Federal Register / Vol. 75, No. 86 / Wednesday, May 5, 2010 / Rules and Regulations 24389 

flexibility to structure the terms and 

conditions for term deposit offerings to 

minimize any adverse effects on small 

institutions. The Board will set terms 

and conditions of term deposit offerings 

that promote the access of small 

institutions to term deposits while still 

maintaining the effectiveness of term 

deposits as a tool to implement 

monetary policy. These steps could 

include those suggested by commenters, 

such as low minimum bid amounts, 

aggregate limits, and noncompetitive 

tenders. 

VIII. Paperwork Reduction Act 

In accordance with the Paperwork 

Reduction Act (PRA) of 1995 (44 U.S.C. 

3506; 5 CFR 1320 Appendix A.1), the 

Board reviewed the final rule under the 

authority delegated to the Board by the 

Office of Management and Budget 

(OMB). The final rule contains no 

collections of information subject to the 

PRA. 

List of Subjects in 12 CFR Part 204 

Banks, banking, Reporting and 

recordkeeping requirements. 

Authority and Issuance 

■ For the reasons set forth in the 

preamble, the Board is proposing to 

amend 12 CFR part 204 as follows: 

PART 204—RESERVE 

REQUIREMENTS OF DEPOSITORY 

INSTITUTIONS (REGULATION D) 

■ 1. The authority citation for Part 204 

continues to read as follows: 

Authority: 12 U.S.C. 248(a), 248(c), 371a, 

461, 601, 611, and 6105. 

■ 2. Amend § 204.2 by adding paragraph 

(dd) to read as follows: 

§ 204.2 Definitions. 

* * * * * 

(dd) Term deposit means those funds 

of an eligible institution that are 

maintained by that institution for a 

specified maturity at a Federal Reserve 

Bank pursuant to section 204.10(e) of 

this part. 

■ 3. Section 204.10 is amended by 

revising paragraph (b)(3) and by adding 

a new paragraph (e) to read as follows: 

§ 204.10 Payment of interest on balances. 

* * * * * 

(b) * * * 

(3) For required reserve balances, 

excess balances, and term deposits, at 

any other rate or rates as determined by 

the Board from time to time, not to 

exceed the general level of short-term 

interest rates. For purposes of this 

subsection, ‘‘short-term interest rates’’ 

are rates on obligations with maturities 

of no more than one year, such as the 

primary credit rate and rates on term 

federal funds, term repurchase 

agreements, commercial paper, term 

Eurodollar deposits, and other similar 

instruments. 

* * * * * 

(e) Term deposits. (1) A Federal 

Reserve Bank may accept term deposits 

from eligible institutions under the 

provisions of this paragraph (e) subject 

to such terms and conditions as the 

Board may establish from time to time, 

including but not limited to conditions 

regarding the maturity of the term 

deposits being offered, maximum and 

minimum amounts that may be 

maintained by an eligible institution in 

a term deposit, the interest rate or rates 

offered, early withdrawal of term 

deposits, pledging term deposits as 

collateral and, if term deposits are 

offered through an auction mechanism, 

the size of the offering, maximum and 

minimum bid amounts, and other 

relevant terms. 

(2) A term deposit will not satisfy any 

institution’s required reserve balance or 

contractual clearing balance. 

(3) A term deposit may not be used for 

general payments or settlement 

activities. 

By order of the Board of Governors of the 

Federal Reserve System, April 29, 2010. 

Jennifer J. Johnson, 

Secretary of the Board. 

[FR Doc. 2010–10483 Filed 5–4–10; 8:45 am] 

BILLING CODE 6210–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0435; Directorate 

Identifier 2010–NM–084–AD; Amendment 

39–16283; AD 2010–10–04] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc. Model DHC–8–400 Series 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

Operators of DHC–8 400 Series aeroplanes 

have been reporting chafing of wires in the 

AC wire harnesses located along the lower 

wing shroud on either wing resulting in a 

loss of various system services. Chafed wires 

may lead to arcing, local overheating and AC 

generator failure. The AC generators provide 

power to the anti-icing heaters, including 

pitot/static heater, engine adapter heater, and 

propeller heater. Failure of both AC 

generators would result in the loss of these 

systems and poses a safety concern. 

* * * * * 

Loss of both AC generators could lead 

to unannunciated loss of heat to both 

engine inlets, which could lead to loss 

of power in both engines during icing 

conditions. This AD requires actions 

that are intended to address the unsafe 

condition described in the MCAI. 

DATES: This AD becomes effective May 

20, 2010. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of May 20, 2010. 

We must receive comments on this 

AD by June 21, 2010. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

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

instructions for submitting comments. 

• Fax: (202) 493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue, SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M– 

30, West Building Ground Floor, Room 

W12–40, 1200 New Jersey Avenue, SE., 

Washington, DC, 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 AD, the regulatory 

evaluation, any 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 FURTHER INFORMATION CONTACT: 

Craig Yates, Aerospace Engineer, 

Airframe and Mechanical Systems 

Branch, ANE–171, FAA, New York 

Aircraft Certification Office, 1600 

Stewart Avenue, Suite 410, Westbury, 


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New York 11590; telephone (516) 228– 

7355; fax (516) 794–5531. 

SUPPLEMENTARY INFORMATION: 

Discussion 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

for Canada, has issued Canadian 

Airworthiness Directive CF–2010–08, 

dated March 16, 2010 (referred to after 

this as ‘‘the MCAI’’), to correct an unsafe 

condition for the specified products. 

The MCAI states: 

Operators of DHC–8 400 Series aeroplanes 

have been reporting chafing of wires in the 

AC wire harnesses located along the lower 

wing shroud on either wing resulting in a 

loss of various system services. Chafed wires 

may lead to arcing, local overheating and AC 

generator failure. The AC generators provide 

power to the anti-icing heaters, including 

pitot/static heater, engine adapter heater, and 

propeller heater. Failure of both AC 

generators would result in the loss of these 

systems and poses a safety concern. 

Investigation has revealed that at four 

wiring harness tie down mount locations, the 

blind fasteners used to attach the tie down 

mount base were found to have protruding 

stems which chafed through the wire 

insulation leading to arcing damage. In 

addition, the wire chafing along the wing rear 

spar lower shroud has been attributed to 

sagging wire bundles resting on the structure 

and insufficient support in low clearance 

areas. 

This directive mandates the replacement of 

the blind fasteners with solid rivets, and to 

inspect for and rectify damaged wiring along 

the wing lower shroud. 

Loss of both AC generators could lead 

to unannunciated loss of heat to both 

engine inlets, which could lead to loss 

of power in both engines during icing 

conditions. The required actions also 

include a detailed inspection for 

damage and chafing of the wires in the 

wiring harness installation, and the 

Teflon tubing if necessary. The 

corrective actions (rectifying) include 

replacement or repair of the chafed or 

damaged wire or Teflon tubing. You 

may obtain further information by 

examining the MCAI in the AD docket. 

Relevant Service Information 

Bombardier has issued Alert Service 

Bulletin A84–24–44, Revision A, dated 

February 2, 2010; and Repair Drawing 

8/4–24–011, Issue 2, dated January 21, 

2010. The actions described in this 

service information are intended to 

correct the unsafe condition identified 

in the MCAI. 

FAA’s Determination and Requirements 

of This AD 

This product has been approved by 

the aviation authority of another 

country, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with the State of 

Design Authority, we have been notified 

of the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all pertinent 

information and determined the unsafe 

condition exists and is likely to exist or 

develop on other products of the same 

type design. 

Differences Between the AD and the 

MCAI or Service Information 

We have reviewed the MCAI and 

related service information and, in 

general, agree with their substance. But 

we might have found it necessary to use 

different words from those in the MCAI 

to ensure the AD is clear for U.S. 

operators and is enforceable. In making 

these changes, we do not intend to differ 

substantively from the information 

provided in the MCAI and related 

service information. 

We might also have required different 

actions in this AD from those in the 

MCAI in order to follow FAA policies. 

Any such differences are highlighted in 

a Note within the AD. 

FAA’s Determination of the Effective 

Date 

An unsafe condition exists that 

requires the immediate adoption of this 

AD. The FAA has found that the risk to 

the flying public justifies waiving notice 

and comment prior to adoption of this 

rule because the chafing of a wire 

bundle could result in an electrical 

short and potential loss of several 

functions essential for safe flight, 

including both AC generators. 

Therefore, we determined that notice 

and opportunity for public comment 

before issuing this AD are impracticable 

and that good cause exists for making 

this amendment effective in fewer than 

30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2010–0435; 

Directorate Identifier 2010–NM–084– 

AD’’ at the beginning of your comments. 

We specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this AD because of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. 

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 AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

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 above, I 

certify this AD: 

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); and 

3. 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 a regulatory evaluation 

of the estimated costs to comply with 

this 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. 

Adoption of the Amendment 

■ Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 


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Federal Register / Vol. 75, No. 86 / Wednesday, May 5, 2010 / Rules and Regulations 24391 

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 AD: 

2010–10–04 Bombardier, Inc.: Amendment 

39–16283. Docket No. FAA–2010–0435; 

Directorate Identifier 2010–NM–084–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective May 20, 2010. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Bombardier, Inc. 

Model DHC–8–400, –401, and –402 

airplanes, serial numbers 4001 through 4169 

inclusive, certificated in any category. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 24: Electrical Power. 

Reason 

(e) The mandatory continued airworthiness 

information (MCAI) states: 

Operators of DHC–8 400 Series aeroplanes 

have been reporting chafing of wires in the 

AC wire harnesses located along the lower 

wing shroud on either wing resulting in a 

loss of various system services. Chafed wires 

may lead to arcing, local overheating and AC 

generator failure. The AC generators provide 

power to the anti-icing heaters, including 

pitot/static heater, engine adapter heater, and 

propeller heater. Failure of both AC 

generators would result in the loss of these 

systems and poses a safety concern. 

Investigation has revealed that at four 

wiring harness tie down mount locations, the 

blind fasteners used to attach the tie down 

mount base were found to have protruding 

stems which chafed through the wire 

insulation leading to arcing damage. In 

addition, the wire chafing along the wing rear 

spar lower shroud has been attributed to 

sagging wire bundles resting on the structure 

and insufficient support in low clearance 

areas. 

This directive mandates the replacement of 

the blind fasteners with solid rivets, and to 

inspect for and rectify damaged wiring along 

the wing lower shroud. 

Loss of both AC generators could lead to 

unannunciated loss of heat to both engine 

inlets, which could lead to loss of power in 

both engines during icing conditions. The 

required actions also include a detailed 

inspection for damage and chafing of the 

wires in the wiring harness installation, and 

the Teflon tubing if necessary. The corrective 

actions (rectifying) include replacement or 

repair of the chafed or damaged wire or 

Teflon tubing. 

Compliance 

(f) You are responsible for having the 

actions required by this AD performed within 

the compliance times specified, unless the 

actions have already been done. 

Replacement of Blind Fasteners, Inspection 

for Chafing at Four Wiring Harness Tie 

Down Mount Locations and Corrective 

Action 

(g) Within 200 flight hours after the 

effective date of this AD: Replace the blind 

fasteners installed at the four wiring harness 

tie down mount locations with solid rivets; 

and do a detailed inspection for chafing and 

damage of the wires and, as applicable, of 

any Teflon tubing and do all applicable 

corrective actions; in accordance with 

paragraph B.(6) of the Accomplishment 

Instructions of Bombardier Alert Service 

Bulletin A84–24–44, Revision A, dated 

February 2, 2010. Do all applicable corrective 

actions before further flight. 

Inspection of AC Feeder Cables Along Lower 

Wing Shroud and Corrective Action 

(h) At the applicable time in paragraph 

(h)(1) or (h)(2) of this AD: Do a detailed 

inspection of the wiring harness installation 

along the wing rear spar lower shroud for any 

chafing and damage, and do all applicable 

corrective actions, in accordance with the 

Accomplishment Instructions of Bombardier 

Alert Service Bulletin A84–24–44, Revision 

A, dated February 2, 2010. Do all applicable 

corrective actions before further flight. 

(1) For airplanes with AC feeder cables not 

covered with protective Teflon tubing 

(Modsum Number IS4Q2450001 or 

production Modsum 4Q109946 not 

incorporated): Within 600 flight hours after 

the effective date of this AD. 

(2) For airplanes with AC feeder cables 

covered with protective Teflon tubing 

(Modsum Number IS4Q2450001 or 

production Modsum 4Q109946 

incorporated): Within 4,000 flight hours after 

the effective date of this AD. 

(i) For airplanes on which the temporary 

repair specified in Bombardier Repair 

Drawing 8/4–24–011, Issue 2, dated January 

21, 2010, has been done: Within 600 flight 

hours after accomplishing the temporary 

repair or 60 flight hours after the effective 

date of this AD, whichever occurs later, do 

the permanent repair or replace the wiring, 

in accordance with Bombardier Repair 

Drawing 8/4–24–011, Issue 2, dated January 

21, 2010. 

Actions According to Previous Issue of 

Service Information 

(j) Actions done before the effective date of 

this AD in accordance with Bombardier Alert 

Service Bulletin A84–24–44, dated January 

27, 2010, are acceptable for compliance with 

the corresponding requirements of 

paragraphs (g) and (h) of this AD. 

(k) Actions done before the effective date 

of this AD in accordance with any 

modification summary identified in Table 1 

of this AD are acceptable for compliance with 

the corresponding requirements of paragraph 

(g) of this AD. 

TABLE 1—MODIFICATION SUMMARIES

Bombardier modification summary— Revision— Dated— 

IS4Q5700013 ................................................................................................................................................... A January 12, 2010. 

IS4Q5700013 ................................................................................................................................................... B January 20, 2010. 

IS4Q5700013 ................................................................................................................................................... C January 27, 2010. 

Reporting Requirement 

(l) Submit a report of the findings (both 

positive and negative) of the inspection 

required by paragraph (h) of this AD to 

Bombardier Technical Help Desk; telephone 

416–375–4000; e-mail 

thd.qseries@aero.bombardier.com; at the 

applicable time specified in paragraph (l)(1) 

or (l)(2) of this AD. Use Figures 1 and 2 

(Feedback Form) of Bombardier Alert Service 

Bulletin A84–24–44, Revision A, dated 

February 2, 2010, to submit the report. The 

report must include the inspection results, a 

description of any discrepancies found, the 

airplane serial number, and the number of 

landings and flight hours on the airplane. 

(1) If the inspection was done on or after 

the effective date of this AD: Submit the 

report within 14 days after the inspection. 

(2) If the inspection was accomplished 

prior to the effective date of this AD: Submit 

the report within 14 days after the effective 

date of this AD. 

FAA AD Differences 

Note 1: This AD differs from the MCAI 

and/or service information as follows: The 

MCAI does not specify a compliance time for 

doing a permanent repair or replacement for 

airplanes on which a temporary repair is 

done. This AD requires that the temporary 

repair is replaced by a permanent repair or 

replacement of the wiring. We have 

coordinated this difference with Transport 

Canada Civil Aviation (TCCA). 

Other FAA AD Provisions 

(m) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, ANE–170, New York 

Aircraft Certification Office, FAA, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 


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24392 Federal Register / Vol. 75, No. 86 / Wednesday, May 5, 2010 / Rules and Regulations 

CFR 39.19. Send information to Attn: 

Program Manager, Continuing Operational 

Safety, FAA, New York ACO, 1600 Stewart 

Avenue, Suite 410, Westbury, New York, 

11590; telephone 516–228–7300; fax 516– 

794–5531. 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. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act 

(44 U.S.C. 3501 et seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(n) Refer to MCAI Canadian Airworthiness 

Directive CF–2010–08, dated March 16, 2010; 

Bombardier Alert Service Bulletin A84–24– 

44, Revision A, dated February 2, 2010; and 

Bombardier Repair Drawing 8/4–24–011, 

Issue 2, dated January 21, 2010; for related 

information. 

Material Incorporated by Reference 

(o) You must use Bombardier Alert Service 

Bulletin A84–24–44, Revision A, dated 

February 2, 2010; and Bombardier Repair 

Drawing 8/4–24–011, Issue 2, dated January 

21, 2010; as applicable; to do the actions 

required by this AD, unless the AD specifies 

otherwise. Bombardier Repair Drawing 8/4– 

24–011, Issue 2, dated January 21, 2010, 

contains the following effective pages: 

Page No. 

Revision 

level shown 

on page 

Date shown on page 

1, 3 ................................................................................................................................................................. 2 January 21, 2010.* 

2, 4–7 ............................................................................................................................................................. 1 January 18, 2010.* 

* Only the first page of this repair drawing contains the issue dates. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Bombardier, Inc., 400 CoˆteVertu Road West, Dorval, Que ́bec H4S 1Y9, 

Canada; telephone 514–855–5000; fax 514– 

855–7401; e-mail 

thd.qseries@aero.bombardier.com; Internet 

http://www.bombardier.com. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue, SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at NARA, call 202–741–6030, or go 

to: http://www.archives.gov/federal_register/

code_of_federal_regulations/ibr_

locations.html. 

Issued in Renton, Washington, on April 27, 

2010. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–10472 Filed 5–4–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF ENERGY 

Federal Energy Regulatory 

Commission 

18 CFR Parts 1b and 157 

[Docket No. RM10–21–000; Order No. 734] 

Transferring Certain Enforcement 

Hotline Matters to the Dispute 

Resolution Service: Correction 

AGENCY: Federal Energy Regulatory 

Commission. 

ACTION: Final Rule: correction. 

SUMMARY: The Federal Energy 

Regulatory Commission is correcting a 

final rule that appeared in the Federal 

Register of April 26, 2010, 75 FR 21503. 

The document transferred certain 

enforcement hotline matters to the 

Commission’s Dispute Resolution 

Service. This document corrects various 

Part references on the first page of the 

rule and in the amendatory language. 

DATES: Effective May 1, 2010. 

FOR FURTHER INFORMATION CONTACT: 

Stuart Fischer, Office of Enforcement, 

Federal Energy Regulatory Commission, 

888 First Street, NE., Washington, DC 

20426, (202) 502–8517. 

Nils Nichols, Office of Administrative 

Litigation/Dispute Resolution Service, 

Federal Energy Regulatory Commission, 

888 First Street, NE., Washington, DC 

20426, (202) 502–8638. 

SUPPLEMENTARY INFORMATION: In FR 

Document 2010–9125, published April 

26, 2010 (75 FR 21403), make the 

following corrections: 

1. On page 21503, column 2, the part 

heading is corrected to read: ‘‘18 CFR 

Parts 1b and 157’’. 

2. On page 21505, column 2, the 

words of issuance are corrected to read 

as follows: 

‘‘In consideration of the foregoing, the 

Commission amends parts 1b and 157, 

Chapter 1, Title 18, Code of Federal 

Regulations, to read as follows:’’ 

3. On page 21505, column 3, 

amendatory instruction 1 is corrected to 

read as follows: 

‘‘1. The authority citation for part 157 

continues to read as follows:’’ 

Nathaniel J. Davis, Sr., 

Deputy Secretary. 

[FR Doc. 2010–10453 Filed 5–4–10; 8:45 am] 

BILLING CODE 6717–01–P 

DEPARTMENT OF HOMELAND 

SECURITY 

U.S. Customs and Border Protection 

19 CFR Part 101 

[CBP Dec. 10—05; USCBP–2009–0035] 

RIN 1651–AA79 

Further Consolidation of CBP 

Drawback Centers 

AGENCY: Customs and Border Protection, 

DHS. 

ACTION: Final rule. 

SUMMARY: This document adopts as a 

final rule the proposal to amend title 19 

of the Code of Federal Regulations to 

reflect the closure of the Customs and 

Border Protection (‘‘CBP’’) Drawback 

Center located at the Port of Los 

Angeles-Long Beach, California. The 

closure of this Drawback Center is 

necessary because of decreases in claim 


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