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

43615 

Vol. 80, No. 141 

Thursday, July 23, 2015 

DEPARTMENT OF AGRICULTURE 

Animal and Plant Health Inspection 

Service 

7 CFR Part 319 

Foreign Quarantine Notices 

CFR Correction 

In Title 7 of the Code of Federal 

Regulations, Parts 300 to 399, revised as 

of January 1, 2015, on page 372, in 

§ 319.56–57, paragraph (c)(2) is correctly 

reinstated to read as follows: 

§ 319.56–57 Sand pears from China. 

* * * * * 

(c) * * * 

(2) Packinghouses must have a 

tracking system in place to readily 

identify all sand pears that enter the 

packinghouse destined for export to the 

United States back to their place of 

production. 

* * * * * 

[FR Doc. 2015–18071 Filed 7–22–15; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF AGRICULTURE 

Commodity Credit Corporation 

7 CFR Part 1412 

Agriculture Risk Coverage, Price Loss 

Coverage, and Cotton Transition 

Assistance Programs 

CFR Correction 

In Title 7 of the Code of Federal 

Regulations, Parts 1200 to 1599, revised 

as of January 1, 2015, on page 516, in 

§ 1412.45, in paragraph (b)(3), the term 

‘‘P&CP’’ is replaced with the term 

‘‘planted’’. 

[FR Doc. 2015–18072 Filed 7–22–15; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–2906; Directorate 

Identifier 2014–SW–068–AD; Amendment 

39–18213; AD 2015–15–04] 

RIN 2120–AA64 

Airworthiness Directives; Bell 

Helicopter Textron, Inc. 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Bell Helicopter Textron, Inc. (Bell), 

Model 204B, 205A, 205A–1, and 212 

helicopters. This AD requires removing 

a certain part-numbered main rotor (M/ 

R) blade grip (grip) from service. This 

AD is prompted by an error in a parts 

manufacturer approval (PMA) that 

incorrectly allows installation of the 

grips on the Bell Model 212. The actions 

specified in this AD are intended to 

prevent grip failure, separation of the 

M/R blade, and subsequent loss of 

control of the helicopter. 

DATES: This AD becomes effective 

August 7, 2015. We must receive 

comments on this AD by September 21, 

2015. 

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 Timken service information 

identified in this AD, contact Timken 

Alcor Aerospace Technologies, Inc., 

Aftermarket Customer Service, 3110 N. 

Oakland, Mesa, AZ 85215; telephone 1– 

480–606–3130; email 

timkenaftermarketsales@timken.com; or 

at http://www.timken.com/en-us/

solutions/aerospace/aftermarket/Pages/

default.aspx. You may review the 

referenced service information at the 

FAA, Office of the Regional Counsel, 

Southwest Region, 10101 Hillwood 

Pkwy, Room 6N–321, Fort Worth, TX 

76177. 

FOR FURTHER INFORMATION CONTACT: 

Scott Franke, Aviation Safety Engineer, 

Fort Worth Aircraft Certification Office, 

Rotorcraft Directorate, FAA, 10101 

Hillwood Pkwy, Fort Worth, TX 76177; 

telephone (817) 222–5170; email 

scott.franke@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. 


rmajette on DSK7SPTVN1PROD with RULES
43616 Federal Register / Vol. 80, No. 141 / Thursday, July 23, 2015 / Rules and Regulations 

Discussion 

We are adopting a new AD for Bell 

Model 204B, 205A, 205A–1, and 212 

helicopters with a grip part number (P/ 

N) ASI–4011–121–113 installed. This 

AD requires removing any grip from 

service if the grip is currently or has 

ever been installed on a Bell Model 212 

helicopter, or if it is unknown whether 

the grip has ever been installed on a 

Model 212 helicopter. This AD also 

prohibits installing grip P/N ASI–4011– 

121–113 on any helicopter if the grip 

has ever been installed on a Bell Model 

212 helicopter. This AD is prompted by 

an error in the PMA that allows 

installing the subject grip on the Bell 

Model 212. 

Grip P/N ASI–4011–121–113 is 

currently produced by Timken Alcor 

Aerospace Technologies, Inc., under a 

PMA as a replacement grip for Bell P/ 

N 204–011–121–113. This approval 

incorrectly listed grip P/N ASI–4011– 

121–113 as eligible for installation on 

Bell Model 212 helicopters. The PMA 

has been revised to remove that 

eligibility. This grip was previously 

produced and sold as a replacement grip 

for Bell P/N 204–011–121–113 by Air 

Services International of Scottsdale, AZ, 

as P/N ASI–4011–121–113. The actions 

required in this AD are intended to 

prevent installation of an unapproved 

grip, which could result in grip failure, 

separation of the M/R blade, and 

subsequent loss of control of the 

helicopter. 

FAA’s Determination 

We are issuing this AD because we 

evaluated all known relevant 

information and determined that the 

unsafe condition described previously is 

likely to exist in other products of these 

same type designs. 

Related Service Information 

We reviewed Timken T–700 Service 

Bulletin, Revision B, dated October 20, 

2014. The service bulletin specifies the 

airworthiness life limitations and 

inspection interval schedule for various 

Timken Alcor Aerospace Technologies, 

Inc., replacement parts and articles. 

AD Requirements 

This AD requires, within 5 hours 

time-in-service (TIS), removing any grip 

P/N ASI–4011–121–113 from service if 

the grip is currently or has ever been 

installed on a Bell Model 212 

helicopter. This AD also prohibits 

installing a grip P/N ASI–4011–121–113 

on any helicopter if the grip is currently 

or has ever been installed on a Bell 

Model 212 helicopter. 

Differences Between This AD and the 

Service Information 

The Timken service bulletin provides 

the airworthiness limitations and 

inspection intervals for various life 

limited parts, including grip P/N ASI– 

4011–121–113. This AD only applies to 

helicopters with grip P/N ASI–4011– 

121–113 and requires removing the grip 

from service if it is currently or has ever 

been installed on a Bell Model 212 

helicopter. 

Costs of Compliance 

We estimate that this AD could affect 

130 helicopters of U.S. Registry. We 

estimate that operators may incur the 

following costs in order to comply with 

this AD. It takes about 20 work-hours to 

replace two M/R grips per helicopter. 

We estimate an average labor rate of $85 

per work-hour, and a required parts cost 

of approximately $56,385 for two grips. 

Based on these figures, we estimate a 

total cost of $58,085 per helicopter and 

$7,551,050 for the U.S. fleet. 

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 find that the risk to the 

flying public justifies waiving notice 

and comment prior to the adoption of 

this rule because the unsafe condition 

can adversely affect control of the 

helicopter and the required corrective 

actions must be accomplished within 5 

hours TIS. 

Since an unsafe condition exists that 

requires the immediate adoption of this 

AD, we determined that notice and 

opportunity for public comment before 

issuing this AD are impracticable and 

contrary to the public interest and that 

good cause exists for making this 

amendment effective in less than 30 

days. 

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 would 

not have federalism implications under 

Executive Order 13132. This AD would 

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 the 

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): 

2015–15–04 Bell Helicopter Textron, Inc. 

(Bell): Amendment 39–18213; Docket 

No. FAA–2015–2906; Directorate 

Identifier 2014–SW–068–AD. 

(a) Applicability 

This AD applies to the following 

helicopters, certificated in any category: 

(1) Bell Model 204B, 205A, and 205A–1 

helicopters, with a main rotor (M/R) blade 

grip (grip) part number (P/N) ASI–4011–121– 


rmajette on DSK7SPTVN1PROD with RULES
Federal Register / Vol. 80, No. 141 / Thursday, July 23, 2015 / Rules and Regulations 43617 

113 installed, if the grip was ever installed 

on a Model 212 helicopter or if it is unknown 

whether a grip was ever installed on a Model 

212 helicopter; and 

(2) Bell Model 212 helicopters, with a grip 

P/N ASI–4011–121–113 installed. 

(b) Unsafe Condition 

This AD defines the unsafe condition as 

installation of a grip that does not meet type 

design. This condition could result in grip 

failure, separation of the M/R blade, and 

subsequent loss of control of the helicopter. 

(c) Effective Date 

This AD becomes effective August 7, 2015. 

(d) Compliance 

You are responsible for performing each 

action required by this AD within the 

specified compliance time unless it has 

already been accomplished prior to that time. 

(e) Required Actions 

(1) Within 5 hours time-in-service, remove 

each grip from service. 

(2) Do not install a grip listed in paragraph 

(a) of this AD on any helicopter. 

(f) Alternative Methods of Compliance 

(AMOC) 

(1) The Manager, Fort Worth Aircraft 

Certification Office, FAA, may approve 

AMOCs for this AD. Send your proposal to: 

Scott Franke, Aviation Safety Engineer, Fort 

Worth Aircraft Certification Office, Rotorcraft 

Directorate, FAA, 10101 Hillwood Pkwy, Fort 

Worth, TX 76177; telephone (817) 222–5170; 

email scott.franke@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. 

(g) Additional Information 

Timken T–700 Service Bulletin, Revision 

B, dated October 20, 2014, which is not 

incorporated by reference, contains 

additional information about the subject of 

this AD. For Timken service information 

identified in this AD, contact Timken Alcor 

Aerospace Technologies, Inc., Aftermarket 

Customer Service, 3110 N. Oakland, Mesa, 

AZ 85215; telephone 1–480–606–3130; email 

timkenaftermarketsales@timken.com; or at 

http://www.timken.com/en-us/solutions/

aerospace/aftermarket/Pages/default.aspx. 

You may review a copy of this service 

information at the FAA, Office of the 

Regional Counsel, Southwest Region, 10101 

Hillwood Pkwy, Room 6N–321, Fort Worth, 

TX 76177. 

(h) Subject 

Joint Aircraft Service Component (JASC) 

Code: 6620, Main Rotor Blade Grip. 

Issued in Fort Worth, Texas, on July 13, 

2015. 

Bruce E. Cain, 

Acting Directorate Manager, Rotorcraft 

Directorate, Aircraft Certification Service. 

[FR Doc. 2015–17953 Filed 7–22–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 73 

[Docket No. FAA–2014–0640; Airspace 

Docket No. 14–ACE–4] 

RIN 2120–AA66 

Modification of Restricted Areas R– 

4501A, R–4501B, R–4501C, R–4501D, 

R–4501F, and R–4501H; Fort Leonard 

Wood, MO 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: This action corrects a final 

rule published in the Federal Register 

on May 26, 2015 by adding one set of 

geographic latitude/longitude 

coordinates that was inadvertently 

omitted from the restricted area R– 

4501H boundary description. 

DATES: Effective date 0901 UTC, August 

20, 2015. 

FOR FURTHER INFORMATION CONTACT: 

Colby Abbott, Airspace Policy and 

Regulations Group, Office of Airspace 

Services, Federal Aviation 

Administration, 800 Independence 

Avenue SW., Washington, DC 20591; 

telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

History 

A final rule was published in the 

Federal Register on May 26, 2015 (80 

FR 29941), that established a single 

ceiling of one restricted area (R–4501B), 

added exclusions to three restricted 

areas (R–4501C, R–4501F, and R– 

4501H) to prevent overlapped restricted 

areas being active at the same time, 

made administrative changes to the title 

of two restricted areas (R–4501A and R– 

4501B), and made administrative 

changes to the using agency information 

of six restricted areas (R–4501A–D, R– 

4501F, and R–4501H) in Fort Leonard 

Wood, MO. Subsequent to publication, 

the FAA determined that one set of 

geographic latitude/longitude 

coordinates was inadvertently omitted 

from the R–4501H boundary 

description. This correction inserts the 

set of geographic latitude/longitude 

coordinates back into the R–4501H 

boundary description to retain the 

lateral boundary of the restricted area as 

it existed prior to the published final 

rule. 

Correction to Final Rule 

Accordingly, pursuant to the 

authority delegated to me, in Docket No. 

FAA–2014–0640, the boundary 

description for restricted area R–4501H, 

as published in the Federal Register on 

May 26, 2015 (80 FR 29941), FR Doc. 

2015–12627, modifying the restricted 

areas at Fort Leonard Wood, MO, is 

corrected as follows: 

§ 73.45 (Amended) 

On page 29942, column 2, line 57, 

after the words ‘‘Reservation boundary;’’ 

insert ‘‘to lat. 37°46′45′′ N., long. 

92°01′41′′ W.;’’. 

Issued in Washington, DC, on July 16, 

2015. 

Gary A. Norek, 

Manager, Airspace Policy and Regulations 

Group. 

[FR Doc. 2015–18012 Filed 7–22–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 95 

[Docket No. 31030; Amdt. No. 521] 

IFR Altitudes; Miscellaneous 

Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This amendment adopts 

miscellaneous amendments to the 

required IFR (instrument flight rules) 

altitudes and changeover points for 

certain Federal airways, jet routes, or 

direct routes for which a minimum or 

maximum en route authorized IFR 

altitude is prescribed. This regulatory 

action is needed because of changes 

occurring in the National Airspace 

System. These changes are designed to 

provide for the safe and efficient use of 

the navigable airspace under instrument 

conditions in the affected areas. 

DATES: Effective 0901 UTC, August 20, 

2015. 

FOR FURTHER INFORMATION CONTACT: 

Richard A. Dunham, Flight Procedure 

Standards Branch (AMCAFS–420), 

Flight Technologies and Programs 

Division, Flight Standards Service, 

Federal Aviation Administration, Mike 

Monroney Aeronautical Center, 6500 

South MacArthur Blvd. Oklahoma City, 

OK 73169 (Mail Address: P.O. Box 


rmajette on DSK7SPTVN1PROD with RULES