the internal cable harness or separate 

totally, resulting in damage to the 

helicopter or injury to persons on the 

ground. 

FAA’s Determination 

We are proposing this AD because we 

evaluated all known relevant 

information and determined that an 

unsafe condition exists and is likely to 

exist or develop on other products of the 

same type design. 

Related Service Information 

Spectrolab has issued Nightsun XP 

Searchlight Safety and Service Bulletin 

#SL 0810–01, Amendment #2, dated 

September 24, 2010 (SB), which 

describes a design change that 

incorporates two positive locking 

mechanisms: a torque value and safety 

wire applied to the nut. These locking 

mechanisms prevent the gimbal azimuth 

top nut from loosening and allowing the 

center shaft to rotate out. The following 

table lists the Nightsun systems 

containing one of these gimbal 

assemblies by P/N and revision: 

AFFECTED SYSTEMS AND P/N 

System P/N Nomenclature Affected revisions 

033338 ................................. Nightsun XP Searchlight System ................................................................................. A through D. 

033338–3 ............................. Nightsun XP Searchlight System ................................................................................. A through D. 

033338–4 ............................. Nightsun XP Searchlight System ................................................................................. A through D. 

033704 ................................. IFCO Nightsun XP Searchlight System ....................................................................... A through C. 

033704–1 ............................. IFCO Nightsun XP Searchlight System ....................................................................... A through C. 

Spectrolab has also issued Nightsun 

XP Searchlight System Kit and 

Procedure to Incorporate EASA AD 

2010–0183 Conformance, 034374 

Revision NC, approved September 28, 

2010 (Kit and Procedure). Once 

modified in accordance with the Kit and 

Procedure, the Nightsun XP gimbals are 

re-identified with a new nameplate and 

overlay from a P/N 033295–1 to 

033295–3, or P/N 033295–2 to 033295– 

4. 

EASA classified this modification as 

mandatory and issued EASA AD No.: 

2010–0237R2, dated December 14, 2010, 

to ensure the continued airworthiness of 

helicopters with the affected system 

installed. 

Proposed AD Requirements 

This proposed AD would require: 

• Before further flight, inserting a 

copy of the SB into the Normal 

Procedures section of the RFM. 

• Before the first flight of each day, 

visually checking the searchlight 

installation for a gap between the top 

shroud rubber edging, P/N 033381, and 

the side covers, P/N 033286, with slight 

pressure applied to either side of the 

searchlight. The edging should remain 

in physical contact with the side covers 

when slight pressure is applied to the 

searchlight. If the edging does not 

remain in contact, the gimbal assembly 

must be modified and re-identified. An 

owner/operator (pilot) holding at least a 

Private Pilot Certificate may perform 

this visual check and must show 

compliance by updating the helicopter 

maintenance records in accordance with 

14 CFR 43.9(a)(1)–(4) and 

91.417(a)(2)(v). 

• Within 100 hours time-in-service 

(TIS), modify and re-identify the gimbal 

assembly in accordance with the Kit and 

Procedure, steps 1 through 13. 


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Federal Register / Vol. 77, No. 46 / Thursday, March 8, 2012 / Proposed Rules 13995 

Differences Between This Proposed AD 

and the Service Information 

The differences between this AD and 

the EASA AD are: 

• We require modifying and reidentifying the searchlight within 100 

hours TIS, while the EASA AD imposes 

a calendar date for compliance. 

• The EASA AD requires contacting 

the design (change) approval holder if 

discrepancies are found during the 

inspection of the searchlight 

installation, and we do not require this 

action. 

Costs of Compliance 

We estimate that this proposed AD 

would affect 6 helicopters of U.S. 

registry. We also estimate that it would 

take minimal time to insert the service 

bulletin into the RFM, and about 3.0 

work hours per helicopter to modify the 

searchlight. At an average labor rate of 

$85 per work hour, this amounts to $255 

per helicopter. Required parts would 

cost about $1,000 per helicopter. Based 

on these figures, we estimate the total 

cost impact of the proposed AD on U.S. 

operators to be $1,255 per helicopter, or 

$7,530 for the fleet. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. ‘‘Subtitle VII: 

Aviation Programs,’’ describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in ‘‘Subtitle VII, 

Part A, Subpart III, Section 44701: 

General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We determined that this proposed AD 

would not have federalism implications 

under Executive Order 13132. This 

proposed AD would not have a 

substantial direct effect on the States, on 

the relationship between the national 

Government and the States, or on the 

distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed, I certify 

this proposed regulation: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); 

3. Will not affect intrastate aviation in 

Alaska to the extent that it justifies 

making a regulatory distinction; and 

4. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

We prepared an economic evaluation 

of the estimated costs to comply with 

this proposed AD and placed it in the 

AD docket. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

The Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 14 CFR part 

39 as follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

Spectrolab Nightsun XP Searchlight:

Docket No. FAA–2012–0221; Directorate 

Identifier 2010–SW–082–AD. 

(a) Applicability 

This AD applies to Spectrolab Nightsun XP 

Searchlight Assembly Systems with gimbal 

assembly part number (P/N) 033295–1 or 

033295–2, installed on, but not limited to, 

Agusta S.p.A. Model AB139 and Model 

AW139 helicopters, Sikorsky Aircraft 

Corporation Model S–92A helicopters, and 

Eurocopter Deutschland GmbH Model EC135 

and Model MBB–BK 117 C–2 helicopters, 

certificated in any category. The searchlight 

assembly system P/Ns and revision level 

using one of the two affected gimbal 

assembly P/Ns are listed in Table 1 of this 

AD. 

TABLE 1—AFFECTED SYSTEMS AND P/N 

System P/N Nomenclature Affected revisions 

033338 ................................................................ Nightsun XP Searchlight System .......................................................... A through D. 

033338–3 ............................................................ Nightsun XP Searchlight System .......................................................... A through D. 

033338–4 ............................................................ Nightsun XP Searchlight System .......................................................... A through D. 

033704 ................................................................ IFCO Nightsun XP Searchlight System ................................................ A through C. 

033704–1 ............................................................ IFCO Nightsun XP Searchlight System ................................................ A through C. 

(b) Unsafe Condition 

This proposed AD is being issued to 

prevent the Searchlight/Gimbal from 

disconnecting from the helicopter and 

remaining attached soley by the internal 

cable harness, or separating totally, resulting 

in damage to the helicopter or injury to 

people on the ground. 

(c) Compliance 

You are responsible for performing each 

action required by this AD within the 

specified compliance time unless it has 

already been accomplished prior to that time. 

(d) Required Actions 

(1) Before further flight, insert a copy of 

Nightsun XP Searchlight Safety and Service 

Bulletin #SL 0810–01, Amendment #2, dated 

September 24, 2010, into the Normal 

Procedures section of the Rotorcraft Flight 

Manual. 

(2) Before the first flight of each day, 

visually check the searchlight installation for 

a gap between the top shroud rubber edging, 

P/N 033381, and the side covers, P/N 033286, 

with slight pressure applied to either side of 

the searchlight. The edging must remain in 

physical contact with the side covers when 

slight pressure is applied to the searchlight. 

(3) The actions required by paragraph 

(d)(2) of this AD may be performed by the 

owner/operator (pilot) holding at least a 

Private Pilot Certificate, and must be entered 

into the helicopter maintenance records in 

accordance with 14 CFR 43.9(a)(1)–(4) and 

91.417(a)(2)(v). The record must be 

maintained as required by 14 CFR 91.417, 

121.380, or 135.439. 

(4) If the edging does not remain in 

physical contact with the side cover when 

slight pressure is applied to the searchlight 

in accordance with the requirements of 

paragraph (d)(2) of this AD, before further 

flight, with an affected Spectrolab Nightsun 

XP Searchlight assembly system installed, 


wreier-aviles on DSK5TPTVN1PROD with PROPOSALS
13996 Federal Register / Vol. 77, No. 46 / Thursday, March 8, 2012 / Proposed Rules 

modify and re-identify the gimbal assembly 

in accordance with paragraph (d)(5) of this 

AD. 

(5) Within 100 hours time-in-service (TIS), 

modify and re-identify the gimbal assembly 

in accordance with Nightsun XP Searchlight 

System Kit and Procedure to Incorporate 

EASA AD 2010–0183 Conformance, 034374 

Revision NC, approved September 28, 2010, 

steps 1 through 13. 

(6) Accomplishing paragraph (d)(5) of this 

AD is terminating action for the requirements 

of this AD. 

(e) Alternative Methods of Compliance 

(AMOC) 

(1) The Manager, Safety Management 

Group, FAA, may approve AMOCs for this 

AD. Send your proposal to: Jim Grigg, 2601 

Meacham Blvd., Fort Worth, Texas 76137; 

telephone: (817) 222–5126; fax: 817–222– 

5961; email: jim.grigg@faa.gov. 

(2) For operations conducted under a Part 

119 operating certificate or under Part 91, 

Subpart K, we suggest that you notify your 

principal inspector, or lacking a principal 

inspector, the manager of the local flight 

standards district office or certificate holding 

district office before operating any aircraft 

complying with this AD through an AMOC. 

(f) Additional Information 

For service information identified in this 

AD, contact Spectrolab, Inc. ATTN: Saul 

Vargas, 12500 Gladstone Ave., Sylmar, CA 

91342, telephone (818) 365–4611, fax (818) 

361–5102, or on the internet at http:// 

www.spectrolab.com. You may review a copy 

of this information at the FAA, Office of the 

Regional Counsel, Southwest Region, 2601 

Meacham Blvd., Room 663, Fort Worth, 

Texas 76137. 

(g) The subject of this AD is addressed in 

European Aviation Safety Agency AD No.: 

2010–0237R2, dated December 14, 2010. 

(h) Subject 

Joint Aircraft Service Component (JASC) 

Code: 3340, Exterior Lighting. 

Issued in Fort Worth, Texas, on February 

24, 2012. 

Lance T. Gant, 

Acting Manager, Rotorcraft Directorate, 

Aircraft Certification Service. 

[FR Doc. 2012–5621 Filed 3–7–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[REG–157714–06] 

RIN 1545–BG43 

Determination of Governmental Plan 

Status; Correction 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Correction to a correction of 

notice of public hearing on an advance 

notice of proposed rulemaking; 

correction. 

SUMMARY: This document corrects a 

correction to a notice of public hearing 

on an advance proposed rulemaking 

(REG–157714–06) that was published in 

the Federal Register on Thursday, 

March 1, 2012 (77 FR 12514) relating to 

the determination of governmental 

plans. 

FOR FURTHER INFORMATION CONTACT: 

Concerning the proposed regulations, 

Pamela Kinard at (202) 622–6060, and 

regarding the submission of public 

comments and the public hearing, Ms. 

Oluwafunmilayo (Funmi) Taylor, at 

(202) 622–7180 (not toll-free numbers). 

SUPPLEMENTARY INFORMATION: 

Background 

The notice of public hearing on an 

advance notice proposed rulemaking 

(REG–157714–06) that is the subject of 

this correction is under section 414(d) of 

the Internal Revenue Code. 

Need for Correction 

As published, REG–157714–06, 

contains an error that may prove to be 

misleading and is in need of 

clarification. 

Correction of Publication 

Accordingly, the publication of the 

correction to a notice of public hearing 

on an advance proposed rulemaking 

(REG–157714–06) which was the subject 

of FR. Doc. 2012–4905, is corrected as 

follows: 

1. On page 12514, column 1, in the 

preamble, under the caption 

‘‘Background:’’, line three, the language 

‘‘(REG–133233–08) that is the subject 

of’’ is corrected to read ‘‘(REG–157714– 

06) that is the subject of’’. 

LaNita Van Dyke, 

Chief, Publications and Regulations Branch, 

Legal Processing Division, Associate Chief 

Counsel (Procedure and Administration). 

[FR Doc. 2012–5595 Filed 3–7–12; 8:45 am] 

BILLING CODE 4830–01–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[REG–133223–08] 

RIN 1545–BI19 

Indian Tribal Government Plans; 

Correction 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Correction to a correction of 

notice of public hearing on an advance 

notice of proposed rulemaking; 

correction. 

SUMMARY: This document corrects a 

correction to a notice of public hearing 

on an advance proposed rulemaking 

(REG–133223–08) that was published in 

the Federal Register on Wednesday, 

February 29, 2012 (77 FR 12226) 

relating to Indian tribal government 

plans. 

FOR FURTHER INFORMATION CONTACT: 

Concerning the proposed regulations, 

Pamela Kinard at (202) 622–6060, and 

regarding the submission of public 

comments and the public hearing, Ms. 

Oluwafunmilayo (Funmi) Taylor, at 

(202) 622–7180 (not toll-free numbers). 

SUPPLEMENTARY INFORMATION: 

Background 

The notice of public hearing on an 

advance notice proposed rulemaking 

(REG–133223–08) that is the subject of 

this correction is under section 414(d) of 

the Internal Revenue Code. 

Need for Correction 

As published, REG–133223–08, 

contains errors that may prove to be 

misleading and are in need of 

clarification. 

Correction of Publication 

Accordingly, the publication of the 

correction to a notice of public hearing 

on an advance proposed rulemaking 

(REG–133223–08) which was the subject 

of FR. Doc. 2012–4850, is corrected as 

follows: 

1. On page 12226, column 3, in the 

preamble, under the caption SUMMARY:, 

line three, the language ‘‘proposed 

rulemaking (REG–133233–08)’’ is 

corrected to read ‘‘proposed rulemaking 

(REG–133223–08)’’ 

2. On page 12226, column 3, in the 

preamble, under the paragraph heading 

‘‘Background’’, line three, the language 

‘‘(REG–133233–08) that is the subject 

of’’ is corrected to read ‘‘REG–133223– 

08) that is the subject of’’. 

3. On page 12226, column 3, in the 

preamble, under the paragraph heading 

‘‘Correction of Publication’’, line three, 

the language ‘‘proposed rulemaking 

(REG–133233–08)’’ is corrected to read 

‘‘proposed rulemaking (REG–133223– 

08)’’. 

LaNita Van Dyke, 

Chief, Publications and Regulations Branch, 

Legal Processing Division, Associate Chief 

Counsel (Procedure and Administration). 

[FR Doc. 2012–5597 Filed 3–7–12; 8:45 am] 

BILLING CODE 4830–01–P 


wreier-aviles on DSK5TPTVN1PROD with PROPOSALS