64504 Federal Register / Vol. 79, No. 210 / Thursday, October 30, 2014 / Rules and Regulations 

1 12 CFR Part 267. 

2Public Law 111–203, 124 Stat. 1376 (Jul. 21, 

2010). 

3Section 1085 of the Dodd-Frank Act. 

4Section 1014 of the Dodd-Frank Act. 

5 5 U.S.C. 553(b)(A). 

officers, and establishing procedures for 

conducting CAC meetings.1

The Dodd-Frank Wall Street Reform 

and Consumer Protection Act (DoddFrank Act) 2 transferred rulemaking 

authority for most consumer financial 

protection laws from the Board and 

other agencies to the Consumer 

Financial Protection Bureau (CFPB). 

The Dodd-Frank Act also repealed the 

requirement in section 703 of ECOA that 

the Board establish and operate the 

CAC3 and instead required the CFPB to 

establish a Consumer Advisory Board 

that would provide the CFPB with the 

type advice that the CAC formerly 

provided to the Board.4 Consequently, 

the Board no longer maintains a CAC, 

and the Rules of Organization and 

Procedure of the Consumer Advisory 

Council are no longer necessary. 

Accordingly, the Board is repealing its 

Rules of Organization and Procedure of 

the Consumer Advisory Council. 

II. Administrative Procedure Act 

This rule is not subject to the 

provisions of the Administrative 

Procedure Act (APA), 5 U.S.C. 553, 

requiring notice, public participation, 

and a deferred effective date. The APA’s 

notice and comment procedures do not 

apply to rules of agency organization, 

procedure, or practice, such as the rules 

adopted by the Board for the operation 

of the CAC.5

List of Subjects in 12 CFR Part 267 

Consumer protection, Credit, 

Organization and functions 

(Government agencies). 

Authority and Issuance 

■ For the reasons set forth in the 

preamble and under the authority of 

Public Law 111–203, section 1085, the 

Board removes and reserves 12 CFR part 

267. 

PART 267—[REMOVED AND 

RESERVED] 

By order of the Board of Governors of the 

Federal Reserve System, October 23, 2014. 

Robert deV. Frierson, 

Secretary of the Board. 

[FR Doc. 2014–25661 Filed 10–29–14; 8:45 am] 

BILLING CODE P 

FEDERAL DEPOSIT INSURANCE 

CORPORATION 

12 CFR Parts 335 and 390 

RIN 3064–AE07 

Transferred OTS Regulations 

Regarding Securities of State Savings 

Associations 

AGENCY: Federal Deposit Insurance 

Corporation. 

ACTION: Final rule; correction. 

SUMMARY: The FDIC is correcting a final 

rule that appeared in the Federal 

Register of October 24, 2014 (79 FR 

63498), regarding Transferred OTS 

Regulations Regarding Securities of 

State Savings Associations. This 

publication corrects a typographical 

error in the Paperwork Reduction Act 

statement in the Regulatory Analysis 

and Procedure section. 

DATES: The correction is effective 

November 24, 2014. 

FOR FURTHER INFORMATION CONTACT: 

Dennis Chapman, Senior Staff 

Accountant, Division of Risk 

Management Supervision, 202–898– 

8922 or dchapman@fdic.gov; Maureen 

Loviglio, Senior Staff Accountant, 

Division of Risk Management 

Supervision, 202–898–6777 or 

mloviglio@fdic.gov; Mark G. Flanigan, 

Supervisory Counsel, Legal Division 

202–898–7426 or mflanigan@fdic.gov; 

or Grace Pyun, Senior Attorney, Legal 

Division 202–898–3609 or gpyun@

fdic.gov. 

SUPPLEMENTARY INFORMATION: In FR Doc. 

2014–25336, appearing on page 63499 

in the Federal Register of October 24, 

2014, in the third column under section 

V. A., the paragraphs ‘‘Title’’ through 

‘‘Total Estimated Annual Burden’’ are 

revised to read as follows: 

Title: Securities of State Nonmember 

Banks and State Savings Associations. 

OMB Number: 3064–0030. 

Form Numbers: 6800/03, 6800/04, 

6800/05, Form 8–A, Form 8–C, Form 8– 

K, Form 10, Form 10–C, Form 10–K, 

Form 10–Q, Form 12b–25, Form 15, 

Form 25, Schedule 13D, Schedule 13E– 

3, Schedule 13G, Schedule 14A, 

Schedule 14C, Schedule 14D–1 

(Schedule TO). 

Affected Public: Generally, any issuer 

of securities, reporting company, or 

shareholder of an issuer registered 

under the Securities Exchange Act of 

1934 with respect to securities 

registered under 12 CFR part 335. 

Estimated Number of Respondents: 

Form 6800/03—58; Form 6800/04—297; 

Form 6800/05—69; Form 8–A—2; Form 

8–C—2; Form 8–K—21; Form 10—2; 

Form 10–C—1; Form 10–K—21; Form 

10–Q—21, Form 12b–25—6; Form 15— 

2; Form 25—2; Schedule 13D—2; 

Schedule 13E–3—2; Schedule 13G—2; 

Schedule 14A—21; Schedule 14C—2; 

Schedule 14D–1 (Schedule TO)—2. 

Estimated Time per Response: Form 

6800/03—1 hour; Form 6800/04—30 

minutes; Form 6800/05—1 hour; Form 

8–A—3 hours; Form 8–C—2 hours; 

Form 8–K—2 hours; Form 10—215 

hours; Form 10–C—1 hour; Form 10– 

K—140 hours; Form 10–Q—100 hours; 

Form 12b–25—3 hours; Form 15—1 

hours; Form 25—1 hours; Schedule 

13D—3 hours; Schedule 13E–3—3 

hours; Schedule 13G—3 hours; 

Schedule 14A—40 hours; Schedule 

14C—40 hours; Schedule 14D–1 

(Schedule TO)—5 hours. 

Frequency of Response: Forms 6800/ 

05 and 10–K and Schedule 14A are filed 

annually. Form 10–Q is filed quarterly. 

All other forms are filed based on each 

event or transaction. 

Existing annual burden: 717 hours. 

New estimated additional annual 

burden: 10,829 hours. 

Total Estimated Annual Burden: 

11,546 hours. 

Dated at Washington, DC, this 27th day of 

October, 2014. 

Federal Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. 2014–25842 Filed 10–29–14; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0705; Directorate 

Identifier 2014–NE–13–AD; Amendment 39– 

18006; AD 2014–22–02] 

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) Trent 1000–A, 

1000–C, 1000–D, 1000–E, 1000–G, and 

1000–H turbofan engines. This AD 

requires removing engine electronic 

controller (EEC) software earlier than 

standard MB6.15 and replacing with a 

software standard eligible for 

installation. This AD was prompted by 

a finding that an intermediate pressure 


tkelley on DSK3SPTVN1PROD with RULES
Federal Register / Vol. 79, No. 210 / Thursday, October 30, 2014 / Rules and Regulations 64505 

(IP) shaft failure may not be detected by 

EEC software earlier than standard 

MB6.15. We are issuing this AD to 

detect IP shaft failure and prevent IP 

compressor turbine burst, uncontained 

engine failure, and damage to the 

airplane. 

DATES: This AD becomes effective 

November 14, 2014. 

We must receive comments on this 

AD by December 15, 2014. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• 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, DE24 8BJ; 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– 

0705; 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), regulatory evaluation, any 

comments received, and other 

information. The 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: 

Kenneth Steeves, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7765; fax: 781–238– 

7199; email: kenneth.steeves@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–2014–0705; 

Directorate Identifier 2014–NE–13–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– 

0192, dated September 1, 2014 (referred 

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

an unsafe condition for the specified 

products. The MCAI states: 

An investigation carried out by RR has 

identified the risk of Intermediate Pressure 

(IP) shaft failure that may not be detected and 

accommodated by the engine control system. 

An IP shaft failure that is not detected may 

result in IP turbine overspeed. 

This condition, if not corrected, could lead 

to IP turbine burst and consequent release of 

high energy debris, possibly resulting 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– 

0705. 

Relevant Service Information 

RR has issued Alert Service Bulletin 

(ASB) No. TRENT 1000 73–AH914, 

dated July 23, 2014. The ASB describes 

procedures for removing software earlier 

than standard MB6.15, and installing a 

software standard eligible for 

installation. 

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 issuing 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 removing EEC software 

earlier than standard MB6.15, and 

replacing with a software standard 

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 $200 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 


tkelley on DSK3SPTVN1PROD with RULES
64506 Federal Register / Vol. 79, No. 210 / Thursday, October 30, 2014 / Rules and Regulations 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

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

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): 

2014–22–02 Rolls-Royce plc: Amendment 

39–18006; Docket No. FAA–2014–0705; 

Directorate Identifier 2014–NE–13–AD. 

(a) Effective Date 

This AD is effective November 14, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

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

Trent 1000–A, 1000–C, 1000–D, 1000–E, 

1000–G, and 1000–H turbofan engines. 

(d) Reason 

This AD was prompted by a finding that 

an intermediate pressure (IP) shaft failure 

may not be detected by engine electronic 

controller (EEC) software earlier than 

standard MB6.15. We are issuing this AD to 

detect IP shaft failure and prevent IP 

compressor turbine burst, 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) Within 30 days or 180 flight cycles after 

the effective date of this AD, whichever 

occurs first, remove from the engine any EEC 

software standard earlier than software 

standard MB6.15. 

(2) Install EEC software eligible for 

installation. 

(f) Installation Prohibition 

After the effective date of this AD, do not 

install any EEC containing a software 

standard earlier than software standard of 

MB6.15, 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. You may email your 

request to: ANE-AD-AMOC@faa.gov. 

(h) Related Information 

(1) For more information about this AD, 

contact Kenneth Steeves, Aerospace 

Engineer, Engine Certification Office, FAA, 

Engine & Propeller Directorate, 12 New 

England Executive Park, Burlington, MA 

01803; phone: 781–238–7765; fax: 781–238– 

7199; email: kenneth.steeves@faa.gov. 

(2) Refer to MCAI European Aviation 

Safety Agency AD 2014–0192, dated 

September 1, 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–2014–0705. 

(3) RR Alert Service Bulletin No. TRENT 

1000 73–AH914, dated July 23, 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) 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.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 

October 17, 2014. 

Colleen M. D’Alessandro, 

Assistant Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2014–25739 Filed 10–29–14; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF DEFENSE 

Office of the Secretary 

[Docket ID: DoD–2014–OS–0091] 

32 CFR Part 311 

Privacy Act; Implementation 

AGENCY: Office of the Secretary, DoD. 

ACTION: Direct final rule with request for 

comments. 

SUMMARY: The Office of the Secretary of 

Defense is exempting those records 

contained in DWHS E05, entitled 

‘‘Mandatory Declassification Review 

Files,’’ pertaining to requests and/or 

appeals from individuals for the 

mandatory review of classified 

documents. The exemption will allow 

DoD to provide protection against 

releasing any documents that remain 

properly classified and not available for 

release. 

DATES: The rule is effective on January 

8, 2015 unless adverse comments are 

received by December 29, 2014. If 

adverse comment is received, the 

Department of Defense will publish a 

timely withdrawal of the rule in the 

Federal Register. 

ADDRESSES: You may submit comments, 

identified by docket number and title, 

by any of the following methods: 

• Federal Rulemaking Portal: http://

www.regulations.gov. Follow the 

instructions for submitting comments. 

• Mail: Federal Docket Management 

System Office, 4800 Mark Center Drive, 

Suite 02G09, Alexandria, VA 22350– 

3100. 

Instructions: All submissions received 

must include the agency name and 

docket number for this Federal Register 

document. The general policy for 

comments and other submissions from 

members of the public is to make these 

submissions available for public 

viewing on the Internet at http://

www.regulations.gov as they are 

received without change, including any 

personal identifiers or contact 

information. 

FOR FURTHER INFORMATION CONTACT: Ms. 

Cindy Allard at (571) 372–0461. 

SUPPLEMENTARY INFORMATION: This 

direct final rule makes nonsubstantive 

changes to the Office of the Secretary 

Privacy Program rules. These changes 

will allow the Department to add an 

exemption rule to the Office of the 

Secretary of Defense Privacy Program 

rules that will exempt applicable 

Department records and/or material 

from certain portions of the Privacy Act. 

This is being published as a direct final 

rule as the Department of Defense does 


tkelley on DSK3SPTVN1PROD with RULES