9380 Federal Register / Vol. 80, No. 35 / Monday, February 23, 2015 / Rules and Regulations 

or national of a country not listed in the 

Appendix to this part has been granted 

access to information subject to § 810.2 

in accordance with Nuclear Regulatory 

Commission access requirements. The 

report should contain the information 

required in § 810.11(b). 

(h) All reports should be sent to: U.S. 

Department of Energy, National Nuclear 

Security Administration, Washington, 

DC 20585, Attention: Senior Policy 

Advisor, Office of Nonproliferation and 

Arms Control (NPAC). 

§ 810.13 Additional information. 

DOE may at any time require a person 

engaging in any generally or specifically 

authorized activity to submit additional 

information. 

§ 810.14 Special provisions regarding 

Ukraine. 

(a) Pre-activity notification 

requirements. Any person beginning 

any generally authorized activity 

involving Ukraine shall provide to DOE 

at least ten days prior to beginning that 

activity a report containing the 

following information: 

(1) The name, address, and 

citizenship of the person submitting the 

notification; 

(2) The name, address, and 

citizenship of the person for which the 

activity is to be performed; 

(3) A description of the activity, the 

date it is proposed to begin, its location, 

status, and anticipated date of 

completion; and 

(4) A written assurance that the 

person that is to perform the activity has 

an agreement with the recipient that any 

subsequent transfer of technology or 

information transferred under general 

authorization will not be transferred to 

a country that is not listed in the 

Appendix to this part without the prior 

written approval of DOE. 

(b) Post-activity reporting 

requirements. Every person completing 

a generally authorized activity in 

Ukraine shall provide to DOE within ten 

days following the original transfer of 

technology or information written 

confirmation that such transfer was 

completed in accordance with the 

description of the activity provided as 

required by paragraph (a) of this section. 

§ 810.15 Violations. 

(a) The Atomic Energy Act provides 

that: 

(1) In accordance with section 232 of 

the AEA, permanent or temporary 

injunctions, restraining or other orders 

may be granted to prevent a violation of 

any provision of the Atomic Energy Act 

or any regulation or order issued 

thereunder. 

(2) In accordance with section 222 of 

the AEA, whoever willfully violates, 

attempts to violate, or conspires to 

violate any provision of section 57 of 

the Atomic Energy Act may be fined up 

to $10,000 or imprisoned up to 10 years, 

or both. If the offense is committed with 

intent to injure the United States or to 

aid any foreign nation, the penalty 

could be up to life imprisonment or a 

$20,000 fine, or both. 

(b) In accordance with Title 18 of the 

United States Code, section 1001, 

whoever knowingly and willfully 

falsifies, conceals, or covers up a 

material fact or makes or uses false, 

fictitious or fraudulent statements or 

representations shall be fined under that 

title or imprisoned up to five or eight 

years depending on the crime, or both. 

§ 810.16 Effective date and savings clause. 

(a) The regulations in this part are 

effective March 25, 2015. 

(b) Except for actions that may be 

taken by DOE pursuant to § 810.10, the 

regulations in this part do not affect the 

validity or terms of any specific 

authorizations granted under 

regulations in effect before March 25, 

2015 or generally authorized activities 

under those regulations for which the 

contracts, purchase orders, or licensing 

arrangements were already in effect. 

Persons engaging in activities that were 

generally authorized under regulations 

in effect before March 25, 2015, but that 

require specific authorization under the 

regulations in this part, must request 

specific authorization by August 24, 

2015 and may continue their activities 

until DOE acts on the request. 

Appendix A to Part 810—Generally 

Authorized Destinations 

Argentina 

Australia 

Austria 

Belgium 

Brazil 

Bulgaria 

Canada 

Chile (For all activities related to INFCIRC/ 

834 only) 

Colombia 

Croatia 

Cyprus 

Czech Republic 

Denmark 

Egypt 

Estonia 

Finland 

France 

Germany 

Greece 

Hungary 

Indonesia 

International Atomic Energy Agency 

Ireland 

Italy 

Japan 

Kazakhstan 

Korea, Republic of 

Latvia 

Lithuania 

Luxembourg 

Malta 

Mexico (For all activities related to INFCIRC/ 

203 Parts 1 and 2 and INFCIRC/825 only) 

Morocco 

Netherlands 

Norway 

Poland 

Portugal 

Romania 

Slovakia 

Slovenia 

South Africa 

Spain 

Sweden 

Switzerland 

Taiwan 

Turkey 

Ukraine (Refer to § 810.14 for specific 

information and requirements) 

United Arab Emirates 

United Kingdom 

Vietnam 

[FR Doc. 2015–03479 Filed 2–20–15; 8:45 am] 

BILLING CODE 6450–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–0561; Directorate 

Identifier 2014–NE–12–AD; Amendment 39– 

18105; AD 2015–04–03] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc Turbofan Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Rolls-Royce plc (RR) RB211 Trent 768– 

60, 772–60, and 772B–60 turbofan 

engines. This AD requires inspection of 

the oil feed tube sealing sleeve and 

removal of those oil feed tube sealing 

sleeves that are affected by this AD. This 

AD was prompted by fractures of the 

high-pressure/intermediate-pressure 

(HP/IP) turbine support internal oil feed 

tube. We are issuing this AD to prevent 

failure of the HP/IP turbine support 

internal oil feed tube, which could 

result in uncontained engine failure and 

damage to the airplane. 

DATES: This AD becomes effective 

March 30, 2015. 

ADDRESSES: See the FOR FURTHER

INFORMATION CONTACT section. 


emcdonald on DSK67QTVN1PROD with RULES
Federal Register / Vol. 80, No. 35 / Monday, February 23, 2015 / Rules and Regulations 9381 

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– 

0561; 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 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 

Document Management Facility, U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Wego Wang, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7134; fax: 781–238– 

7199; email: wego.wang@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to the specified products. The 

NPRM was published in the Federal 

Register on September 18, 2014 (79 FR 

56025). The NPRM proposed to correct 

an unsafe condition for the specified 

products. The MCAI states: 

There have been nine occurrences of high oil 

consumption, caused by fracture of the High/ 

Intermediate Pressure (HP/IP) turbine 

support internal oil feed tube Part Number 

(P/N) FW45909. 

The oil feed tube threaded end adaptor and 

sealing sleeve P/N FW15003 are designed to 

form a sliding joint which, if restrained, can 

compress the oil feed tube during thermal 

contraction of the turbine casing at the end 

of the flight cycle. On each subsequent flight, 

the thermal growth and contraction of the 

turbine casing relative to the oil tube, during 

the heating and cooling phases of the flight 

cycle, apply a load cycle to the tube, which 

may lead to low cycle fatigue fracture. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (79 

FR 56025, September 18, 2014). 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting this AD 

as proposed. 

Costs of Compliance 

We estimate that this AD affects 69 

engines installed on airplanes of U.S. 

registry. We also estimate that it will 

take about 8.5 hours per engine to 

comply with this AD. The average labor 

rate is $85 per hour. Based on these 

figures, we estimate the cost of this AD 

on U.S. operators to be $49,853. 

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 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): 

2015–04–03 Rolls-Royce plc: Amendment 

39–18105; Docket No. FAA–2014–0561; 

Directorate Identifier 2014–NE–12–AD. 

(a) Effective Date 

This AD becomes effective March 30, 2015. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Rolls-Royce plc (RR) 

RB211 Trent 768–60, 772–60, and 772B–60 

turbofan engines, serial numbers 41693 

through 42309 inclusive, 42313, 42318, 

42319, 42320, 42328, and 42330 with highpressure/intermediate-pressure (HP/IP) 

turbine support internal oil feed tube sealing 

sleeve, part number (P/N) FW15003, 

installed, that is marked with the prefix ‘‘B/ 

N’’ followed by a six digit batch number and 

does not contain the marking 102013, 112013 

or 102013L. 

(d) Reason 

This AD was prompted by fractures of the 

HP/IP turbine support internal oil feed tube. 

We are issuing this AD to prevent failure of 

the HP/IP turbine support internal oil feed 

tube, which could result in 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 6 months after the effective date 

of this AD, perform on-wing or in-shop 

inspection for, and remove from service, any 

affected HP/IP turbine support internal oil 

feed tube sealing sleeve. 

(2) Remove from service any HP/IP turbine 

support internal oil feed tube sealing sleeve 

on which markings cannot be sufficiently 

identified to determine whether said sealing 

sleeve is part of the affected population. 

(3) From the effective date of this AD, you 

may install on engines HP/IP turbine support 

internal oil feed tube sealing sleeves, P/N 

FW15003, that are marked with the prefix 

‘‘B/N’’ followed by a six digit batch number, 

provided that the part is marked with 

102013, 112013, or 102013L. 


emcdonald on DSK67QTVN1PROD with RULES
9382 Federal Register / Vol. 80, No. 35 / Monday, February 23, 2015 / Rules and Regulations 

(f) 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. 

(g) Related Information 

(1) For more information about this AD, 

contact Wego Wang, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7134; fax: 781–238–7199; 

email: wego.wang@faa.gov. 

(2) Refer to MCAI European Aviation 

Safety Agency AD 2014–0168, dated July 16, 

2014, for more information. You may 

examine the MCAI in the AD docket on the 

Internet at http://www.regulations.gov/#!

docketDetail;D=FAA-2014-0561. 

(h) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

February 11, 2015. 

Colleen M. D’Alessandro, 

Assistant Directorate Manager, Engine & 

Propeller Directorate, Aircraft Certification 

Service. 

[FR Doc. 2015–03533 Filed 2–20–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2014–1001; Directorate 

Identifier 2014–CE–034–AD; Amendment 

39–18003; AD 2015–04–01] 

RIN 2120–AA64 

Airworthiness Directives; Short 

Brothers & Harland Ltd. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for Short 

Brothers & Harland Ltd. Model SC–7 

Series 3 airplanes. This AD results from 

mandatory continuing airworthiness 

information (MCAI) issued by an 

aviation authority of another country to 

identify and correct an unsafe condition 

on an aviation product. The MCAI 

describes the unsafe condition as fatigue 

cracking, which could lead to structural 

failure of the nose landing gear (NLG). 

We are issuing this AD to require 

actions to address the unsafe condition 

on these products. 

DATES: This AD is effective March 30, 

2015. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in the AD 

as of March 30, 2015. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2014– 

1001; or in person at Document 

Management Facility, U.S. Department 

of Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC 20590. 

For service information identified in 

this AD, contact Short Brothers & 

Harland Ltd. service information 

identified in this proposed AD, contact 

Airworthiness, Short Brothers PLC, P.O. 

Box 241, Airport Road, Belfast, BT3 9DZ 

Northern Ireland, United Kingdom; 

phone: +44–2890–462469, fax: 44– 

2890–733647, email: michael.

mulholland@aero.bombardier.com, 

internet: None; and for SAFRAN 

Messier-Buggatti-Dowty service 

information contact Messier-Dowty 

Limited, Cheltenham Road, Gloucester 

GL2 9QH, ENGLAND; phone: 

+44(0)1452 712424; fax: +44(0)1452 

713821; email: americacsc@

safranmbd.com, Internet: http://

www.safranmbd.com. You may view 

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. You can also find 

this service information on the Internet 

at http://www.regulations.gov by 

searching for and locating Docket No. 

FAA–2014–1001. It is also available on 

the Internet at http://www.regulations.

gov by searching for and locating Docket 

No. FAA–2014–1001. 

FOR FURTHER INFORMATION CONTACT: 

Doug Rudolph, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 

Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329– 

4059; fax: (816) 329–4090; email: 

doug.rudolph@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to adding an AD that would 

apply to Short Brothers & Harland Ltd 

Model SC–7 Series 3 airplane. The 

NPRM was published in the Federal 

Register on December 8, 2014 (79 FR 

72562). The NPRM proposed to correct 

an unsafe condition for the specified 

products and was based on mandatory 

continuing airworthiness information 

(MCAI) originated by an aviation 

authority of another country. The MCAI 

states: 

A fracture of the nose landing gear (NLG) 

sliding tube was reported. The subsequent 

investigation determined fatigue cracking as 

possible cause of the failure. 

This condition, if not detected and 

corrected, could lead to structural failure of 

the NLG, possibly resulting in loss of control 

of the aeroplane during take-off or landing. 

To address this unsafe condition, the 

Messier-Dowty Ltd, the NLG manufacturer, 

issued Service Bulletin (SB) 32–17M to 

provide inspection instructions. 

Consequently Short Brothers PLC issued SB 

32–74 which references Messier-Dowty Ltd 

SB 32–17M. 

For the reasons described above, this AD 

requires one-time visual and fluorescent 

penetrant inspections and, depending on 

findings, accomplishment of applicable 

corrective action(s). 

The MCAI requires you report the 

findings to Short Brothers PLC to obtain 

FAA-approved repair instructions and 

accomplish the repair accordingly. The 

MCAI can be found in the AD docket on 

the Internet at: http://

www.regulations.gov/

#!documentDetail;D=FAA-2014-1001- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (79 

FR 72562, December 8, 2014) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (79 FR 

72562, December 8, 2014) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (79 FR 72562, 

December 8, 2014). 

Relative Service Information Under 1 

CFR Part 51 

We reviewed Short Brothers & 

Harland Ltd. Shorts Service Bulletin 

Number 32–74, dated November 1, 

2014; and SAFRAN Messier-BuggattiDowty Service Bulletin No. 32–17M, 

dated November 1, 2014. The Shorts 

Service Bulletin Number 32–74, dated 

November 1, 2014, and SAFRAN 

Messier-Buggatti-Dowty Service Bulletin 

No. 32–17M, dated November 1, 2014, 

describe procedures for a visual 

inspection and a fluorescent penetrant 

inspection (FPI) for cracking of the NLG 


emcdonald on DSK67QTVN1PROD with RULES