Federal Register / Vol. 75, No. 82 / Thursday, April 29, 2010 / Rules and Regulations 22521 

Subject 

(d) Air Transport Association (ATA) of 

America Code 34: Navigation. 

Unsafe Condition 

(e) This AD results from discovery of 

software anomalies which, in certain 

situations, can cause the FMS to generate 

misleading navigational guidance to the 

pilots and to the autopilot system of various 

airplanes having this same system software. 

The Federal Aviation Administration is 

issuing this AD to provide the flightcrew 

with procedures to recover from or work 

around these software anomalies during 

flight, which could lead to an airplane 

departing from its scheduled flight path, and 

result in possible collision with other aircraft 

or terrain. 

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. 

Revise the Airplane Flight Manual (AFM) 

(g) Within 14 days after the effective date 

of this AD, revise the Limitations section of 

the applicable AFM to include the 

information in the applicable service 

information letter (SIL) specified in Table 2 

of this AD. 

TABLE 2—SERVICE INFORMATION

Honeywell Service Information Letter— Revision— Model— Dated— 

D201002000007 .................................... Original ............. PC–12/47E airplanes ........................................................... February 16, 2010. 

D201002000051 .................................... 1 ....................... ERJ 170 and ERJ 190 airplanes ......................................... March 26, 2010. 

D201002000052 .................................... Original ............. ERJ 170 and ERJ 190 airplanes ......................................... March 3, 2010. 

Note 1: The actions required by paragraph 

(g) of this AD may be done by inserting a 

copy of the applicable SIL specified in Table 

2 of this AD into the applicable AFM. When 

the applicable SIL has been included in the 

general revisions of the applicable AFM, the 

general revisions may be inserted into the 

AFM, provided the relevant information in 

the general revision is identical to that in the 

SIL. 

Alternative Methods of Compliance 

(AMOCs) 

(h) The manager of the office having 

certificate responsibility for the affected 

airplanes has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. Before 

using any approved AMOC on any aircraft 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. 

(1) For transport airplanes: Send 

information to ATTN: Chip Adam, Flight 

Test Pilot, Flight Test Branch, ANM–160L, 

FAA, Los Angeles Aircraft Certification 

Office, 3960 Paramount Boulevard, 

Lakewood, California 90712–4137; telephone 

(562) 627–5369; fax (562) 627–5210. 

(2) For small airplanes: Send information 

to ATTN: Doug Rudolph, Aerospace 

Engineer, Small Airplane Directorate, FAA, 

901 Locust Street, Room 301, Kansas City, 

Missouri 64106; telephone (816) 329–4059; 

fax (816) 329–4090. 

Material Incorporated by Reference 

(i) You must use the applicable service 

information contained in Table 3 of this AD 

to do the actions required by this AD, unless 

the AD specifies otherwise. 

TABLE 3—MATERIAL INCORPORATED BY REFERENCE

Document Revision Date 

Honeywell Service Information Letter D201002000007 ........................................................................... Original ............. February 16, 2010. 

Honeywell Service Information Letter D201002000051 ........................................................................... 1 ....................... March 26, 2010. 

Honeywell Service Information Letter D201002000052 ........................................................................... Original ............. March 3, 2010. 

(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 Honeywell Technical 

Operations Center, 1944 E. Sky Harbor Circle, 

Phoenix, Arizona 85034; telephone 602–365– 

3099 or 800–601–3099; fax 602–365–3343; email AeroTechSupport@Honeywell.com; 

Internet http://portal.honeywell.com/wps/ 

portal/aero. 

(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 8, 

2010. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–9090 Filed 4–28–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0525; Directorate 

Identifier 2009–NM–027–AD; Amendment 

39–16275; AD 2010–09–10] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc. Model CL–600–2B19 (Regional Jet 

Series 100 & 440) Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) for 

the products listed above. This AD 

results from mandatory continuing 

airworthiness information (MCAI) 

originated by an aviation authority of 

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22522 Federal Register / Vol. 75, No. 82 / Thursday, April 29, 2010 / Rules and Regulations 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as: 

AD CF–2002–12 [which corresponds to 

FAA AD 2003–04–21, amendment 39–13070] 

mandated installation of revised overwing 

emergency exit placards showing that the 

exit door should be opened and disposed 

from a seated position. However, it was later 

discovered that the new placards illustrated 

an incorrect hand position for removal of the 

exit upper handle cover. These incorrect 

instructions could cause difficulty or delay 

when opening the overwing emergency exit. 

As a result, the timely and safe 

evacuation of passengers and crew may 

be impeded. We are issuing this AD to 

require actions to correct the unsafe 

condition on these products. 

DATES: This AD becomes effective June 

3, 2010. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of June 3, 2010. 

On April 4, 2003 (68 FR 9509, 

February 28, 2003), the Director of the 

Federal Register approved the 

incorporation by reference of a certain 

other publication listed in this AD. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue, SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Christopher Alfano, Aerospace 

Engineer, Airframe and Mechanical 

Systems Branch, ANE–171, FAA, New 

York Aircraft Certification Office, 1600 

Stewart Avenue, Suite 410, Westbury, 

New York 11590; telephone (516) 228– 

7340; fax (516) 794–5531. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a supplemental notice of 

proposed rulemaking (NPRM) to amend 

14 CFR part 39 to include an AD that 

would apply to the specified products. 

That supplemental NPRM was 

published in the Federal Register on 

December 23, 2009 (74 FR 68198), and 

proposed to supersede AD 2003–04–21, 

Amendment 39–13070 (68 FR 9509, 

February 28, 2003). That supplemental 

NPRM proposed to correct an unsafe 

condition for the specified products. 

The MCAI states: 

AD CF–2002–12 [which corresponds to 

FAA AD 2003–04–21] mandated installation 

of revised overwing emergency exit placards 

showing that the exit door should be opened 

and disposed from a seated position. 

However, it was later discovered that the new 

placards illustrated an incorrect hand 

position for removal of the exit upper handle 

cover. These incorrect instructions could 

cause difficulty or delay when opening the 

overwing emergency exit. 

As a result, the timely and safe 

evacuation of passengers and crew may 

be impeded. The required actions 

include replacing the incorrect placards 

with revised placards. You may obtain 

further information by examining the 

MCAI in the AD docket. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

considered the comment received from 

the only commenter. 

Request To Refer to Updated Service 

Information 

Air Wisconsin requests that we 

update the supplemental NPRM to refer 

to the most recent service information. 

Air Wisconsin notes that Bombardier 

Service Bulletin 601R–11–088, Revision 

A, dated March 24, 2009, has been 

revised. Bombardier has issued Service 

Bulletin 601R–11–088, Revision B, 

dated November 17, 2009. 

We agree to refer to the latest service 

information. We have determined that 

the actions specified in the revised 

service bulletin are essentially identical 

to the actions specified in Bombardier 

Service Bulletin 601R–11–088, Revision 

A, dated March 24, 2009. We have 

revised paragraphs (h) and (k) of this AD 

to refer to Bombardier Service Bulletin 

601R–11–088, Revision B, dated 

November 17, 2009. We have revised 

paragraph (i) of this AD to also give 

credit for actions done in accordance 

with Bombardier Service Bulletin 601R– 

11–088, Revision A, dated March 24, 

2009. 

Explanation of Change Made to This 

AD 

We have revised this AD to identify 

the legal name of the manufacturer as 

published in the most recent type 

certificate data sheet for the affected 

airplane models. 

Conclusion 

We reviewed the relevant data, 

considered the comment received, and 

determined that air safety and the 

public interest require adopting the AD 

with the changes described previously. 

We also determined that these changes 

will not increase the economic burden 

on any operator or increase the scope of 

the AD. 

Differences Between This 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 our FAA 

policies. Any such differences are 

highlighted in a Note within the AD. 

Explanation of Change to Costs of 

Compliance 

After the supplemental NPRM was 

issued, we reviewed the figures we have 

used over the past several years to 

calculate AD costs to operators. To 

account for various inflationary costs in 

the airline industry, we find it necessary 

to increase the labor rate used in these 

calculations from $80 per work hour to 

$85 per work hour. The cost impact 

information, below, reflects this 

increase in the specified hourly labor 

rate. 

Costs of Compliance 

We estimate that this AD will affect 

664 products of U.S. registry. We also 

estimate that it will take about 1 workhour per product to comply with the 

basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts will cost about $128 per 

product. Where the service information 

lists required parts costs that are 

covered under warranty, we have 

assumed that there will be no charge for 

these parts. As we do not control 

warranty coverage for affected parties, 

some parties may incur costs higher 

than estimated here. Based on these 

figures, we estimate the cost of this AD 

to the U.S. operators to be $141,432, or 

$213 per product. 

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 

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Federal Register / Vol. 75, No. 82 / Thursday, April 29, 2010 / Rules and Regulations 22523 

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. 

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 the NPRM, 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. 

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: 

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 

removing Amendment 39–13070 (68 FR 

9509, February 28, 2003) corrected at 68 

FR 14309, March 25, 2003, and adding 

the following new AD: 

2010–09–10 Bombardier, Inc.: Amendment 

39–16275. Docket No. FAA–2009–0525; 

Directorate Identifier 2009–NM–027–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective June 3, 2010. 

Affected ADs 

(b) This AD supersedes AD 2003–04–21 

R1, Amendment 39–13070. 

Applicability 

(c) This AD applies to Bombardier, Inc. 

Model CL–600–2B19 (Regional Jet Series 100 

& 440) airplanes, certificated in any category, 

serial numbers 7003 and subsequent. 

Subject 

(d) Air Transport Association (ATA) of 

America Code 11: Placards and markings. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

AD CF–2002–12 [which corresponds to 

FAA AD 2003–04–21, amendment 39–13070] 

mandated installation of revised overwing 

emergency exit placards showing that the 

exit door should be opened and disposed 

from a seated position. However, it was later 

discovered that the new placards illustrated 

an incorrect hand position for removal of the 

exit upper handle cover. These incorrect 

instructions could cause difficulty or delay 

when opening the overwing emergency exit. 

As a result, the timely and safe evacuation of 

passengers and crew may be impeded. The 

required action includes replacing the 

incorrect placards with revised placards. 

Restatement of Certain Requirements of AD 

2003–04–21 R1 

(f) Unless already done, for airplanes 

identified in Table 1 of this AD, within 12 

months after April 4, 2003 (the effective date 

of AD 2003–04–21 R1), replace the door 

weight placards, and no-baggage placards 

with new placards (including cleaning of the 

applicable surface), as applicable, per 

Bombardier Alert Service Bulletin A601R– 

11–077, Revision A, dated December 11, 

2001, excluding Service Bulletin Comment 

Sheet—Facsimile Reply Sheet and CRJ 100/ 

200 Service Bulletin Compliance Facsimile 

Reply Sheet. 

TABLE 1—SERIAL NOS. 

Serial Nos. 

7003 through 7434 inclusive. 

7436 through 7442 inclusive. 

7444 through 7452 inclusive. 

7454 through 7458 inclusive. 

7460 through 7497 inclusive. 

7499 through 7504 inclusive. 

(g) Replacement accomplished before April 

4, 2003, per Bombardier Alert Service 

Bulletin A601R–11–077, dated July 12, 2001, 

is considered acceptable for compliance with 

the replacement specified in paragraph (f) of 

this AD. 

New Requirements of This AD 

Actions and Compliance 

(h) Unless already done, within 24 months 

after the effective date of this AD, replace the 

existing overwing emergency exit placards 

with new placards in accordance with the 

Accomplishment Instructions of Bombardier 

Service Bulletin 601R–11–088, Revision B, 

dated November 17, 2009. 

(i) Replacing the overwing emergency exit 

placards with new placards before the 

effective date of this AD in accordance with 

Bombardier Service Bulletin 601R–11–088, 

dated June 25, 2008; or Revision A, dated 

March 24, 2009; is considered acceptable for 

compliance with the corresponding action 

specified in this AD. 

FAA AD Differences 

Note 1: This AD differs from the MCAI 

and/or service information as follows: The 

MCAI applicability includes certain 

airplanes. This AD expands the applicability 

to include serial numbers 7003 and 

subsequent. 

Other FAA AD Provisions 

(j) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, New York Aircraft 

Certification Office, 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: Program 

Manager, ANE–170, 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. AMOCs 

approved previously in accordance with AD 

2003–04–21, Amendment 39–13070, are 

approved as AMOCs for the corresponding 

provisions of 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. 

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22524 Federal Register / Vol. 75, No. 82 / Thursday, April 29, 2010 / Rules and Regulations 

Related Information 

(k) Refer to MCAI Canadian Airworthiness 

Directive CF–2009–02, dated January 19, 

2009; Bombardier Alert Service Bulletin 

A601R–11–077, Revision A, dated December 

11, 2001; and Bombardier Service Bulletin 

601R–11–088, Revision B, dated November 

17, 2009; for related information. 

Material Incorporated by Reference 

(l) You must use Bombardier Service 

Bulletin 601R–11–088, Revision B, dated 

November 17, 2009; and Bombardier Alert 

Service Bulletin A601R–11–077, Revision A, 

dated December 11, 2001, excluding Service 

Bulletin Comment Sheet—Facsimile Reply 

Sheet and CRJ 100/200 Service Bulletin 

Facsimile Reply Sheet; as applicable; to do 

the actions required by this AD, unless the 

AD specifies otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

Bombardier Service Bulletin A601R–11–088, 

Revision B, dated November 17, 2009, under 

5 U.S.C. 552(a) and 1 CFR part 51. 

(2) The Director of the Federal Register 

previously approved the incorporation by 

reference of Bombardier Alert Service 

Bulletin A601R–11–077, Revision A, dated 

December 11, 2001, excluding Service 

Bulletin Comment Sheet—Facsimile Reply 

Sheet and CRJ 100/200 Service Bulletin 

Compliance Facsimile Reply Sheet, on April 

4, 2003 (68 FR 9509, February 28, 2003). 

(3) For service information identified in 

this AD, contact Bombardier, Inc., 400 Coˆte 

Vertu Road West, Dorval, Que ́bec H4S 1Y9, 

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

855–7401; e-mail 

thd.crj@aero.bombardier.com; Internet http:// 

www.bombardier.com. 

(4) 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 or 425–227–1152. 

(5) 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 16, 

2010. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2010–9594 Filed 4–28–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 522 

[Docket No. FDA–2010–N–0002] 

Implantation or Injectable Dosage 

Form New Animal Drugs; Butorphanol 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule. 

SUMMARY: The Food and Drug 

Administration (FDA) is amending the 

animal drug regulations to reflect 

approval of an original abbreviated new 

animal drug application (ANADA) filed 

by Modern Veterinary Therapeutics, 

LLC. The ANADA provides for use of an 

injectable solution of butorphanol 

tartrate in cats for the relief of pain. 

DATES: This rule is effective April 29, 

2010. 

FOR FURTHER INFORMATION CONTACT: John 

K. Harshman, Center for Veterinary 

Medicine (HFV–170), Food and Drug 

Administration, 7500 Standish Pl., 

Rockville, MD 20855, 240–276–8197, email: john.harshman@fda.hhs.gov. 

SUPPLEMENTARY INFORMATION: Modern 

Veterinary Therapeutics, LLC, 1550 

Madruga Ave., suite 329, Coral Gables, 

FL 33146, filed ANADA 200–446 for the 

use of BUTORPHINE (butorphanol 

tartrate, USP) Veterinary Injection in 

cats for the relief of pain. Modern 

Veterinary Therapeutics’ BUTORPHINE 

Veterinary Injection is approved as a 

generic copy of TORBUGESIC–SA 

(butorphanol tartrate, USP) Veterinary 

Injection, approved under NADA 141– 

047 held by Fort Dodge Animal Health, 

Division of Wyeth, a wholly owned 

subsidiary of Pfizer, Inc. The ANADA is 

approved as of March 26, 2010, and the 

regulations in 21 CFR 522.246 are 

amended to reflect the approval. 

In accordance with the freedom of 

information provisions of 21 CFR part 

20 and 21 CFR 514.11(e)(2)(ii), a 

summary of safety and effectiveness 

data and information submitted to 

support approval of this application 

may be seen in the Division of Dockets 

Management (HFA–305), Food and Drug 

Administration, 5630 Fishers Lane, rm. 

1061, Rockville, MD 20852, between 9 

a.m. and 4 p.m., Monday through 

Friday. 

FDA has determined under 21 CFR 

25.33 that this action is of a type that 

does not individually or cumulatively 

have a significant effect on the human 

environment. Therefore, neither an 

environmental assessment nor an 

environmental impact statement is 

required. 

This rule does not meet the definition 

of ‘‘rule’’ in 5 U.S.C. 804(3)(A) because 

it is a rule of ‘‘particular applicability.’’ 

Therefore, it is not subject to the 

congressional review requirements in 5 

U.S.C. 801–808. 

List of Subjects in 21 CFR Part 522 

Animal drugs. 

■ Therefore, under the Federal Food, 

Drug, and Cosmetic Act and under 

authority delegated to the Commissioner 

of Food and Drugs and redelegated to 

the Center for Veterinary Medicine, 21 

CFR part 522 is amended as follows: 

PART 522—IMPLANTATION OR 

INJECTABLE DOSAGE FORM NEW 

ANIMAL DRUGS 

■ 1. The authority citation for 21 CFR 

part 522 continues to read as follows: 

Authority: 21 U.S.C. 360b. 

§ 522.246 [Amended] 

■ 2. In paragraph (b)(2) of § 522.246, 

remove ‘‘No. 059130’’ and in its place 

add ‘‘Nos. 015914 and 059130’’. 

Dated: April 23, 2010. 

William T. Flynn, 

Acting Director, Center for Veterinary 

Medicine. 

[FR Doc. 2010–9871 Filed 4–28–10; 8:45 am] 

BILLING CODE 4160–01–S 

ENVIRONMENTAL PROTECTION 

AGENCY 

40 CFR Part 228 

[EPA–R10–OW–2010–0086; FRL–9143–2] 

Ocean Dumping; Designation of Ocean 

Dredged Material Disposal Sites 

Offshore of the Siuslaw River, Oregon 

AGENCY: Environmental Protection 

Agency (EPA). 

ACTION: Final rule. 

SUMMARY: This action finalizes the 

designation of the Siuslaw River ocean 

dredged material disposal sites pursuant 

to the Marine Protection, Research and 

Sanctuaries Act, as amended (MPRSA). 

The new sites are needed primarily to 

serve the long-term need for a location 

to dispose of material dredged from the 

Siuslaw River navigation channel, and 

to provide a location for the disposal of 

dredged material for persons who have 

received a permit for such disposal. The 

newly designated sites will be subject to 

ongoing monitoring and management to 

ensure continued protection of the 

marine environment. 

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