This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

38391 

Vol. 80, No. 128 

Monday, July 6, 2015 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–2435; Directorate 

Identifier 2015–CE–020–AD; Amendment 

39–18197; AD 2015–13–10] 

RIN 2120–AA64 

Airworthiness Directives; M7 

Aerospace LLC Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are superseding 

Airworthiness Directive (AD) 2011–17– 

07 for certain M7 Aerospace LLC (type 

certificate previously held by M7 

Aerospace LP) Models SA226–T, 

SA226–T(B), SA226–TC, and SA226– 

AT airplanes. AD 2011–17–07 required 

repetitive replacement and inspection of 

certain elevator, rudder, aileron, and 

aileron-to-rudder interconnect primary 

control cables, and checking and setting 

of flight control cable tension. This AD 

requires repetitively inspecting and 

replacing the primary flight control 

rudder cables, repetitively replacing all 

other primary flight control and trim tab 

cables, and checking/setting the flight 

control cable tension. This AD was 

prompted by a report of extensive 

damage found on the left hand primary 

flight control rudder cable located under 

the cockpit floor on one of the airplanes 

affected by AD 2011–17–07. We are 

issuing this AD to correct the unsafe 

condition on these products. 

DATES: This AD is effective July 21, 

2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of July 21, 2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain other publication listed in 

this AD as of September 1, 2011 (76 FR 

50881, August 17, 2011). 

We must receive any comments on 

this AD by August 20, 2015. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, 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 W12–140, 1200 New Jersey 

Avenue SE., Washington, DC 20590, 

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

through Friday, except Federal holidays. 

For service information identified in 

this AD, contact M7 Aerospace LLC, 

10823 NE Entrance Road, San Antonio, 

Texas 78216; phone: (210) 824–9421; 

fax: (210) 804–7766; Internet: http://

www.elbitsystems-us.com; email: 

MetroTech@M7Aerospace.com. You 

may review this referenced service 

information at the FAA, Small Airplane 

Directorate, 901 Locust, Kansas City, 

Missouri 64106. For information on the 

availability of this material at the FAA, 

call (816) 329–4148. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

2435. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

2435; 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 this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (phone: 800–647– 

5527) is in the ADDRESSES section. 

Comments will be available in the AD 

docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Andrew McAnaul, Aerospace Engineer, 

FAA, ASW–143 (c/o San Antonio 

MIDO), 10100 Reunion Place, Suite 650, 

San Antonio, Texas 78216; phone: (210) 

308–3365; fax: (210) 308–3370; email: 

andrew.mcanaul@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On August 2, 2011, we issued AD 

2011–17–07, Amendment 39–16771 (76 

FR 50881, August 17, 2011), (‘‘AD 2011– 

17–07’’), for certain M7 Aerospace LLC 

(type certificate previously held by M7 

Aerospace LP) Models SA226–T, 

SA226–T(B), SA226–TC, and SA226– 

AT airplanes. AD 2011–17–07 required 

repetitive replacement and inspection of 

certain elevator, rudder, aileron, and 

aileron-to-rudder interconnect primary 

control cables, and checking and setting 

of flight control cable tension. AD 2011– 

17–07 resulted from a report that the 

left-hand primary rudder control cable 

on a Model SA226–T airplane failed 

where the cable makes a 30 degree angle 

over a small pulley to accommodate rerouting of the control cable alongside 

the camera system installed in the 

center of the cabin. 

We issued AD 2011–17–07 to prevent 

failure of a rudder, aileron and/or 

elevator control cable. 

Actions Since AD 2011–17–07 Was 

Issued 

Since we issued AD 2011–17–07, 

extensive damage to the left hand (LH) 

primary flight control rudder cable was 

found under the cockpit floor on one of 

the airplanes affected by AD 2011–17– 

07. Inspection of the cable revealed five 

of the seven wires that make up the LH 

cable were broken adjacent to the pulley 

at FS126.06. A follow-on inspection of 

the right hand (RH) primary flight 

control rudder cable also showed 

several strands of some of the 7 x 19 

cable wires were broken at the same RH 

FS126.06 pulley location. Both cables 

had been replaced at 1,513 hours timein-service (TIS) before the finding of the 

broken cables to comply with the 3,500- 

hour TIS replacement time required in 

AD 2011–17–07. 

We are issuing this AD to correct the 

unsafe condition on these products. 

Related Service Information Under 1 

CFR Part 51 

We reviewed M7 Aerospace SA226 

Series Service Bulletin 226–27–072, 

issued June 27, 2011, and M7 Aerospace 

SA226 Series Service Letter 226–SL– 

050, issued April 15, 2015. The service 


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38392 Federal Register / Vol. 80, No. 128 / Monday, July 6, 2015 / Rules and Regulations 

information describes procedures for 

repetitively inspecting and replacing all 

elevator, rudder, aileron, and aileron-torudder interconnect primary control 

cables. This service information is 

reasonably available because the 

interested parties have access to it 

through their normal course of business 

or by the means identified in the 

ADDRESSES section of this AD. 

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 the same 

type design. 

AD Requirements 

This AD retains the actions previously 

required in AD 2011–17–07 and adds 

new inspection and replacement 

requirements for the LH and RH primary 

flight control rudder cables. 

Differences Between This AD and the 

Service Information 

M7 Aerospace SA226 Series Service 

Bulletin 226–27–072, issued June 27, 

2011, requires replacing the LH and the 

RH primary flight control rudder cables 

every 3,500 hours TIS. This AD requires 

inspecting the LH and the RH primary 

flight control rudder cables every 200 

hours TIS and requires replacing the LH 

and the RH primary flight control 

rudder cables every 800 hours TIS. 

FAA’s Justification and 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 there are no airplanes 

currently on the U.S. registry and thus, 

does not have any impact upon the 

public. Therefore, we find that notice 

and opportunity for prior public 

comment are unnecessary and that good 

cause exists for making this amendment 

effective in less than 30 days. 

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 before it becomes effective. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include Docket No. FAA–2015– 

2435 and Directorate Identifier 2015– 

CE–020–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. 

Costs of Compliance 

There are no affected airplanes 

currently on the U.S. registry. However, 

if an airplane affected by this AD were 

to become a U.S.-registered airplane, we 

estimate the following costs to comply 

with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Inspection of all elevator, rudder, aileron, and aileron-to-rudder interconnect primary control cables.100 work-hours × $85 per hour = 

$8,500.

Not Applicable ......... $8,500 None to date. 

Replacement of all elevator, rudder, aileron, and 

aileron-to-rudder interconnect primary control 

cables.

180 work-hours × $85 per hour = 

$15,300.

$18,800 ................... 34,100 None to date. 

Check (set) flight control cable tension ................. 25 work-hours × $2,125 .............. Not Applicable ......... 2,125 None to date. 

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 

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 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, 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. 

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 part 39 of the Federal 

Aviation Regulations (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 Airworthiness Directive (AD) 

2011–17–07, Amendment 39–16771 (76 


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Federal Register / Vol. 80, No. 128 / Monday, July 6, 2015 / Rules and Regulations 38393 

FR 50881, August 17, 2011) and adding 

the following new AD: 

2015–13–10 M7 Aerospace LLC (type 

certificate previously held by M7 

Aerospace LP): Amendment 39–18197; 

Docket No. FAA–2015–2435; Directorate 

Identifier 2015–CE–020–AD. 

(a) Effective Date 

This AD is effective July 21, 2015. 

(b) Affected ADs 

(1) This AD supersedes AD 2011–17–07, 

Amendment 39–16771 (76 FR 50881, August 

17, 2011) (‘‘AD 2011–17–07’’). 

(2) AD 87–02–02, Amendment 39–5518 (52 

FR 2511, January 23, 1987) relates to the 

subject of this AD. 

(c) Applicability 

This AD applies to the following M7 

Aerospace LLC airplanes, certificated in any 

category, as identified in table 1 of paragraph 

(c) of this AD: 

TABLE 1 OF PARAGRAPH (C) OF THIS

AD—APPLICABILITY

Model Serial numbers 

SA226–T .............. T265, T267 

SA226–T(B) ......... T(B)348 

SA226–TC ............ TC277 

SA226–AT ............ AT071, AT072, AT073 

(d) Subject 

Joint Aircraft System Component (JASC)/

Air Transport Association (ATA) of America 

Code 27, Flight Controls. 

(e) Unsafe Condition 

This AD was prompted by a report of 

extensive damage found to the left hand 

primary flight control rudder cable located 

under the cockpit floor on one of the 

airplanes affected by AD 2011–17–07. We are 

issuing this AD to prevent failure of a rudder, 

aileron and/or elevator control cable. 

(f) Compliance 

Unless already done, comply with 

paragraphs (g) through (k) of this AD. If the 

hours time-in-service (TIS) of the control 

cables cannot be positively determined by 

the logbook, then you must use hours TIS of 

the airplane to comply with the requirements 

of this AD. 

(g) Primary Flight Control Rudder Cable 

Inspection 

Within the next 10 hours TIS after July 21, 

2015 (the effective date of this AD) or within 

the next 60 days after July 21, 2015 (the 

effective date of this AD), whichever occurs 

first, and repetitively thereafter at or before 

reaching 200 hours TIS from the last 

inspection or replacement, do a detailed 

visual inspection of the left hand (LH) and 

right hand (RH) primary flight control rudder 

cables under the floor between FS 116.56 and 

FS 138.56, with specific focus on the cable 

and the pulley at FS126.06. Do the inspection 

as stated in paragraph 4. ACTION of M7 

Aerospace SA226 Series Service Letter 226– 

SL–050, issued April 15, 2015, following the 

procedures specified in paragraph 2. 

ACCOMPLISHMENT INSTRUCTIONS, 

section B., subparagraph (2) of M7 Aerospace 

SA226 Series Service Bulletin 226–27–072, 

issued June 27, 2011. 

(h) Primary Flight Control Rudder Cable OnCondition Replacement 

Before further flight after any inspection 

required in paragraph (g) of this AD, if any 

one of the conditions described in paragraph 

2. ACCOMPLISHMENT INSTRUCTIONS, 

section B., subparagraphs (3)(a) through 

(3)(d) of M7 Aerospace SA226 Series Service 

Bulletin 226–27–072, issued June 27, 2011, is 

found, replace the affected primary flight 

control rudder cable or cables with a new 

cable. Do the replacements following 

paragraph 2. ACCOMPLISHMENT 

INSTRUCTIONS, sections C. through E., 

including all subparagraphs of M7 Aerospace 

Service Bulletin 226–27–072, issued June 27, 

2011. 

(i) Primary Flight Control Rudder Cable 

Mandatory Life Limit Replacement 

Within the next 800 hours TIS after the last 

replacement or within the next 50 hours TIS 

after July 21, 2015 (the effective date of this 

AD), whichever occurs later, and repetitively 

thereafter every 800 hours TIS, replace the 

LH and RH primary flight control rudder 

cables with new cables. Do the replacements 

following paragraph 2. ACCOMPLISHMENT 

INSTRUCTIONS, sections C. through E., 

including all subparagraphs of M7 Aerospace 

SA226 Series Service Bulletin 226–27–072, 

issued June 27, 2011. 

(j) Primary Flight Control and Trim Tab 

Cable (Other Than Rudder Cables) 

Mandatory Life Limit Replacement 

(1) For cables with more than 6,000 hours 

TIS: Inspect cables for deficiencies within 10 

hours TIS after September 1, 2011, (the 

effective date retained from AD 2011–17–07). 

(2) If any deficiencies are found during the 

inspection required in paragraph (j)(1) of this 

AD, before further flight replace the cable(s). 

(3) Replace all other primary control and 

trim tab cables (pilot and co-pilot aileron 

cables, rudder/aileron interconnect cables, 

aileron trim tab cables, rudder trim tab 

cables, and elevator cables) within the initial 

compliance times as listed in paragraphs 

(j)(3)(i) through (j)(3)(iii) below and 

repetitively thereafter at intervals not to 

exceed 3,500 hours TIS. Do the replacements 

following paragraph 2. ACCOMPLISHMENT 

INSTRUCTIONS, sections C. through E., 

including all subparagraphs of M7 Aerospace 

SA226 Series Service Bulletin 226–27–072, 

issued June 27, 2011. 

(i) For cables with less than or equal to 

3,500 hours TIS: replace cables when the 

control cables reach a total of 3,500 hours TIS 

or 150 hours TIS after September 1, 2011, 

(the effective date retained from AD 2011– 

17–07), whichever occurs later. 

(ii) For cables with less than or equal to 

5,000 hours TIS but greater than 3,500 hours 

TIS: replace cables within 150 hours TIS after 

September 1, 2011, (the effective date 

retained from AD 2011–17–07). 

(iii) For cables with more than 5,000 hours 

TIS: replace cables within 50 hours TIS after 

September 1, 2011, (the effective date 

retained from AD 2011–17–07). 

(k) Set Flight Control Cable Tension 

Between 50 hours TIS and 200 hours TIS 

after installing any new control cable as 

required in paragraphs (g) through (j) of this 

AD, including all subparagraphs, check (set) 

flight control cable tension following 

paragraph 2. ACCOMPLISHMENT 

INSTRUCTIONS, sections C. through E. of 

M7 Aerospace SA226 Series Service Bulletin 

226–27–072, issued June 27, 2011. 

(l) Paperwork Reduction Act Burden 

Statement 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject to 

a 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 OMB Control Number for this 

information collection is 2120–0056. Public 

reporting for this collection of information is 

estimated to be approximately 5 minutes per 

response, including the time for reviewing 

instructions, completing and reviewing the 

collection of information. All responses to 

this collection of information are 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. 

(m) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Fort Worth Airplane 

Certification Office, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of the ACO, send it to the 

attention of the person identified in 

paragraph (n) of this AD. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/

certificate holding district office. 

(3) AMOCs approved for AD 2011–17–07, 

Amendment 39–16771 (76 FR 50881, August 

17, 2011) are not approved as AMOCs for the 

corresponding provisions of this AD. 

(n) Related Information 

For more information about this AD, 

contact Andrew McAnaul, Aerospace 

Engineer, FAA, ASW–143 (c/o San Antonio 

MIDO), 10100 Reunion Place, Suite 650, San 

Antonio, Texas 78216; phone: (210) 308– 

3365; fax: (210) 308–3370; email: 

andrew.mcanaul@faa.gov. 

(o) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 


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(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(3) The following service information was 

approved for IBR on July 21, 2015. 

(i) M7 Aerospace SA226 Series Service 

Letter 226–SL–050, issued April 15, 2015. 

(ii) Reserved. 

(4) The following service information was 

approved for IBR on September 1, 2011 (76 

FR 50881, August 17, 2011). 

(i) M7 Aerospace SA226 Series Service 

Bulletin 226–27–072, issued June 27, 2011. 

(ii) Reserved. 

(5) For M7 Aerospace LLC service 

information identified in this AD, contact M7 

Aerospace LLC, 10823 NE Entrance Road, 

San Antonio, Texas 78216; phone: (210) 824– 

9421; fax: (210) 804–7766; Internet: http://

www.elbitsystems-us.com; email: 

MetroTech@M7Aerospace.com. 

(6) You may view this service information 

at FAA, FAA, Small Airplane Directorate, 

901 Locust, Kansas City, Missouri 64106. For 

information on the availability of this 

material at the FAA, call (816) 329–4148. 

(7) You may view this 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/cfr/ibrlocations.html. 

Issued in Kansas City, Missouri, on June 

25, 2015. 

Earl Lawrence, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2015–16171 Filed 7–2–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 100 

[Docket No. USCG–2015–0376] 

RIN 1625–AA08 

Special Local Regulations; Annual 

Events in the Captain of the Port 

Detroit Zone 

AGENCY: Coast Guard, DHS. 

ACTION: Notice of enforcement of 

regulation. 

SUMMARY: The Coast Guard will enforce 

the safety zones for annual marine 

events in the Captain of the Port Detroit 

zone on the dates and times noted 

below. This action is necessary and 

intended to ensure safety of life on the 

navigable waters immediately prior to, 

during, and immediately after marine 

events. During the aforementioned 

period, the Coast Guard will enforce 

restrictions upon, and control 

movement of, vessels in a portion of the 

Captain of the Port Detroit zone. 

DATES: The regulations in 33 CFR 

100.921, 33 CFR 100.927, and 33 CFR 

100.928 will be enforced on the dates 

and times noted below. 

FOR FURTHER INFORMATION CONTACT: If 

you have questions on this notice, call 

or email LT Jennifer M. Disco, 

Waterways Branch Chief, Marine Safety 

Unit Toledo, 420 Madison Ave., Suite 

700, Toledo, OH 43604; telephone (419) 

418–6023; email Jennifer.M.Disco@

uscg.mil. 

SUPPLEMENTARY INFORMATION: The Coast 

Guard will enforce the special local 

regulations listed in 33 CFR 100.921, 33 

CFR 100.927, and 33 CFR 100.928, 

Special Local Regulations; Annual 

Events in the Captain of the Port Detroit 

Zone, at the following times for the 

following events: 

(1) Kelley’s Island Swim, Lake Erie, 

Lakeside, OH. The special local 

regulation listed in 33 CFR 100.921 will 

be enforced from 7 a.m. until 11 a.m. on 

July 15, 2015. This special local 

regulation will encompass all U.S. 

navigable waters of Lake Erie, Lakeside, 

OH, contained by a line connecting the 

following points: two points on land at 

the Lakeside dock, 41°32′51.96′′ N./

082°45′3.15′′ W. and 41°32′52.21′′ N./

082°45′2.19′′ W., and two points on 

Kelley’s Island at the Kelley’s Island 

Dock, 41°35′24.59′′ N./082°42′16.61′′ W., 

and 41°35′24.44′′ N./082°42′16.04′′ W. 

(NAD 83). 

(2) Dragon Boat Races, Maumee River; 

Toledo, OH. The special local regulation 

listed in 33 CFR 100.927 will be 

enforced from 6 a.m. to 6 p.m. on June 

20, 2015. This special local regulation 

will encompass all U.S. navigable 

waters of the Maumee River, Toledo, 

OH, bound by a line extending from a 

point on land just north of the Cherry 

Street Bridge at position 41°39′5.27′′ N.; 

083°31′34.01′′ W. straight across the 

river along the Cherry Street bridge to 

position 41°39′12.83′′ N.; 083°31′42.58′′ 

W. and a line extending from a point of 

land just south of International Park at 

position 41°38′46.62′′ N.; 083°31′50.54′′ 

W. straight across the river to the shore 

adjacent to position 41°38′47.37′′ N.; 

083°32′2.05′′ W. (NAD 83). 

(3) Frogtown Race Regatta, Toledo, 

OH. The special local regulation listed 

in 33 CFR 100.928 will be enforced from 

5 a.m. to 7 p.m. on September 26, 2015. 

This special local regulation will 

encompass all navigable waters of the 

United States on the Maumee River, 

Toledo, OH, from the Norfolk and 

Southern Railway Bridge at River Mile 

1.80 to the Anthony Wayne Bridge at 

River Mile 5.16. 

Under the provisions of 33 CFR 

100.921, 33 CFR 100.927, and 33 CFR 

100.928, vessels transiting within the 

regulated area shall travel at a no-wake 

speed and remain vigilant for event 

participants and safety craft. 

Additionally, vessels shall yield rightof-way for event participants and event 

safety craft and shall follow directions 

given by the Coast Guard’s on-scene 

representative or by event 

representatives during the event. The 

‘‘on-scene representative’’ of the Captain 

of the Port Detroit is any Coast Guard 

commissioned, warrant, or petty officer 

who has been designated by the Captain 

of the Port Detroit to act on his behalf. 

The on-scene representative of the 

Captain of the Port Detroit will be 

aboard either a Coast Guard or Coast 

Guard Auxiliary vessel. The Captain of 

the Port, Sector Detroit or his designated 

on scene representative may be 

contacted via VHF Channel 16. 

Dated: June 8, 2015. 

Scott B. Lemasters, 

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

Port Detroit. 

[FR Doc. 2015–16530 Filed 7–2–15; 8:45 am] 

BILLING CODE 9110–04–P 

DEPARTMENT OF HOMELAND 

SECURITY 

Coast Guard 

33 CFR Part 100 

[Docket Number USCG–2015–0328] 

RIN 1625–AA08 

Special Local Regulations For Marine 

Events, Manasquan River; Seaside 

Park, New Jersey 

AGENCY: Coast Guard, DHS. 

ACTION: Temporary final rule. 

SUMMARY: The Coast Guard is 

temporarily changing the enforcement 

date of the special local regulation for 

the recurring New Jersey Offshore Grand 

Prix, held in the waters of the 

Manasquan River and Atlantic Ocean, 

near Seaside Park, New Jersey. The 

change of enforcement date for the 

special local regulation is necessary to 

provide for the safety of life on 

navigable waters during the event. This 

action will restrict vessel traffic in the 

waters of the Manasquan River and 

Atlantic Ocean near Seaside Park, New 

Jersey, from 10:00 a.m. to 5:00 p.m. on 

July 9, 2015, and July 10, 2015. 

DATES: This rule is effective from July 9 

to July 30, 2015. 

ADDRESSES: Documents mentioned in 

this preamble are part of docket [USCG– 


Lhorne on DSK7TPTVN1PROD with RULES