28172 Federal Register / Vol. 80, No. 95 / Monday, May 18, 2015 / Rules and Regulations 

preempted; (2) no retroactive effect will 

be given to this rule; and (3) no 

administrative proceedings will be 

required before parties may file suit in 

court challenging this rule. 

E-Government Act 

FSIS and USDA are committed to 

achieving the purposes of the EGovernment Act (44 U.S.C. 3601, et 

seq.) by, among other things, promoting 

the use of the Internet and other 

information technologies and providing 

increased opportunities for citizen 

access to Government information and 

services, and for other purposes. 

USDA Nondiscrimination Statement 

No agency, officer, or employee of the 

USDA shall, on the grounds of race, 

color, national origin, religion, sex, 

gender identity, sexual orientation, 

disability, age, marital status, family/

parental status, income derived from a 

public assistance program, or political 

beliefs, exclude from participation in, 

deny the benefits of, or subject to 

discrimination any person in the United 

States under any program or activity 

conducted by the USDA. 

To file a complaint of discrimination, 

complete the USDA Program 

Discrimination Complaint Form, which 

may be accessed online at http://

www.ocio.usda.gov/sites/default/files/

docs/2012/Complain_combined_6_8_

12.pdf, or write a letter signed by you 

or your authorized representative. 

Send your completed complaint form 

or letter to USDA by mail, fax, or email: 

Mail: U.S. Department of Agriculture, 

Director, Office of Adjudication, 1400 

Independence Avenue SW., 

Washington, DC 20250–9410. 

Fax: (202)690–7442/ 

Email: program.intake@usda.gov 

Persons with disabilities who require 

alternative means for communication 

(Braille, large print, audiotape, etc.) 

should contact USDA’s TARGET Center 

at (202) 720–2600 (voice and TDD). 

Additional Public Notification 

Public awareness of all segments of 

rulemaking and policy development is 

important. Consequently, FSIS will 

announce it on-line through the FSIS 

Web page located at: http://

www.fsis.usda.gov/federal-register. 

FSIS also will make copies of this 

Federal Register publication available 

through the FSIS Constituent Update, 

which is used to provide information 

regarding FSIS policies, procedures, 

regulations, Federal Register notices, 

FSIS public meetings, and other types of 

information that could affect or would 

be of interest to our constituents and 

stakeholders. The Update is available on 

the FSIS Web page. Through the Web 

page, FSIS is able to provide 

information to a much broader, more 

diverse audience. In addition, FSIS 

offers an email subscription service 

which provides automatic and 

customized access to selected food 

safety news and information. This 

service is available at: http://

www.fsis.usda.gov/subscribe. Options 

range from recalls to export information, 

regulations, directives, and notices. 

Customers can add or delete 

subscriptions themselves, and have the 

option to password-protect their 

accounts. 

List of Subjects in 9 CFR Part 317 

Food labeling, Food packaging, Meat 

inspection, Nutrition, Reporting and 

recordkeeping requirements. 

For the reasons discussed in the 

preamble, FSIS amends 9 CFR Chapter 

III as follows: 

PART 317—LABELING, MARKING 

DEVICES, AND CONTAINERS 

■ 1. The authority citation for part 317 

continues to read as follows: 

Authority: 21 U.S.C. 601–695; 7 CFR 2.18, 

2.53. 

■ 2. Amend § 317.2 by adding a new 

paragraph (e)(3) to read as follows: 

§ 317.2 Labels: definition; required 

features. 

* * * * * 

(e) * * * 

(3) Product name and required 

validated cooking instructions for 

needle- or blade-tenderized beef 

products. 

(i) Unless the product is destined to 

be fully cooked or to receive another full 

lethality treatment at an official 

establishment, the product name for a 

raw or partially cooked beef product 

that has been mechanically tenderized, 

whether by needle or by blade, must 

contain the term ‘‘mechanically 

tenderized,’’ ‘‘needle tenderized,’’ or 

‘‘blade tenderized,’’ as a descriptive 

designation and an accurate description 

of the beef component. 

(ii) The product name must appear in 

a single easy-to-read type style and color 

and on a single-color contrasting 

background. The print may appear in 

upper and lower case letters, with the 

lower case letters not smaller than 1⁄3

the size of the largest letter. 

(iii) The labels on raw or partially 

cooked needle- or blade-tenderized beef 

products destined for household 

consumers, hotels, restaurants, or 

similar institutions must contain 

validated cooking instructions, 

including the cooking method, that 

inform consumers that these products 

need to be cooked to a specified 

minimum internal temperature, whether 

the product needs to be held for a 

specified time at that temperature or 

higher before consumption to ensure 

that potential pathogens are destroyed 

throughout the product, and a statement 

that the internal temperature should be 

measured by a thermometer. These 

validated cooking instructions may 

appear anywhere on the label. 

* * * * * 

Done, at Washington, DC, on May 13, 2015. 

Alfred V. Almanza, 

Acting Administrator. 

[FR Doc. 2015–11916 Filed 5–15–15; 8:45 am] 

BILLING CODE 3410–DM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–1537; Directorate 

Identifier 2015–SW–014–AD; Amendment 

39–18160; AD 2015–08–51] 

RIN 2120–AA64 

Airworthiness Directives; The Enstrom 

Helicopter Corporation 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are publishing a new 

airworthiness directive (AD) for 

Enstrom Helicopter Corporation 

(Enstrom) Model F–28A, 280, F–28C, F– 

28C–2, F–28C–2R, 280C, F–28F, F–28F– 

R, 280F, 280FX, and 480 helicopters. 

This AD was sent previously to all 

known U.S. owners and operators of 

these helicopters and supersedes 

Emergency AD (EAD) 2015–04–51, 

dated February 12, 2015. This AD 

requires inspecting certain main rotor 

spindles (spindles) for cracks and 

reporting the inspection results to the 

FAA. This AD is prompted by a fatal 

accident and reports of spindles with 

cracks. The actions specified in this AD 

are intended to detect a crack in a 

spindle and prevent loss of a main rotor 

blade and subsequent loss of control of 

the helicopter. 

DATES: This AD becomes effective June 

2, 2015 to all persons except those 

persons to whom it was made 

immediately effective by EAD 2015–08– 

51, issued on April 10, 2015, which 

contains the requirements of this AD. 

We must receive comments on this 

AD by July 17, 2015. 


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Federal Register / Vol. 80, No. 95 / Monday, May 18, 2015 / Rules and Regulations 28173 

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 AD, the economic 

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 service information identified in 

this AD, contact Enstrom Helicopter 

Corporation, 2209 22nd Street, 

Menominee, MI; telephone (906) 863– 

1200; fax (906) 863–6821; or at 

www.enstromhelicopter.com. You may 

review 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: 

Gregory J. Michalik, Senior Aerospace 

Engineer, Chicago Aircraft Certification 

Office, Small Airplane Directorate, FAA, 

2300 East Devon Ave., Des Plaines, IL 

60018; (847) 294–7135; email 

gregory.michalik@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not provide you with notice and 

an opportunity to provide your 

comments prior to it becoming effective. 

However, 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 resulted from 

adopting this AD. The most helpful 

comments reference a specific portion of 

the AD, 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 them 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 

rulemaking during the comment period. 

We will consider all the comments we 

receive and may conduct additional 

rulemaking based on those comments. 

Discussion 

On February 12, 2015, we issued EAD 

2015–04–51, which was prompted by a 

fatal accident. Preliminary results of the 

investigation indicated that the accident 

was caused by a crack in the spindle, 

which resulted in the main rotor blade 

separating from the helicopter. The 

crack was discovered at the last thread 

of the spindle retention nut threads. 

While the investigation could not 

determine when the crack initiated, it 

was able to determine that the crack 

existed, undetected, for a significant 

amount of time before the separation. 

EAD 2015–04–51 required, before 

further flight, conducting a magnetic 

particle inspection (MPI) in any spindle 

that had 5,000 or more hours time-inservice (TIS) or where the hours TIS of 

the spindle is not known. If there was 

a crack in the spindle, EAD 2015–04–51 

required replacing it before further 

flight. EAD 2015–04–51 also required 

reporting the inspection results to the 

FAA within 72 hours. 

Since we issued EAD 2015–04–51, 

inspection reports received by the FAA 

indicate approximately 20% of the 

spindles reported with TIS data had 

evidence of cracks. The FAA also 

received inspection reports of spindles 

without TIS data which did not have 

evidence of cracks. The inspection 

reports include spindles with cracks at 

less than 5,000 hours TIS. With analysis 

of available data, we determined the 

need to expand the applicability to 

include spindles with 1,500 or more 

hours TIS. 

On April 10, 2015, we issued EAD 

2015–08–51, which supersedes EAD 

2015–04–51. EAD 2015–08–51 retains 

all of the requirements of EAD 2014–04– 

51 except it reduces the TIS of the 

spindles to be inspected from 5,000 

hours to 1,500 hours. EAD 2015–08–51 

was sent previously to all known U.S. 

owners and operators of these 

helicopters. 

FAA’s Determination 

We are issuing this AD because we 

evaluated all the relevant information 

and determined the unsafe condition 

described previously is likely to exist or 

develop in other products of these same 

type designs. 

Related Service Information 

Enstrom has issued Service Directive 

Bulletin No. 0119, Revision 1, dated 

April 1, 2015, for all serial numbered 

Model F–28A, F–28C, F–28F, 280, 280C, 

280F, and 280FX helicopters with a 

main rotor spindle, part number (P/N) 

28–14282–11 and 28–14282–13. 

Enstrom has also issued Service 

Directive Bulletin No. T–050, Revision 

1, dated April 1, 2015, for Model 480 

helicopters, serial numbers 5001 

through 5004 and 5006, and with a main 

rotor spindle, P/N 28–14282–13, except 

those aircraft modified with tensiontorsion straps. Both service directives 

specify, for any spindle that has been in 

service more than 3,500 hours, within 5 

hours TIS, sending the spindle to 

Enstrom for an MPI. For any spindle 

with less than 3,500 hours TIS, the 

service directives specify sending the 

spindle to Enstrom for an MPI at or 

before it reaches 3,500 hours TIS. The 

service directives also specify repeating 

the MPI every 300 hours for spindles 

with over 3,500 hours TIS. 

AD Requirements 

This AD requires conducting an MPI 

before further flight to determine if a 

crack exists in any spindle that has 

1,500 or more hours TIS or where the 

hours TIS of the spindle is not known. 

If there is a crack in the spindle, this AD 

requires replacing it before further 

flight. The MPI of the spindle must be 

conducted by a Level II or Level III 

inspector qualified in the MPI method 

in the Aeronautics Sector according to 

the EN4179 or NAS410 standard or 

equivalent. This AD also requires 

reporting certain information to the 

FAA within 72 hours. 

Differences Between This AD and the 

Service Information 

This AD requires that the MPI be 

conducted by a Level II or Level III 

inspector or equivalent and that the 

results of the MPI be reported to the 

FAA, whereas the service information 

specifies that the MPI be accomplished 

by or reported to Enstrom. This AD 

requires an MPI on spindles with 1,500 

or more hours TIS, whereas the service 

information specifies performing an 

initial MPI on spindles with 3,500 or 

more hours TIS. This AD does not 

require a recurring inspection, whereas 

the service information specifies to 

repeat the MPI every 300 hours TIS for 

spindles with over 3,500 hours TIS. 

This AD requires the MPI before further 


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28174 Federal Register / Vol. 80, No. 95 / Monday, May 18, 2015 / Rules and Regulations 

flight, whereas the service information 

specifies that it be accomplished within 

5 hours TIS. 

Interim Action 

We consider this AD to be an interim 

action. The inspection reports that are 

required by this AD will enable us to 

obtain better insight into the root cause 

and extent of the cracking, and 

eventually to develop final action to 

address the unsafe condition. Once final 

action has been identified, we might 

consider further rulemaking. 

Costs of Compliance 

We estimate that this AD affects 323 

helicopters of U.S. Registry and that 

operators may incur the following costs 

to comply with this AD. Inspecting the 

spindles will take about 15 work-hours 

per helicopter and reporting the 

required inspection information will 

take about 0.5 work-hour. We estimate 

an average labor rate of $85 per workhour, for a total cost of $1,318 per 

helicopter and $425,714 for the U.S. 

fleet. Replacing a spindle will cost 

$8,164 for parts and no additional workhours. 

Paperwork Reduction Act 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject 

to penalty for failure to comply with a 

collection of information subject to the 

requirements of the Paperwork 

Reduction Act unless that collection of 

information displays a current valid 

OMB control number. The control 

number for the collection of information 

required by this AD is 2120–0056. The 

paperwork cost associated with this AD 

has been detailed in the Costs of 

Compliance section of this document 

and includes time for reviewing 

instructions, as well as completing and 

reviewing the collection of information. 

Therefore, all reporting required by this 

AD is mandatory. Comments concerning 

the accuracy of this burden and 

suggestions for reducing the burden 

should be directed to the FAA at 800 

Independence Ave. SW., Washington, 

DC 20591. ATTN: Information 

Collection Clearance Officer, AES–200. 

FAA’s Justification and Determination 

of the Effective Date 

Providing an opportunity for public 

comments prior to adopting these AD 

requirements would delay 

implementing the safety actions needed 

to correct this known unsafe condition. 

Therefore, we found and continue to 

find that the risk to the flying public 

justifies waiving notice and comment 

prior to the adoption of this rule 

because the previously described unsafe 

condition can adversely affect the 

controllability of the helicopter and the 

initial required action must be 

accomplished before further flight. 

Since it was found that immediate 

corrective action was required, notice 

and opportunity for prior public 

comment before issuing this AD were 

impracticable and contrary to the public 

interest and good cause existed to make 

the AD effective immediately by EAD 

2015–08–51, issued on April 10, 2015, 

to all known U.S. owners and operators 

of these helicopters. These conditions 

still exist and the AD is hereby 

published in the Federal Register as an 

amendment to section 39.13 of the 

Federal Aviation Regulations (14 CFR 

39.13) to make it effective to all persons. 

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, I certify 

that 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); 

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 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: 

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): 

2015–08–51 The Enstrom Helicopter 

Corporation (Enstrom): Amendment 39– 

18160; Docket No. FAA–2015–1537; 

Directorate Identifier 2015–SW–014–AD. 

(a) Applicability 

This AD applies to Enstrom Model F–28A, 

280, F–28C, F–28C–2, F–28C–2R, 280C, F– 

28F, F–28F–R, 280F, and 280FX helicopters, 

all serial numbers; and Enstrom Model 480 

helicopters, serial numbers 5001 through 

5006; with a main rotor spindle (spindle), 

part number (P/N) 28–14282–11 or 28– 

14282–13, installed, certificated in any 

category. This AD applies to any helicopter 

that has a spindle with 1,500 or more hours 

time-in-service (TIS) or where the hours TIS 

of the spindle is not known. 

(b) Unsafe Condition 

This AD defines the unsafe condition as a 

crack in the spindle, which, if not detected, 

could result in loss of a main rotor blade and 

subsequent loss of control of the helicopter. 

(c) Affected ADs 

This AD supersedes Emergency AD 2015– 

04–51, Directorate Identifier 2015–SW–002– 

AD, dated February 12, 2015. 

(d) Effective Date 

This AD becomes effective June 2, 2015 to 

all persons except those persons to whom it 

was made immediately effective by 

Emergency AD 2015–08–51, issued on April 

10, 2015, which contains the requirements of 

this AD. 

(e) Compliance 

You are responsible for performing each 

action required by this AD within the 

specified compliance time unless it has been 

accomplished on or after February 11, 2015. 


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Federal Register / Vol. 80, No. 95 / Monday, May 18, 2015 / Rules and Regulations 28175 

(f) Required Actions 

(1) Before further flight, conduct a 

magnetic particle inspection (MPI) of the 

spindle to determine if a crack exists, paying 

particular attention to the threaded portion of 

the spindle. The MPI of the spindle must be 

conducted by a Level II or Level III inspector 

qualified in the MPI in the Aeronautics 

Sector according to the EN4179 or NAS410 

standard or equivalent. If there is a crack in 

the spindle, replace it with an airworthy 

spindle before further flight. 

(2) Within 72 hours after accomplishing 

the MPI, report the information requested in 

Appendix 1 to this AD by mail to the 

Manager, Chicago Aircraft Certification 

Office, Federal Aviation Administration, 

ATTN: Gregory J. Michalik, 2300 East Devon 

Ave., Des Plaines, IL, 60018; by fax to (847) 

294–7834; or email to gregory.michalik@

faa.gov. 

(g) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Chicago Aircraft 

Certification Office, FAA, may approve 

AMOCs for this AD. Send your proposal to: 

Gregory J. Michalik, Senior Aerospace 

Engineer, Chicago Aircraft Certification 

Office, Small Airplane Directorate, FAA, 

2300 East Devon Ave., Des Plaines, IL, 60018; 

(847) 294–7135; email gregory.michalik@

faa.gov. 

(2) For operations conducted under a 14 

CFR part 119 operating certificate or under 

14 CFR 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. 

(3) Any AMOC approved previously in 

accordance with EAD 2015–04–51, dated 

February 12, 2015, is approved as an AMOC 

for the corresponding requirements in 

paragraph (f)(1) of this AD. 

(h) Additional Information 

Enstrom Helicopter Corporation Service 

Directive Bulletin No. 0119, Revision 1, 

dated April 1, 2015, and Enstrom Helicopter 

Corporation Service Directive Bulletin No. T– 

050, Revision 1, dated April 1, 2015, which 

are not incorporated by reference, contain 

additional information about the subject of 

this AD. For service information identified in 

this AD, contact Enstrom Helicopter 

Corporation, 2209 22nd Street, Menominee, 

MI; telephone (906) 863–1200; fax (906) 863– 

6821; or at www.enstromhelicopter.com. You 

may review this service information at the 

FAA, Office of the Regional Counsel, 

Southwest Region, 2601 Meacham Blvd., 

Room 663, Fort Worth, Texas 76137. 

(i) Subject 

Joint Aircraft Service Component (JASC) 

Code: 6220, Main Rotor Head. 

Appendix 1 to AD 2015–08–51 

Spindle Inspection (Sample Format) 

Provide the following information by mail 

to the Manager, Chicago Aircraft Certification 

Office, Federal Aviation Administration, 

ATTN: Gregory J. Michalik, 2300 East Devon 

Ave., Des Plaines, IL, 60018; by fax to (847) 

294–7834; or email to gregory.michalik@

faa.gov. 

Aircraft Registration No.: 

Helicopter Model: 

Helicopter Serial Number: 

Helicopter Owner or Operator: 

Contact Phone No.: 

Spindle Part Number and Serial Number: 

Total Hours Time-in-Service (TIS) on 

Spindle: 

Total Hours TIS on Helicopter (if hours TIS 

on spindle were not available): 

Who Performed the Inspection: 

Date and Location Inspection was 

Accomplished: 

Crack Found? If yes, describe the crack size, 

location, orientation (provide a sketch or 

picture): 

Provide Any Other Comments: 

Issued in Fort Worth, Texas, on May 8, 

2015. 

Lance T. Gant, 

Acting Directorate Manager, Rotorcraft 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–11732 Filed 5–15–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 100 

[Docket No. USCG–2015–0282] 

Eighth Coast Guard District Annual 

Marine Event; Mayor’s Hike, Bike and 

Paddle; Ohio River 602.0–603.5; 

Louisville, KY 

AGENCY: Coast Guard, DHS. 

ACTION: Notice of enforcement of 

regulation. 

SUMMARY: The Coast Guard will enforce 

the Mayor’s Hike, Bike and Paddle 

marine event for all waters of the Ohio 

River, beginning at mile marker 602.0 

and ending at 603.5, Louisville, KY. 

This rule will be enforced from 9:00 

a.m. to 12:30 p.m. on May 25, 2015. 

This action is necessary to protect 

persons, property, and infrastructure 

from potential damage and safety 

hazards associated with the Mayor’s 

Hike, Bike and Paddle. During the 

enforcement period, deviation from the 

regulations is prohibited unless 

specifically authorized by the Captain of 

the Port (COTP) Ohio Valley or a 

designated representative. 

DATES: The regulations in 33 CFR 

100.801, Table 1, Line 35 will be 

enforced from 9:00 a.m. to 12:30 p.m. on 

May 25, 2015. 

FOR FURTHER INFORMATION CONTACT: If 

you have questions on this document, 

call or email Petty Officer James C. 

Robinson, U.S. Coast Guard; telephone 

502–779–5347, email James.c.robinson@

uscg.mil or Petty Officer Stephen F. 

McConnell, U.S. Coast Guard; telephone 

502–779–5334, email 

Stephen.F.McConnell@uscg.mil. 

SUPPLEMENTARY INFORMATION: The Coast 

Guard will enforce the ‘‘Mayor’s Hike, 

Bike and Paddle’’ marine event in 33 

CFR 100.801, Table 1, Line 35 from 9:00 

a.m. to 12:30 p.m. on May 25, 2015. 

These regulations can be found in the 

Code of Federal Regulations, at 33 CFR 

100.801. 

Under the provisions of 33 CFR 

100.801, a vessel may not enter the 

regulated area, unless it receives 

permission from the COTP Ohio Valley 

or a designated representative. Spectator 

vessels may safely transit outside the 

regulated area but may not anchor, 

block, loiter in, or impede the transit of 

official patrol vessels. The Coast Guard 

may be assisted by other Federal, State, 

or local law enforcement agencies in 

enforcing this regulation. 

This document is issued under 

authority of 5 U.S.C. 552(a), and 33 

U.S.C. 1233. In addition to this 

document in the Federal Register, the 

Coast Guard will provide the maritime 

community with extensive advance 

notification of this enforcement period 

via the Local Notice to Mariners (LNM) 

and Broadcast Notice to Mariners 

(BNM). If the COTP Ohio Valley 

determines that the regulated area need 

not be enforced for the full duration 

stated in the notice, he or she may use 

a BNM to grant general permission to 

enter the regulated area. 

Dated: April 22, 2015. 

R.V. Timme, 

Captain, U.S. Coast Guard, Captain of the 

Port Ohio Valley. 

[FR Doc. 2015–11941 Filed 5–15–15; 8:45 am] 

BILLING CODE 9110–04–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 100 

[Docket No. USCG–2015–0240] 

RIN 1625–AA08 

Eighth Coast Guard District Annual 

Special Local Regulation; REV3 

Triathlon; Tennessee River 646.0– 

649.0; Knoxville, TN 

AGENCY: Coast Guard, DHS. 

ACTION: Notice of enforcement of 

regulation. 


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