Federal Register / Vol. 76, No. 124 / Tuesday, June 28, 2011 / Rules and Regulations 37629 

(ii) Its tier 1 risk-based capital ratio as 

calculated under 12 CFR part 208, appendix 

A, as adjusted to include certain debt or 

equity instruments issued before May 19, 

2010 as described in section 171(b)(4)(B) of 

the Dodd-Frank Act. 

(b) Each bank holding company must hold 

capital commensurate with the level and 

nature of all risks to which the bank holding 

company is exposed. 

(c) When a bank holding company subject 

to 12 CFR part 225, appendix E calculates its 

risk-based capital requirements under this 

appendix, the bank holding company must 

also refer to 12 CFR part 225, appendix E for 

supplemental rules to calculate risk-based 

capital requirements adjusted for market risk. 

* * * * * 

Federal Deposit Insurance Corporation 

12 CFR Chapter III 

Authority for Issuance 

For the reasons stated in the common 

preamble, the Federal Deposit Insurance 

Corporation amends Part 325 of Chapter 

III of Title 12, Code of the Federal 

Regulations as follows: 

PART 325—CAPITAL MAINTENANCE 

■ 9. The authority citation for part 325 

continues to read as follows: 

Authority: 12 U.S.C. 1815(a), 1815(b), 

1816, 1818(a), 1818(b), 1818(c), 1818(t), 

1819(Tenth), 1828(c), 1828(d), 1828(i), 

1828(n), 1828(o), 1831o, 1835, 3907, 3909, 

4808; Pub. L. 102–233, 105 Stat. 1761, 1789, 

1790 (12 U.S.C. 1831n note); Pub. L. 102– 

242, 105 Stat. 2236, as amended by Pub. L. 

103–325, 108 Stat. 2160, 2233 (12 U.S.C. 

1828 note); Pub. L. 102–242, 105 Stat. 2236, 

2386, as amended by Pub. L. 102–550, 106 

Stat. 3672, 4089 (12 U.S.C. 1828 note). 

■ 10. Amend Appendix A to part 325 as 

follows: 

■ a. In section II.C, revise the first 

sentence of the introductory text; 

■ b. In sections II.D, and II.E, 

redesignate footnotes 45 through 50 as 

footnotes 46 through 51. 

■ c. In section II.C, Category 4, add new 

paragraph (d) and a new footnote 45. 

Appendix A to Part 325—Statement of 

Policy on Risk-Based Capital 

* * * * * 

II. * * * 

C. Risk Weights for Balance Sheet Assets (see 

Table II) 

The risk based capital framework contains 

five risk weight categories—0 percent, 20 

percent, 50 percent, 100 percent, and 200 

percent. * * * 

* * * * * 

Category 4—100 Percent Risk Weight. 

* * * 

(d) Subject to the requirements below, a 

bank may assign an asset not included in the 

categories above to the risk weight category 

applicable under the capital guidelines for 

bank holding companies (12 CFR part 225, 

appendix A), provided that all of the 

following conditions apply: 

(1) The bank is not authorized to hold the 

asset under applicable law other than debt 

previously contracted or similar authority; 

and 

(2) The risks associated with the asset are 

substantially similar to the risks of assets that 

are otherwise assigned to a risk weight 

category less than 100 percent under this 

appendix. 

* * * * * 

■ 11. In Appendix D to part 325: 

■ a. Revise section 3 to read as set forth 

below; and 

■ b. Remove section 21(e). 

Appendix D to Part 325—Capital 

Adequacy Guidelines for Banks: 

Internal Ratings-Based and Advanced 

Measurement Approaches 

Part I. General Provisions 

* * * * * 

Section 3. Minimum Risk-Based Capital 

Requirements 

(a)(1) Except as modified by paragraph (c) 

of this section or by section 23 of this 

appendix, each bank must meet a minimum: 

(i) Total risk-based capital ratio of 8.0 

percent; and 

(ii) Tier 1 risk-based capital ratio of 4.0 

percent. 

(2) A bank’s total risk-based capital ratio is 

the lower of: 

(i) Its total qualifying capital to total riskweighted assets, and 

(ii) Its total risk-based capital ratio as 

calculated under appendix A of this part. 

(3) A bank’s tier 1 risk-based capital ratio 

is the lower of: 

(i) Its tier 1 capital to total risk-weighted 

assets, and 

(ii) Its tier 1 risk-based capital ratio as 

calculated under appendix A of this part. 

(b) Each bank must hold capital 

commensurate with the level and nature of 

all risks to which the bank is exposed. 

(c) When a bank subject to appendix C of 

this part calculates its risk-based capital 

requirements under this appendix, the bank 

must also refer to appendix C of this part for 

supplemental rules to calculate risk-based 

capital requirements adjusted for market risk. 

* * * * * 

Dated: June 14, 2011. 

John Walsh, 

Comptroller of the Currency. 

By order of the Board of Governors of the 

Federal Reserve System, June 14, 2011. 

Jennifer J. Johnson, 

Secretary of the Board. 

Dated at Washington, DC, this 14th day of 

June 2011. 

By order of the Board of Directors. Federal 

Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. 2011–15669 Filed 6–27–11; 8:45 am] 

BILLING CODE 4810–33–P; 6210–01–P; 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2011–0126; Directorate 

Identifier 2011–NE–03–AD; Amendment 39– 

16726; AD 2011–13–03] 

RIN 2120–AA64 

Airworthiness Directives: Lycoming 

Engines (Type Certificate Previously 

Held by Textron Lycoming) and 

Teledyne Continental Motors (TCM) 

Turbocharged Reciprocating Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for the 

products listed above. This AD requires 

inspecting certain Lycoming and TCM 

reciprocating engines with certain 

Hartzell Engine Technologies, LLC 

(HET) turbochargers installed, and 

disassembly and cleaning of the 

turbocharger center housing and 

rotating assembly (CHRA) cavities of 

affected turbochargers. This AD was 

prompted by a turbocharger failure due 

to machining debris left in the cavities 

of the CHRA during manufacture. We 

are issuing this AD to prevent seizure of 

the turbocharger turbine, which could 

result in damage to the engine, and 

smoke in the airplane cabin. 

DATES: This AD is effective July 13, 

2011. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of July 13, 2011. 

We must receive comments on this 

AD by August 12, 2011. 

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. 

• 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– 

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37630 Federal Register / Vol. 76, No. 124 / Tuesday, June 28, 2011 / Rules and Regulations 

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 Hartzell Engine 

Technologies, LLC, 2900 Selma 

Highway, Montgomery, AL 36108, 

phone: 334–386–5400; fax: 334–386– 

5450. You may review copies of the 

referenced 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; 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: Gary 

Wechsler, Aerospace Engineer, Atlanta 

Aircraft Certification Office, 1701 

Columbia Avenue, College Park, GA 

30337; phone: 404–474–5575; fax: 404– 

474–5606; e-mail: 

gary.wechsler@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

HET recently informed us of a failure 

of one of their turbochargers installed 

on a TCM TSIO–550–K model 

reciprocating engine. HET identified the 

cause of the failure as machining debris 

left in the CHRA. HET also informed us 

that the debris was a by-product of 

manufacture that had not been removed. 

This debris, if present, could result in 

seizure of the turbocharger turbine, 

which could result in damage to the 

engine, and smoke in the airplane cabin. 

Relevant Service Information 

We reviewed Hartzell Engine 

Technologies, LLC Service Bulletin (SB) 

No. 040, Revision A, dated December 

22, 2010. The SB describes procedures 

for identifying affected turbochargers, 

and performing a one-time disassembly, 

CHRA cleaning, and reassembly. 

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 turbochargers of the 

same type design. 

AD Requirements 

This AD requires accomplishing the 

cleaning specified in the service 

information described previously. 

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 airplanes with no more 

than 50 hours time-in-service on new or 

overhauled affected turbochargers are at 

risk of the unsafe condition described in 

this AD. Therefore, we find that notice 

and opportunity for prior public 

comment are impracticable 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 

was not preceded by notice and an 

opportunity for public comment. 

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 the docket number 

FAA–2011–0126 and Directorate 

Identifier 2011–NE–03–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 

We estimate that about 2,761 

turbochargers are installed on Lycoming 

and TCM engines, installed on airplanes 

of U.S. registry. We also estimate it will 

take about 1 work-hour to inspect each 

turbocharger and that 264 turbochargers 

will fail inspection and require 

corrective action. Each corrective action 

will require 3 work-hours. The average 

labor rate is $85 per work-hour. No 

additional parts are required. Based on 

these figures, we estimate the cost of the 

AD on U.S. operators to be $391,765. 

Our cost estimate is exclusive of 

possible warranty coverage. 

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 

turbochargers 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 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

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Federal Register / Vol. 76, No. 124 / Tuesday, June 28, 2011 / Rules and Regulations 37631 

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): 

2011–13–03 Lycoming Engines (Type 

certificate previously held by Textron 

Lycoming) and Teledyne Continental 

Motors (TCM) Turbocharged 

Reciprocating Engines: Amendment 39– 

16726; Docket No. FAA–2011–0126; 

Directorate Identifier 2011–NE–03–AD. 

Effective Date 

(a) This AD is effective July 13, 2011. 

Affected ADs 

(b) None. 

Applicability 

(c) This AD applies to the Lycoming 

Engines and TCM turbocharged reciprocating 

engines listed in, but not limited to, Table 1 

of this AD, with the following Hartzell 

Engine Technologies, LLC (HET) 

turbocharger models TA3601, TAO401, 

TAO402, TAO411, TAO413, T1879, T18A21, 

T18A44, THO867, and TEO659, installed: 

(1) Newly manufactured turbochargers 

(otherwise known as the –0000 series) before 

serial number H–NJL00003, or rebuilt 

(otherwise known as the –9000 series) before 

serial number H–NJR00002; and 

(2) With less than 50 hours time-in-service 

(TIS) on the effective date of this AD; and 

(3) With a part number listed in Table 2 or 

Table 3 of this AD; and 

(4) With a ‘‘slanted A’’ foundry mark 

located on the center housing and rotating 

assembly (CHRA). 

TABLE 1—ENGINES AFFECTED

TSIO–520–BE. 

TSIO–360–MB, SB. 

TIO–540–AK1A. 

L/TSIO–360–RB. 

TIO–540–AE2A. 

TSIO–360–H. 

O–540–L3C5D. 

TSIO–520–T. 

L/TO–360–E1A6D. 

TIO–540–AG1A. 

TIO–540–AF1A. 

TIO–540–AF1B. 

TIO–540–AH1A. 

TIO–541–E1D4. 

TIO–541–E1C4. 

TIGO–541–E. 

GTSIO–520–F. 

GTSIO–520–K. 

GTSIO–520–D. 

GTSIO–520–H. 

TABLE 2—KAES TURBOCHARGER PART NUMBERS AFFECTED

406990–9004 407540–0003 407540–9003 407800–9003 408590–9012 048610–0001 

465292–0001 465292–9001 465292–0002 465292–9002 465292–0004 465292–9004 

465398–9002 466011–0002 466011–9002 466304–0003 466304–9003 466642–0001 

466642–0002 466642–9002 466642–0005 466642–9005 466642–0006 466642–0007 

408610–9001 465398–0002 466642–9001 N/A N/A N/A 

TABLE 3—ORIGINAL EQUIPMENT TURBOCHARGER PART NUMBERS AFFECTED

637374–1 633274–4 635034–2 642518–4 646677 649151–1 

649151–2 46C19836 46C19839 46C22924 C295001–0301 C295001–0304 

LW–10191 LW–13310 LW–16254 N/A N/A N/A 

(d) This AD does not require action for: 

(1) Turbochargers with more than 50 hours 

TIS on the effective date of this AD. 

(2) Turbochargers with a circled ‘‘JT’’ 

foundry mark on the CHRA. 

(e) This AD does not apply to engines with 

new or overhauled turbochargers installed on 

or before September 2001. 

Unsafe Condition 

(f) This AD was prompted by a 

turbocharger failure due to machining debris 

that was not cleaned from the cavities of the 

center housing and rotating assembly 

(CHRA), during manufacture. We are issuing 

this AD to prevent seizure of the turbocharger 

turbine, which could result in damage to the 

engine, and smoke in the airplane cabin. 

Compliance 

(g) Unless already done, disassemble, 

clean, and reassemble the turbochargers 

affected by this AD as follows: 

Turbochargers With Between 0 and 10 Hours 

TIS 

(1) For affected turbochargers including 

overhauls, with between 0 and 10 hours TIS 

on the effective date of this AD, before 

further flight, disassemble the turbocharger, 

clean the CHRA center housing cavity, and 

reassemble the turbocharger. 

Turbochargers With More Than 10 Hours 

TIS But Less Than 50 Hours TIS 

(2) For affected turbochargers including 

overhauls, with more than 10 hours TIS but 

less than 50 hours TIS on the effective date 

of this AD, within the next 10 hours TIS, 

disassemble the turbocharger, clean the 

CHRA center housing cavity, and reassemble 

the turbocharger. 

(3) Use paragraphs 1 through 10 of the 

CLEANING CHRA CENTER HOUSING 

section of Hartzell Engine Technologies, LLC 

SB No. 040, Revision A, dated December 22, 

2010, to do the cleaning. 

(4) The reference to Step 16 in paragraph 

10 of the CLEANING CHRA CENTER 

HOUSING section of Hartzell Engine 

Technologies, LLC SB No. 040, Revision A, 

dated December 22, 2010, is incorrect. The 

correct reference is Step 9. 

Turbochargers With More Than 50 Hours 

TIS 

(h) For turbochargers with more than 50 

hours TIS on the effective date of this AD, 

no further action is required. 

Special Flight Permits 

(i) Special flight permits are restricted to 

day Visual Meteorological Conditions flight 

only. 

Alternative Methods of Compliance 

(AMOCs) 

(j) The Manager, Atlanta Aircraft 

Certification Office, has the authority to 

approve AMOCs for this AD if requested 

using the procedures found in 14 CFR 39.19. 

Related Information 

(k) For more information about this AD, 

contact Gary Wechsler, Aerospace Engineer, 

Atlanta Aircraft Certification Office, 1701 

Columbia Avenue, College Park, GA 30337; 

phone: 404–474–5575; fax: 404–474–5606; email: gary.wechsler@faa.gov. 

Material Incorporated by Reference 

(l) You must use Hartzell Engine 

Technologies, LLC Service Bulletin No. 040, 

Revision A, dated December 22, 2010, to 

clean the turbocharger. 

(m) The Director of the Federal Register 

approved the incorporation by reference of 

this service bulletin in accordance with 5 

U.S.C. 552(a) and 1 CFR part 51. 

(n) For service information identified in 

this AD, contact Hartzell Engine 

Technologies, LLC, 2900 Selma Highway, 

Montgomery, AL 36108, phone: 334–386– 

5400; fax: 334–386–5450. 

(o) You may review copies of the service 

information that is incorporated by at the 

FAA, New England Region, 12 New England 

Executive Park, Burlington, MA; or at the 

National Archives and Records 

Administration (NARA). For information on 

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37632 Federal Register / Vol. 76, No. 124 / Tuesday, June 28, 2011 / Rules and Regulations 

the availability of this material at the FAA, 

call 781–238–7125. 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 Burlington, Massachusetts, on 

June 14, 2011. 

Peter A. White, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2011–16087 Filed 6–27–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Industry and Security 

15 CFR Part 744 

[Docket No. 110128065–1135–01] 

RIN 0694–AF12 

Addition of Certain Persons on the 

Entity List: Addition of Persons Acting 

Contrary to the National Security or 

Foreign Policy Interests of the United 

States 

AGENCY: Bureau of Industry and 

Security, Commerce. 

ACTION: Final rule. 

SUMMARY: This rule amends the Export 

Administration Regulations (EAR) by 

adding eight persons to the Entity List 

(Supplement No. 4 to part 744) on the 

basis of section 744.11 of the EAR. The 

persons who are added to the Entity List 

have been determined by the U.S. 

Government to be acting contrary to the 

national security or foreign policy 

interests of the United States. These 

eight persons will be listed under the 

following three destinations on the 

Entity List: France, Iran and the United 

Arab Emirates (U.A.E.). 

The Entity List provides notice to the 

public that certain exports, reexports, 

and transfers (in-country) to parties 

identified on the Entity List require a 

license from the Bureau of Industry and 

Security (BIS) and that availability of 

license exceptions in such transactions 

is limited. 

DATES: This rule is effective June 28, 

2011. 

FOR FURTHER INFORMATION CONTACT: 

Karen Nies-Vogel, Chair, End-User 

Review Committee, Office of the 

Assistant Secretary, Export 

Administration, Bureau of Industry and 

Security, Department of Commerce, 

Phone: (202) 482–5991, Fax: (202) 482– 

3911, E-mail: ERC@bis.doc.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

The Entity List provides notice to the 

public that certain exports, reexports, 

and transfers (in-country) to parties 

identified on the Entity List require a 

license from BIS, and that availability of 

license exceptions in such transactions 

is limited. Persons are placed on the 

Entity List on the basis of criteria set 

forth in certain sections of part 744 

(Control Policy: End-User and End-Use 

Based) of the EAR. 

The End-User Review Committee 

(ERC), composed of representatives of 

the Departments of Commerce (Chair), 

State, Defense, Energy and, where 

appropriate, Treasury, makes all 

decisions regarding additions to, 

removals from, or changes to the Entity 

List. The ERC makes all decisions to add 

an entry to the Entity List by majority 

vote, and all decisions to remove or 

modify an entry by unanimous vote. 

ERC Entity List Decisions 

The ERC made a determination to add 

eight persons to the Entity List on the 

basis of section 744.11 (License 

Requirements that Apply to Entities 

Acting Contrary to the National Security 

or Foreign Policy Interests of the United 

States) of the EAR. The eight entries 

added to the Entity List consist of three 

new entries in France, three new entries 

in Iran, and two new entries in the 

U.A.E. 

The ERC reviewed the criteria for 

revising the Entity List (section 

744.11(b) of the EAR) in making the 

determination to add these persons to 

the Entity List. These criteria establish 

how to add to the Entity List those 

entities that, based on specific and 

articulable facts, there is reasonable 

cause to believe have been involved, are 

involved, or pose a significant risk of 

being or becoming involved in activities 

that are contrary to the national security 

or foreign policy interests of the United 

States, and those acting on behalf of 

such entities (section 744.11 of the 

EAR). The persons being added to the 

Entity List under this rule have been 

determined by the ERC to be involved 

in activities that could be contrary to the 

national security or foreign policy 

interests of the United States. An 

illustrative list of such activities can be 

found in paragraphs (b)(1)–(b)(5) of 

section 744.11 of the EAR. 

Pursuant to section 744.11, these eight 

persons are being added based on 

evidence that they have engaged in 

actions that could enhance the military 

capability of Iran, a country designated 

by the U.S. Secretary of State as having 

repeatedly provided support for acts of 

international terrorism. These persons 

are also being added because their 

overall conduct poses a risk of ongoing 

EAR violations. 

Additions to the Entity List 

This rule implements the decision of 

the ERC to add eight persons to the 

Entity List on the basis of section 744.11 

of the EAR. For all eight persons added 

to the Entity List, the ERC specified a 

license requirement for all items subject 

to the EAR and established a license 

application review policy of a 

presumption of denial. A BIS license is 

required to export, reexport or transfer 

(in-country) any item subject to the EAR 

to any of the persons described below, 

including any transaction in which any 

of the listed persons will act as 

purchaser, intermediate consignee, 

ultimate consignee, or end-user of the 

items. This listing of these persons also 

prohibits the use of license exceptions 

(see part 740 of the EAR) for exports, 

reexports and transfers (in-country) of 

items subject to the EAR involving such 

persons. 

Specifically, this rule adds the 

following eight persons to the Entity 

List: 

France 

(1) Aerotechnic France SAS, 8 Rue de 

la Bruyere, 31120 Pinsaguel, France; 

(2) Luc Teuly, 8 Rue de la Bruyere, 

31120 Pinsaguel, France; and 

(3) Philippe Sanchez, 8 Rue de la 

Bruyere, 31120 Pinsaguel, France. 

Iran 

(1) Hassan Seifi, Unit #23, Eighth 

Floor, No. 193 West Sarve Boulevard 

Kaj Square, Saadat Abad, 19987–14434, 

Tehran, Iran; 

(2) Reza Seifi, Unit #23, Eighth Floor, 

No. 193 West Sarve Boulevard Kaj 

Square, Saadat Abad, 19987–14434, 

Tehran, Iran; and 

(3) Sabanican Company, (a.k.a., 

Sabanican Pad Co.), Unit #23, Eighth 

Floor, No. 193 West Sarve Boulevard 

Kaj Square, Saadat Abad, 19987–14434, 

Tehran, Iran. 

United Arab Emirates 

(1) Aletra General Trading, (a.k.a., 

Erman & Sultan Trading Co.), Sabkha 

Street, Shop No. 8, Dubai, U.A.E.; and 

(2) Syed Amir Ahmed Najfi, Sabkha 

Street, Shop No. 8, Dubai, U.A.E. 

Savings Clause 

Shipments of items removed from 

eligibility for a license exception or 

export or reexport without a license 

(NLR) as a result of this regulatory 

action that were on dock for loading, on 

lighter, laden aboard an exporting or 

reexporting carrier, or en route aboard a 

WReier-Aviles on DSKGBLS3C1PROD with RULES