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

36387 

Vol. 79, No. 124 

Friday, June 27, 2014 

DEPARTMENT OF AGRICULTURE 

Food and Nutrition Service 

7 CFR Parts 210 and 245 

RIN 0584–AE17 

National School Lunch Program: 

Independent Review of Applications 

Required by the Healthy, Hunger-Free 

Kids Act of 2010; Approval of 

Information Collection Request 

AGENCY: Food and Nutrition Service, 

USDA. 

ACTION: Final rule; Notice of approval of 

Information Collection Request (ICR). 

SUMMARY: In accordance with the 

Paperwork Reduction Act of 1995 

(PRA), the Food and Nutrition Service 

(FNS) is announcing the Office of 

Management and Budget’s (OMB) 

approval of information collection 

requirements contained in a final rule 

published in the Federal Register. 

DATES: The ICR associated with the 

National School Lunch Program: 

Independent Review of Applications 

Required by the Healthy, Hunger-Free 

Kids Act of 2010 rule published in the 

Federal Register on February 6, 2014 

(79 FR 7049), and effective March 10, 

2014, was approved by OMB on March 

12, 2014. 

FOR FURTHER INFORMATION CONTACT: 

Lynn Rodgers-Kuperman, Chief, 

Program Monitoring Branch, Child 

Nutrition Programs, Food and Nutrition 

Service at (703) 305–2590. 

SUPPLEMENTARY INFORMATION: The rule 

titled National School Lunch Program: 

Independent Review of Applications 

Required by the Healthy, Hunger-Free 

Kids Act of 2010 was published on 

February 6, 2014. OMB cleared the 

associated ICR on March 12, 2014 under 

0584–0573. The ICR approved under 

0584–0573 has been transferred to 

0584–0026. 

This document announces approval of 

the ICR. 

Dated: June 19, 2014. 

Audrey Rowe, 

Administrator, Food and Nutrition Service. 

[FR Doc. 2014–15092 Filed 6–26–14; 8:45 am] 

BILLING CODE 3410–30–P 

DEPARTMENT OF THE TREASURY 

Comptroller of the Currency 

12 CFR Part 5 

Rules, Policies, and Procedures for 

Corporate Activities 

CFR Correction 

■ In Title 12 of the Code of Federal 

Regulations, Parts 1 to 199, revised as of 

January 1, 2014, on page 293, in § 5.20, 

the first sentence of paragraph (i)(5)(ii) 

is moved to the end of paragraph 

(i)(5)(i). 

[FR Doc. 2014–15105 Filed 6–26–14; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF THE TREASURY 

Comptroller of the Currency 

12 CFR Part 5 

Rules, Policies, and Procedures for 

Corporate Activities 

CFR Correction 

■ In Title 12 of the Code of Federal 

Regulations, parts 1 to 199, revised as of 

January 1, 2014, on page 310, in § 5.34, 

the word ‘‘and’’ is added to the end of 

paragraph (e)(5)(vi)(C). 

[FR Doc. 2014–15108 Filed 6–26–14; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF THE TREASURY 

Comptroller of the Currency 

12 CFR Part 23 

Leasing 

CFR Correction 

■ In Title 12 of the Code of Federal 

Regulations, parts 1 to 199, revised as of 

January 1, 2014, on page 466, in § 23.6, 

remove the phrase ‘‘and Regulation W, 

12 CFR part 223’’ from the third 

sentence and add it to the end of the 

first sentence. Also, on the same page, 

in the same section, remove the 

quotation mark and the word ‘‘before’’ 

from the third sentence. 

[FR Doc. 2014–15111 Filed 6–26–14; 8:45 am] 

BILLING CODE 1505–01–P 

DEPARTMENT OF THE TREASURY 

Comptroller of the Currency 

12 CFR Part 37 

Debt Cancellation Contracts and Debt 

Suspension Agreements 

CFR Correction 

■ In Title 12 of the Code of Federal 

Regulations, parts 1 to 199, revised as of 

January 1, 2014, on page 617, in § 37.7, 

in paragraph (a), in the first sentence, 

‘‘§ 37.6(d)’’ is corrected to read 

‘‘§ 37.6(b)’’ and in the last sentence 

‘‘§ 37.6(b)’’ is corrected to read 

‘‘§ 37.6(d)’’. 

[FR Doc. 2014–15113 Filed 6–26–14; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0281; Directorate 

Identifier 2014–NE–05–AD; Amendment 39– 

17878; AD 2014–13–03] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Rolls-Royce plc (RR) RB211 Trent 553– 

61, 553A2–61, 556–61, 556A2–61, 

556B–61, 556B2–61, 560–61, and 

560A2–61 turbofan engines. We are 

issuing this AD to address, through an 

update to the electronic engine control 

(EEC) software, multiple risks of 

uncontained engine failure and damage 

to the airplane. 

DATES: This AD becomes effective July 

14, 2014. 


wreier-aviles on DSK5TPTVN1PROD with RULES
36388 Federal Register / Vol. 79, No. 124 / Friday, June 27, 2014 / Rules and Regulations 

We must receive comments on this 

AD by August 11, 2014. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov and follow 

the instructions for sending your 

comments electronically. 

• Mail: U.S. Department of 

Transportation, 1200 New Jersey 

Avenue SE., West Building Ground 

Floor, Room W12–140, Washington, DC 

20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• Fax: 202–493–2251. 

For service information identified in 

this AD, contact Rolls-Royce plc, 

Corporate Communications, P.O. Box 

31, Derby, England, DE248BJ; phone: 

011–44–1332–242424; fax: 011–44– 

1332–249936; email: http://www.rollsroyce.com/contact/civil_team.jsp; 

Internet: https://www.aeromanager.com. 

You may view this service information 

at the FAA, Engine & Propeller 

Directorate, 12 New England Executive 

Park, Burlington, MA. For information 

on the availability of this material at the 

FAA, call 781–238–7125. 

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–2014– 

0281; 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 mandatory 

continuing airworthiness information 

(MCAI), the regulatory evaluation, any 

comments received, and other 

information. The address for the Docket 

Office (phone: 800–647–5527) is in 

ADDRESSES section. Comments will be 

available in the AD docket shortly after 

receipt. 

FOR FURTHER INFORMATION CONTACT: 

Mark Riley, Aerospace Engineer, Engine 

Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: (781) 238–7758; fax: (781) 238– 

7199; email: mark.riley@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments about this AD. 

Send your comments to an address 

listed under the ADDRESSES section. 

Include ‘‘Docket No. FAA–2014–0281; 

Directorate Identifier 2014–NE–05–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 with FAA 

personnel concerning this AD. 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued EASA AD 2014– 

0086, dated April 11, 2014 (referred to 

hereinafter as ‘‘the MCAI’’), to correct an 

unsafe condition for the specified 

products. The MCAI states: 

Investigation carried out by RR has 

identified the risk of fan flutter during 

ground maintenance running, which 

indicated the need to introduce a fan flutter 

Keep Out Zone (KOZ). In addition, following 

Intermediate Pressure (IP) turbine overspeed 

events experienced on other Trent series 

engines, the need to introduce a protection 

against IP shaft failures in the event of an 

internal engine fire was identified. 

Fan flutter may result in multiple fan blade 

failures and consequent release of 

uncontained high energy debris. An 

unprotected IP shaft failure may result in IP 

turbine overspeed, IP turbine burst and, 

ultimately, release of uncontained high 

energy debris. These conditions, if not 

corrected, could result in damage to, and 

reduced control of, the aeroplane. 

You may obtain further information 

by examining the MCAI in the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

0281. 

Relevant Service Information 

RR has issued Alert Service Bulletin 

(ASB) No. RB.211–73–AH531, Revision 

1, dated March 7, 2014. The ASB 

describes procedures for modifying 

affected RB211 Trent 500 turbofan 

engines by installing new EEC software 

Version L6.1.2. 

FAA’s Determination and Requirements 

of This AD 

This product has been approved by 

the aviation authority of the United 

Kingdom, and is approved for operation 

in the United States. Pursuant to our 

bilateral agreement with the European 

Community, EASA has notified us of 

the unsafe condition described in the 

MCAI and service information 

referenced above. We are proposing this 

AD because we evaluated all 

information provided by EASA and 

determined the unsafe condition exists 

and is likely to exist or develop on other 

products of the same type design. This 

AD requires removal of EEC software, 

Version L5.6.1 or earlier, and 

installation of a software version eligible 

for installation. 

FAA’s Determination of the Effective 

Date 

No domestic operators use this 

product. 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. 

Costs of Compliance 

We estimate that this AD affects no 

engines installed on airplanes of U.S. 

registry. We also estimate that it will 

take about 1 hour per engine to comply 

with this AD. The average labor rate is 

$85 per hour. Required parts cost is 

about $0 per engine. Based on these 

figures, we estimate the cost of this AD 

on U.S. operators to be $0. 

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. 


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Federal Register / Vol. 79, No. 124 / Friday, June 27, 2014 / Rules and Regulations 36389 

For the reasons discussed above, I 

certify this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

the DOT Regulatory Policies and 

Procedures (44 FR 11034, February 26, 

1979), 

(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. 

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): 

2014–13–03 Rolls-Royce plc: Amendment 

39–17878; Docket No. FAA–2014–0281; 

Directorate Identifier 2014–NE–05–AD. 

(a) Effective Date 

This AD is effective July 14, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to all Rolls-Royce plc (RR) 

RB211 Trent 553–61, 553A2–61, 556–61, 

556A2–61, 556B–61, 556B2–61, 560–61, and 

560A2–61 turbofan engines. 

(d) Reason 

This AD was prompted by the risk of fan 

flutter occurring during ground maintenance 

running, and the risk of intermediatepressure (IP) shaft failure which may result 

in IP turbine overspeed and disk burst. We 

are issuing this AD to address, through an 

update to the electronic engine control (EEC) 

software, multiple risks of uncontained 

engine failure and damage to the airplane. 

(e) Actions and Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(1) After the effective date of this AD, 

within 3 months or 200 flight cycles, 

whichever occurs first, modify the engine by 

removing EEC software, Version L5.6.1 or 

earlier. 

(2) Install EEC software eligible for 

installation. 

(f) Installation Prohibition 

After modification of an engine as required 

by paragraph (e) of this AD, do not install any 

EEC with a software Version L5.6.1 or earlier 

into any engine. 

(g) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs to this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. 

(h) Related Information 

(1) For more information about this AD, 

contact Mark Riley, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: (781) 238–7758; fax: (781) 238–7199; 

email: mark.riley@faa.gov. 

(2) Refer to MCAI European Aviation 

Safety Agency AD 2014–0086, dated April 

11, 2014, for more information. You may 

examine the MCAI in the AD docket on the 

Internet at http://www.regulations.gov by 

searching for and locating it in Docket No. 

FAA–2014–0281. 

(3) RR Alert Service Bulletin No. RB.211– 

73–AH531, Revision 1, dated March 7, 2014, 

which is not incorporated by reference in this 

AD, can be obtained from RR using the 

contact information in paragraph (h)(4) of 

this AD. 

(4) Rolls-Royce plc, Corporate 

Communications, P.O. Box 31, Derby, 

England, DE248BJ; phone: 011–44–1332– 

242424; fax: 011–44–1332–249936; email: 

http://www.rolls-royce.com/contact/civil_

team.jsp; Internet: https://

www.aeromanager.com. 

(5) You may view this service information 

at the FAA, Engine & Propeller Directorate, 

12 New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(i) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

June 13, 2014. 

Ann C. Mollica, 

Acting Assistant Directorate Manager, Engine 

& Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2014–14807 Filed 6–26–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 95 

[Docket No. 30967; Amdt. No. 514] 

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 Date: 0901 UTC, July 

24, 2014. 

FOR FURTHER INFORMATION CONTACT: 

Harry Hodges, 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 

25082, Oklahoma City, OK 73125), 

telephone: (405) 954–4164. 

SUPPLEMENTARY INFORMATION: This 

amendment to part 95 of the Federal 

Aviation Regulations (14 CFR part 95) 

amends, suspends, or revokes IFR 

altitudes governing the operation of all 

aircraft in flight over a specified route 

or any portion of that route, as well as 

the changeover points (COPs) for 

Federal airways, jet routes, or direct 

routes as prescribed in part 95. 

The Rule 

The specified IFR altitudes, when 

used in conjunction with the prescribed 

changeover points for those routes, 

ensure navigation aid coverage that is 

adequate for safe flight operations and 

free of frequency interference. The 

reasons and circumstances that create 

the need for this amendment involve 

matters of flight safety and operational 

efficiency in the National Airspace 

System, are related to published 

aeronautical charts that are essential to 

the user, and provide for the safe and 

efficient use of the navigable airspace. 

In addition, those various reasons or 


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