Federal Register / Vol. 72, No. 96 / Friday, May 18, 2007 / Rules and Regulations 27953 

Federal Reserve Office 

Number of business days following the banking day funds are 

deposited 

Utica: 

0210, 0280 .................... 3 

Kansas City: 

0865, 2865 .................... 3 

By order of the Board of Governors of the 

Federal Reserve System, acting through the 

Secretary of the Board under delegated 

authority, May 14, 2007. 

Jennifer J. Johnson, 

Secretary of the Board. 

[FR Doc. E7–9558 Filed 5–17–07; 8:45 am] 

BILLING CODE 6210–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2006–26284; Directorate 

Identifier 2006–CE–68–AD; Amendment 39–

15057; AD 2007–10–16] 

RIN 2120–AA64 

Airworthiness Directives; British 

Aerospace Regional Aircraft Jetstream 

Model 3201 Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD results 

from mandatory continuing 

airworthiness information (MCAI) 

issued 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: 

The Airworthiness Limitations Section of 

the Aircraft Maintenance Manual (AMM) 

applicable to the British Aerospace Jetstream 

3200 has been revised. Some lives have been 

amended and new lives introduced. 

Compliance with these requirements is 

necessary to maintain airworthiness. 

We are issuing this AD to require 

actions to correct the unsafe condition 

on these products. 

DATES: This AD becomes effective June 

22, 2007. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

dms.dot.gov or in person at the Docket 

Management Facility, U.S. Department 

of Transportation, 400 Seventh Street, 

SW., Nassif Building, Room PL–401, 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Taylor Martin, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 

Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329–

4138; fax: (816) 329–4090. 

SUPPLEMENTARY INFORMATION: 

Streamlined Issuance of AD 

The FAA is implementing a new 

process for streamlining the issuance of 

ADs related to MCAI. The streamlined 

process will allow us to adopt MCAI 

safety requirements in a more efficient 

manner and will reduce safety risks to 

the public. This process continues to 

follow all FAA AD issuance processes to 

meet legal, economic, Administrative 

Procedure Act, and Federal Register 

requirements. We also continue to meet 

our technical decision-making 

responsibilities to identify and correct 

unsafe conditions on U.S.-certificated 

products. 

This AD references the MCAI and 

related service information that we 

considered in forming the engineering 

basis to correct the unsafe condition. 

The AD contains text copied from the 

MCAI and for this reason might not 

follow our plain language principles. 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on March 13, 2007 (72 FR 

11300). That NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

The Airworthiness Limitations Section of 

the Aircraft Maintenance Manual (AMM) 

applicable to the British Aerospace Jetstream 

3200 has been revised. Some lives have been 

amended and new lives introduced. 

Compliance with these requirements is 

necessary to maintain airworthiness. 

From the effective date of this 

Airworthiness Directive (AD), comply with 

the requirements of BAE Jetstream Series 

3200 Aircraft Maintenance Manual, Chapter 

05–10–05, Airworthiness Limitations 

Description and Operation Section*, 

Revision 14 or later EASA approved revision. 

*Only the structural fatigue tasks are 

mandated by this AD, the following tasks are 

not addressed by this AD: All the tasks 

recorded in Tables 2, 4, 5 and 8. Together 

with the Table No 3—task 27–70–000 Gust 

lock system. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed. 

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 FAA policies. 

Any such differences are highlighted in 

a NOTE within the AD. 

Costs of Compliance 

We estimate that this AD will affect 

20 products of U.S. registry. We also 

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

requirements of this AD (inserting the 

document into the Airworthiness 

Limitations section of the Instructions 

for Continued Airworthiness or other 

FAA-approved maintenance document). 

The average labor rate is $80 per workhour. Based on these figures, we 

estimate the cost of this AD on U.S. 

operators to be $1,600, or $80 per 

product. 

We have no way of determining the 

costs associated with having to replace 

certain parts at an earlier time due to 

reduced life limits. 

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. 


cprice-sewell on PRODPC61 with RULES
27954 Federal Register / Vol. 72, No. 96 / Friday, May 18, 2007 / Rules and Regulations 

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 

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://dms.dot.gov; or in 

person at the Docket Management 

Facility 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 Office (telephone (800) 647–

5227) 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, 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 adding 

the following new AD: 

2007–10–16 British Aerospace Regional 

Aircraft Jetstream: Amendment 39–

15057; Docket No. FAA–2006–26284; 

Directorate Identifier 2006–CE–68–AD. 

Effective Date 

(a) This airworthiness directive (AD) 

becomes effective June 22, 2007. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to Jetstream Model 

3201 airplanes, all serial numbers, 

certificated in any category. 

Subject 

(d) Air Transport Association of America 

(ATA) Code 55: Structures. 

Reason 

(e) The mandatory continuing 

airworthiness information (MCAI) states: 

The Airworthiness Limitations Section of 

the Aircraft Maintenance Manual (AMM) 

applicable to the British Aerospace Jetstream 

3200 has been revised. Some lives have been 

amended and new lives introduced. 

Compliance with these requirements is 

necessary to maintain airworthiness. 

From the effective date of this 

Airworthiness Directive (AD), comply with 

the requirements of BAE Jetstream Series 

3200 Aircraft Maintenance Manual, Chapter 

05–10–05, Airworthiness Limitations 

Description and Operation Section*, 

Revision 14 or later EASA approved revision. 

*Only the structural fatigue tasks are 

mandated by this AD, the following tasks are 

not addressed by this AD: All the tasks 

recorded in Tables 2, 4, 5 and 8. Together 

with the Table No 3—task 27–70–000 Gust 

lock system. 

Actions and Compliance 

(f) Within the next 60 days after June 22, 

2007 (the effective date of this AD) do the 

following, unless already done: 

(1) Incorporate the information referenced 

below from Aircraft Maintenance Manual 05–

10–05 001—AIRWORTHINESS 

LIMITATIONS—DESCRIPTION AND 

OPERATION—BAe Jetstream 32, dated 

January 11, 2006, for Recurring Mandatory 

Inspections and Maintenance Actions into 

the Airworthiness Limitations section of the 

Instructions for Continued Airworthiness or 

other FAA-approved maintenance document. 

You may use a later European Aviation 

Safety Agency (EASA)-approved revision that 

incorporates these same life limits. 

Table number in document Affected areas AD applies 

(i) Table No. 1 ........................................................................... Wing, Fuselage, Fin, Tailplane, Engine mounting, Flap system.Yes. 

(ii) Table No. 2 ........................................................................... Electrical Power (all Items) ....................................................... No. 

(iii) Table No. 3 .......................................................................... Rudder pedal/brake master cylinder attachment brackets ...... Yes. 

(iv) Table No. 3 .......................................................................... Gust lock system ...................................................................... No. 

(v) Table No. 4 and Table No. 5 ............................................... Ice and rain protection (all items) ............................................. No. 

(vi) Table No. 6 and Table No. 7 .............................................. Landing gear (all items) ............................................................ Yes. 

(vii) Table No. 8 ......................................................................... Lighting (all items) .................................................................... No. 

(viii) Table No. 9 ........................................................................ Doors (all items) ....................................................................... Yes. 

(ix) Table No. 10 ........................................................................ Fuselage (all items) .................................................................. Yes. 

(x) Table No. 11 ........................................................................ Stabilizers (all items) ................................................................ Yes. 

(xi) Table No. 12 ........................................................................ Wings (all items) ....................................................................... Yes. 

(2) The owner/operator holding at least a 

private pilot certificate as authorized by 

section 43.7 of the Federal Aviation 

Regulations (14 CFR 43.7) may do the actions 

of this AD. Make an entry into the aircraft 

records showing compliance with this AD in 

accordance with section 43.9 of the Federal 

Aviation Regulations (14 CFR 43.9). 

FAA AD Differences 

Note: This AD differs from the MCAI and/ 

or service information as follows: 

(1) The MCAI requires you to comply with 

a version of a maintenance manual that 

changes life limits. The FAA requires such 

changes through a change to the 

Airworthiness Limitations section of the 

Instructions for Continued Airworthiness or 

other FAA-approved maintenance document, 

and the FAA is mandating this through this 

AD. 

(2) We added information in paragraph (f) 

that allows the owner/operator to insert this 

information into the Airworthiness 

Limitations section of the Instructions for 

Continued Airworthiness or other FAAapproved maintenance document. Without 

this information, a licensed mechanic would 

be required to do the action. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Staff, 

FAA, Small Airplane Directorate, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 

CFR 39.19. Send information to ATTN: 

Taylor Martin, Aerospace Engineer, FAA, 

Small Airplane Directorate, 901 Locust, 


cprice-sewell on PRODPC61 with RULES
Federal Register / Vol. 72, No. 96 / Friday, May 18, 2007 / Rules and Regulations 27955 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4138; fax: (816) 329–

4090. Before using any approved AMOC on 

any airplane to which the AMOC applies, 

notify your appropriate principal inspector 

(PI) in the FAA Flight Standards District 

Office (FSDO), or lacking a PI, your local 

FSDO. 

(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 

(h) Refer to MCAI Civil Aviation Authority 

AD No. G–2004–0024, Issue Date: September 

22, 2004, EASA approved on September 16, 

2004, under approval number 2004–9648, for 

related information. 

Issued in Kansas City, Missouri, on May 9, 

2007. 

Charles L. Smalley, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 07–2472 Filed 5–17–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Part 510 

New Animal Drugs; Change of 

Sponsor’s Address 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule. 

SUMMARY: The Food and Drug 

Administration (FDA) is amending the 

animal drug regulations to reflect a 

change of sponsor’s address for Modern 

Veterinary Therapeutics, LLC. 

DATES: This rule is effective May 18, 

2007. 

FOR FURTHER INFORMATION CONTACT: 

David R. Newkirk, Center for Veterinary 

Medicine (HFV–100), Food and Drug 

Administration, 7500 Standish Pl., 

Rockville, MD 20855, 301–827–6967, email: david.newkirk@fda.hhs.gov. 

SUPPLEMENTARY INFORMATION: Modern 

Veterinary Therapeutics, LLC, 18301 

SW. 86th Ave., Miami, FL 33157, has 

informed FDA of a change of address to 

1550 Madruga Ave., suite 329, Coral 

Gables, FL 33146. Accordingly, the 

agency is amending the regulations in 

21 CFR 510.600(c) to reflect the change. 

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 510 

Administrative practice and 

procedure, Animal drugs, Labeling, 

Reporting and recordkeeping 

requirements. 

■ 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 510 is amended as follows: 

PART 510—NEW ANIMAL DRUGS 

■ 1. The authority citation for 21 CFR 

part 510 continues to read as follows: 

Authority: 21 U.S.C. 321, 331, 351, 352, 

353, 360b, 371, 379e. 

■ 2. In § 510.600, in the table in 

paragraph (c)(1) revise the entry for 

‘‘Modern Veterinary Therapeutics, 

LLC’’; and in the table in paragraph 

(c)(2) revise the entry for ‘‘015914’’ to 

read as follows: 

§ 510.600 Names, addresses, and drug 

labeler codes of sponsors of approved 

applications. 

* * * * * 

(c) * * * 

(1) * * * 

Firm name and address Drug labeler 

code 

* * * * * 

Modern Veterinary Therapeutics, LLC, 1550 

Madruga Ave., suite 329, 

Coral Gables, FL 33146 015914 

* * * * * 

(2) * * * 

Drug labeler 

code Firm name and address 

* * * * * 

015914 Modern Veterinary Therapeutics, LLC, 1550 

Madruga Ave., suite 329, 

Coral Gables, FL 33146 

* * * * * 

Dated: May 7, 2007. 

Bernadette Dunham, 

Deputy Director, Center for Veterinary 

Medicine. 

[FR Doc. E7–9555 Filed 5–17–07; 8:45 am] 

BILLING CODE 4160–01–S 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Parts 510 and 520 

Oral Dosage Form New Animal Drugs; 

Phenylbutazone Powder 

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 abbreviated new animal 

drug application (ANADA) filed by 

Superior Equine Pharmaceuticals, Inc. 

The ANADA provides for the veterinary 

prescription use of phenylbutazone 

powder administered to horses in feed 

for the relief of inflammatory conditions 

associated with the musculoskeletal 

system. 

DATES: This rule is effective May 18, 

2007. 

FOR FURTHER INFORMATION CONTACT: John 

K. Harshman, Center for Veterinary 

Medicine (HFV–104), Food and Drug 

Administration, 7500 Standish Pl., 

Rockville, MD 20855, 301–827–0169, email: john.harshman@fda.hhs.gov. 

SUPPLEMENTARY INFORMATION: Superior 

Equine Pharmaceuticals, Inc., Pleasant 

Grove, UT 84062, filed ANADA 200–

333 that provides for the veterinary 

prescription use of SUPERIORBUTE 

(phenylbutazone) Powder administered 

to horses in feed for the relief of 

inflammatory conditions associated 

with the musculoskeletal system. 

Superior Equine Pharmaceuticals, Inc.’s 

SUPERIORBUTE Powder is approved as 

a generic copy of IVX Animal Health, 

Inc.’s Phenylbutazone Tablets, USP, 

approved under NADA 91–818. The 

ANADA is approved as of April 20, 

2007, and the regulations are amended 

in 21 CFR 520.1720e to reflect the 

approval. The basis of approval is 

discussed in the freedom of information 

summary. 

In addition, Superior Equine 

Pharmaceuticals, Inc., has not been 

previously listed in the animal drug 

regulations as a sponsor of an approved 

application. At this time, 21 CFR 

510.600(c) is being amended to add 

entries for the firm. 


cprice-sewell on PRODPC61 with RULES