4184 Federal Register / Vol. 89, No. 15 / Tuesday, January 23, 2024 / Rules and Regulations 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, International Validation 

Branch, FAA, has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. In 

accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of the International Validation 

Branch, send it to the attention of the person 

identified in paragraph (k) of this AD and 

email to ANE-AD-AMOC@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local flight standards district office/ 

certificate holding district office. 

(k) Additional Information 

For more information about this AD, 

contact Barbara Caufield, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; phone: (781) 238– 

7146; email: barbara.caufield@faa.gov. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) European Union Aviation Safety Agency 

(EASA) AD 2023–0021, dated January 23, 

2023. 

(ii) [Reserved] 

(3) For EASA AD 2023–0021, contact 

EASA, Konrad-Adenauer-Ufer 3, 50668 

Cologne, Germany; phone: +49 221 8999 000; 

email: ADs@easa.europa.eu; website: 

easa.europa.eu. You may find this EASA AD 

on the EASA website at ad.easa.europa.eu. 

(4) You may view this service information 

at FAA, Airworthiness Products Section, 

Operational Safety Branch, 1200 District 

Avenue, Burlington, MA 01803. For 

information on the availability of this 

material at the FAA, call (817) 222–5110. 

(5) You may view this material at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

visit www.archives.gov/federal-register/cfr/ 

ibr-locationsoremailfr.inspection@nara.gov. 

Issued on January 17, 2024. 

Victor Wicklund, 

Deputy Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2024–01218 Filed 1–22–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2023–1647; Project 

Identifier AD–2023–00487–E; Amendment 

39–22650; AD 2023–26–07] 

RIN 2120–AA64 

Airworthiness Directives; General 

Electric Company Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: The FAA is adopting a new 

airworthiness directive (AD) for certain 

General Electric Company (GE) Model 

GE90–90B, GE90–94B, GE90–110B1, 

and GE90–115B engines. This AD was 

prompted by a manufacturer 

investigation that revealed certain highpressure turbine (HPT) stage 1 disks, 

HPT stage 2 disks, forward HPT rotor 

seals, interstage HPT seals, and stages 

7–9 compressor rotor spools were 

manufactured from powder metal 

material suspected to contain iron 

inclusion. This AD requires replacement 

of affected HPT stage 1 disks, HPT stage 

2 disks, forward HPT rotor seals, 

interstage HPT seals, and stages 7–9 

compressor rotor spools. The FAA is 

issuing this AD to address the unsafe 

condition on these products. 

DATES: This AD is effective February 27, 

2024. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of February 27, 2024. 

ADDRESSES: 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2023–1647; or in person at 

Docket Operations between 9 a.m. and 

5 p.m., Monday through Friday, except 

Federal holidays. The AD docket 

contains this final rule, any comments 

received, and other information. The 

address for Docket Operations is U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE, Washington, DC 

20590. 

Material Incorporated by Reference: 

• For service information identified 

in this final rule, contact General 

Electric Company, 1 Neumann Way, 

Cincinnati, OH 45215; phone: (513) 

552–3272; email: aviation.fleetsupport@

ge.com; website: ge.com. 

• You may view this service 

information at the FAA, Airworthiness 

Products Section, Operational Safety 

Branch, 1200 District Avenue, 

Burlington, MA 01803. For information 

on the availability of this material at the 

FAA, call (817) 222–5110. It is also 

available at regulations.gov under 

Docket No. FAA–2023–1647. 

FOR FURTHER INFORMATION CONTACT: 

Alexei Marqueen, Aviation Safety 

Engineer, FAA, 2200 South 216th Street, 

Des Moines, WA 98198; phone: (781) 

238–7178; email: Alexei.T.Marqueen@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

The FAA issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain GE Model GE90–90B, 

GE90–94B, GE90–110B1, and GE90– 

115B engines. The NPRM published in 

the Federal Register on September 5, 

2023 (88 FR 60603). The NPRM was 

prompted by the manufacturer’s 

detection of iron inclusion in a turbine 

disk manufactured from the same 

powder metal material used to 

manufacture certain HPT stage 1 disks, 

HPT stage 2 disks, forward HPT rotor 

seals, interstage HPT seals, and stages 

7–9 compressor rotor spools for GE90– 

90B, GE90–94B, GE90–110B1, and 

GE90–115B engines. Further 

investigation by the manufacturer 

determined that the iron inclusion is 

attributed to deficiencies in the 

manufacturing process and may cause 

reduced material properties and a lower 

fatigue life capability, which may result 

in premature fracture and subsequent 

uncontained failure. The FAA was also 

informed that GE communicated with 

affected operators having affected HPT 

stage 1 and stage 2 disks identified in 

Table 1 to Paragraph (c) of this AD 

regarding the corrective action for this 

unsafe condition. As a result, affected 

operators are already aware of the 

corrective action and have already 

performed the actions required by this 

AD. Therefore, the FAA has determined 

that the compliance time to replace 

these affected HPT stage 1 and stage 2 

disks before further flight is appropriate. 

In the NPRM, the FAA proposed to 

require replacement of certain HPT 

stage 1 disks, HPT stage 2 disks, forward 

HPT rotor seals, interstage HPT seals, 

and stages 7–9 compressor rotor spools 

with parts eligible for installation. The 

FAA is issuing this AD to address the 

unsafe condition on these products. 

Discussion of Final Airworthiness 

Directive 

Comments 

The FAA received comments from 

five commenters. Commenters included 


khammond on DSKJM1Z7X2PROD with RULES
Federal Register / Vol. 89, No. 15 / Tuesday, January 23, 2024 / Rules and Regulations 4185 

The Boeing Company (Boeing), Federal 

Express (FedEx), GE, United Airlines, 

and an individual commenter. Boeing, 

United Airlines, and the individual 

commenter supported the NPRM 

without change. FedEx and GE 

requested changes to the proposed AD. 

The following presents the comments 

received on the NPRM and the FAA’s 

response to each comment. 

Request To Reference Additional 

Service Information 

FedEx and GE requested that the FAA 

add the following service information to 

the NPRM in a section designated as 

Other Related Service Information: GE 

GE90–100 Service Bulletin (SB) 72– 

0904 R00, dated May 25, 2022; GE 

GE90–100 SB 72–0911 R01, dated 

September 21, 2022; and GE GE90 SB 

72–1223, dated January 25, 2023. FedEx 

and GE both noted that Table 1 to 

Paragraph (c) of the proposed AD listed 

affected components that were partially 

copied from those GE SBs, and not 

including mention of those GE SBs 

could cause confusion for operators, 

even though additional GE SBs would 

not be incorporated by reference. 

The FAA agrees and for the ease of 

the reader, instead of including these 

additional GE SBs in a section identified 

as Other Related Service Information in 

the preamble, has added Note 1 to 

paragraph (c) of this AD to include the 

three additional GE SBs identified by 

the commenters and to clarify that the 

affected parts can also be found in these 

additional GE SBs. These additional GE 

SBs will not be incorporated by 

reference in this AD. 

Request To Update Affected Part 

Number 

GE requested that the FAA update 

Table 1 to Paragraph (c) of the proposed 

AD by changing the part number (P/N) 

for an affected HPT stage 1 disk having 

serial number (S/N) GWN10NNW from 

‘‘1865M13G08’’ to ‘‘2445M04G11.’’ GE 

noted that the HPT stage 1 disk with S/ 

N GWN10NNW was repaired and remarked to P/N 2445M04G11. 

The FAA agrees and has updated 

Table 1 to Paragraph (c) of this AD as 

requested by GE. 

Request To Clarify Language in 

Background Section 

GE requested that the FAA add 

language to the Background section of 

the NPRM to clarify that GE 

communicated with affected operators 

having affected HPT stage 1 and stage 2 

disks identified in Table 1 to Paragraph 

(c) of the proposed AD regarding the 

proposed corrective action for the 

identified unsafe condition. GE noted 

that the current language in the NPRM 

does not specify that the affected disks 

are identified in Table 1 to Paragraph (c) 

of the proposed AD, and additional HPT 

stage 2 disks are identified in General 

Electric GE90–100 Service Bulletin 72– 

0914, dated January 25, 2023, which 

could cause a misinterpretation of the 

required actions on HPT stage 2 disks. 

The FAA agrees and has revised the 

language in the Background section of 

this final rule accordingly. 

Conclusion 

The FAA reviewed the relevant data, 

considered any comments received, and 

determined that air safety requires 

adopting this AD as proposed. 

Accordingly, the FAA is issuing this AD 

to address the unsafe condition on these 

products. Except for minor editorial 

changes, and any other changes 

described previously, this AD is 

adopted as proposed in the NPRM. 

None of the changes will increase the 

economic burden on any operator. 

Related Service Information Under 1 

CFR Part 51 

The FAA reviewed GE GE90–100 

Service Bulletin (SB) 72–0914, dated 

January 25, 2023 (GE GE90–100 SB 72– 

0914); which provides the affected part 

and serial numbers of the HPT stage 2 

disks, forward HPT rotor seals, and 

stages 7–9 compressor rotor spools; and 

specifies replacement instructions for 

the HPT stage 2 disks, forward HPT 

rotor seals, and stages 7–9 compressor 

rotor spools. This service information is 

reasonably available because the 

interested parties have access to it 

through their normal course of business 

or by the means identified in the 

ADDRESSES section. 

Interim Action 

The FAA considers this AD to be an 

interim action. This unsafe condition is 

still under investigation by the 

manufacturer and, depending on the 

results of that investigation, the FAA 

may consider further rulemaking action. 

Costs of Compliance 

The FAA estimates that this AD 

affects 9 engines installed on airplanes 

of U.S. registry. The FAA estimates that 

0 engines installed on airplanes of U.S. 

registry require replacement of the 

interstage HPT seal. 

The FAA estimates the following 

costs to comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Replace HPT stage 2 disk .............................. 8 work-hours × $85 per hour = $680 ............. $531,578 $532,258 $532,258 

Replace stages 7–9 compressor rotor spool .. 8 work-hours × $85.per hour = $680 ............. 493,588 494,268 1,977,072 

Replace forward HPT rotor seal ..................... 8 work-hours × $85 per hour = $680 ............. 25,093 25,773 51,546 

Replace interstage HPT seal .......................... 8 work-hours × $85 per hour = $680 ............. 108,256 108,936 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. 

The FAA is 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 

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: 


khammond on DSKJM1Z7X2PROD with RULES
4186 Federal Register / Vol. 89, No. 15 / Tuesday, January 23, 2024 / Rules and Regulations 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Will not affect intrastate aviation 

in Alaska, and 

(3) 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. 

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: 

2023–26–07 General Electric Company: 

Amendment 39–22650; Docket No. 

FAA–2023–1647; Project Identifier AD– 

2023–00487–E. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective February 27, 2024. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to General Electric 

Company (GE) Model GE90–90B and GE90– 

94B engines with interstage HPT seals listed 

in Table 1 to Paragraph (c) of this AD and 

GE90–110B1 and GE90–115B engines with 

an installed high-pressure turbine (HPT) 

stage 1 disk, HPT stage 2 disk, forward HPT 

rotor seal, or stages 7–9 compressor rotor 

spool part number (P/N) and serial number 

(S/N) identified in Table 1 to Paragraph (c) 

of this AD, or identified in Paragraph 4. 

APPENDIX—A, Tables 1, 2, or 3, of GE 

GE90–100 Service Bulletin (SB) 72–0914, 

dated January 25, 2023 (GE90–100 SB 72– 

0914). 

Table 1 to Paragraph (c)—Affected HPT 

Stage 1 and Stage 2 Disks, and Interstage 

HPT Seals 

Note 1 to paragraph (c): Part numbers and 

serial numbers for affected HPT stage 1 disks, 

HPT stage 2 disks, and interstage HPT seals 

are also listed in GE GE90–100 Service 

Bulletin (SB) 72–0904 R00, dated May 25, 

2022; GE GE90–100 SB 72–0911 R01, dated 

September 21, 2022; and GE GE90 SB 72– 

1223, dated January 25, 2023. 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code 7230, Turbine Engine Compressor 

Section; 7250, Turbine Section. 

(e) Unsafe Condition 

This AD was prompted by a manufacturer 

investigation that revealed certain HPT stage 

1 disks, HPT stage 2 disks, forward HPT rotor 

seals, interstage HPT seals, and stages 7–9 

compressor rotor spools were manufactured 

from powder metal material suspected to 

contain iron inclusion. The FAA is issuing 

this AD to prevent premature fracture and 

subsequent uncontained failure. The unsafe 

condition, if not addressed, could result in 

uncontained debris release, damage to the 

engine, and damage to the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Required Actions 

At the applicable times specified in 

paragraphs (g)(1) through (6) of this AD, 

remove each affected HPT stage 1 disk, HPT 

stage 2 disk, forward HPT rotor seal, 

interstage HPT seal, and stages 7–9 

compressor rotor spool from service and 

replace with a part eligible for installation. 

(1) For HPT stage 1 disks, before further 

flight. 

(2) For HPT stage 2 disks with a part 

number and serial number identified in 

Paragraph 4. APPENDIX—A, Table 1 of 

GE90–100 SB 72–0914, at the next piece part 

exposure or before exceeding 3,500 cycles 

since new (CSN), whichever occurs first. 

(3) For HPT stage 2 disks with a part 

number and serial number identified in Table 

1 to paragraph (c) of this AD, before further 

flight. 

(4) For forward HPT rotor seals with a part 

number and serial number identified in 

Paragraph 4. APPENDIX—A, Table 3 of 

GE90–100 SB 72–0914, at the next piece part 

exposure or before exceeding 14,200 CSN, 

whichever occurs first. 

(5) For interstage HPT seals, at the next 

piece part exposure or before exceeding 

12,600 CSN, whichever occurs first. 


khammond on DSKJM1Z7X2PROD with RULESER23JA24.021</GPH>

Part Name PIN SIN 

HPT stage 1 disk 1865M13G08 GWN11657 

GWN117GN 

GWNI0PGW 

GWNI0T0A 

GWNI0T0C 

GWNI0THW 

GWNI0TJ0 

HPT stage 1 disk 2445M04Gll GWNI0NNW 

HPT stage 2 disk 1865M14P04 TMT4RN06 

TMT4RN26 

Interstage HPT seal 2453M60P01 NCU61528 

NCU61686 

NCU56200 

NCU61527 

NCU61687 
Federal Register / Vol. 89, No. 15 / Tuesday, January 23, 2024 / Rules and Regulations 4187 

(6) For stages 7–9 compressor rotor spools, 

at the next piece part exposure or before 

exceeding the cyclic removal thresholds 

identified in Paragraph 4. APPENDIX—A, 

Table 2 of GE90–100 SB 72–0914, whichever 

occurs first. 

(h) Definition 

For the purpose of this AD, a ‘‘part eligible 

for installation’’ is any HPT stage 1 disk, HPT 

stage 2 disk, stages 7–9 compressor rotor 

spool, forward HPT rotor seal, or interstage 

HPT seal with a part number and serial 

number that is not identified in paragraph (c) 

of this AD. 

(i) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, AIR–520 Continued 

Operational Safety Branch, FAA, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 

CFR 39.19. In accordance with 14 CFR 39.19, 

send your request to your principal inspector 

or local Flight Standards District Office, as 

appropriate. If sending information directly 

to the manager of AIR–520 Continued 

Operational Safety Branch, send it to the 

attention of the person identified in 

paragraph (j) of this AD and email to: ANEAD-AMOC@faa.gov. 

(2) Before using any approved AMOC, 

notify your appropriate principal inspector, 

or lacking a principal inspector, the manager 

of the local Flight Standards District Office/ 

certificate holding district office. 

(j) Additional Information 

For more information about this AD, 

contact Alexei Marqueen, Aviation Safety 

Engineer, FAA, 2200 South 216th Street, Des 

Moines, WA 98198; phone: (781) 238–7178; 

email: Alexei.T.Marqueen@faa.gov. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless the AD specifies otherwise. 

(i) General Electric GE90–100 Service 

Bulletin 72–0914, dated January 25, 2023. 

(ii) [Reserved] 

(3) For service information identified in 

this AD, contact General Electric Company, 

1 Neumann Way, Cincinnati, OH 45215; 

phone: (513) 552–3272; email: 

aviation.fleetsupport@ge.com; website: 

ge.com. 

(4) You may view this service information 

at FAA, Airworthiness Products Section, 

Operational Safety Branch, 1200 District 

Avenue, Burlington, MA 01803. For 

information on the availability of this 

material at the FAA, call (817) 222–5110. 

(5) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, 

visit: www.archives.gov/federal-register/cfr/ 

ibr-locations or email: fr.inspection@

nara.gov. 

Issued on January 2, 2024. 

Caitlin Locke, 

Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2024–01166 Filed 1–22–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

Bureau of Industry and Security 

15 CFR Part 744 

[Docket No. 240117–0016] 

RIN 0694–AJ52 

Removals From the Unverified List 

AGENCY: Bureau of Industry and 

Security, Department of Commerce. 

ACTION: Final rule. 

SUMMARY: The Bureau of Industry and 

Security (BIS) is amending the Export 

Administration Regulations (EAR) by 

removing three persons, including one 

under the destination of Canada, one 

under the destination of People’s 

Republic of China (China), and one 

under the destination of the United 

Arab Emirates, from the Unverified List 

(UVL) because BIS was able to verify 

their bona fides. 

DATES: This rule is effective on January 

19, 2024. 

FOR FURTHER INFORMATION CONTACT: 

Kevin J. Kurland, Deputy Assistant 

Secretary for Export Enforcement, 

Phone: (202) 482–4255 or by email at 

UVLRequest@bis.doc.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

The UVL, found in supplement no. 6 

to part 744 of the EAR (15 CFR parts 

730–774), contains the names and 

addresses of foreign persons who are or 

have been parties to a transaction, as 

described in § 748.5 of the EAR, 

involving the export, reexport, or 

transfer (in-country) of items subject to 

the EAR. These foreign persons are 

added to the UVL because BIS or federal 

officials acting on BIS’s behalf were 

unable to verify their bona fides (i.e., 

legitimacy and reliability relating to the 

end-use and end user of items subject to 

the EAR) through an end-use check. 

These checks, such as a pre-license 

check (PLC) or a post-shipment 

verification (PSV), cannot be completed 

satisfactorily for reasons outside the 

U.S. Government’s control. 

As set forth in the EAR, there are any 

number of reasons why these checks 

cannot be completed to the satisfaction 

of the U.S. Government. Section 

744.15(c)(1) of the EAR provides 

illustrative examples of those 

circumstances, including reasons 

unrelated to the cooperation of the 

foreign party subject to the end-use 

check. Such examples include: (i) 

During the conduct of an end-use check, 

the subject of the check is unable to 

demonstrate the disposition of items 

subject to the EAR; (ii) The existence or 

authenticity of the subject of an end-use 

check cannot be verified (e.g., the 

subject of the check cannot be located 

or contacted); (iii) Lack of cooperation 

by the host government authority 

prevents an end-use check from being 

conducted. 

BIS’s inability to confirm the bona 

fides of foreign persons subject to enduse checks raises concerns about the 

suitability of such persons as 

participants in future exports, reexports, 

or transfers (in-country) of items subject 

to the EAR; it also indicates a risk that 

such items may be diverted to 

prohibited end-uses and/or end-users. 

Under such circumstances, there may 

not be sufficient information to add the 

foreign person at issue to the Entity List 

under § 744.11 of the EAR. Therefore, 

BIS may add the foreign person to the 

UVL. 

As provided in § 740.2(a)(17) of the 

EAR, the use of license exceptions for 

exports, reexports, and transfers (incountry) involving a party or parties to 

the transaction who are listed on the 

UVL is suspended. Additionally, under 

§ 744.15(b) of the EAR, there is a 

requirement for exporters, reexporters, 

and transferors to obtain (and maintain 

a record of) a UVL statement from a 

party or parties to the transaction who 

are listed on the UVL before proceeding 

with exports, reexports, and transfers 

(in-country) to such persons, when the 

exports, reexports and transfers (incountry) are not subject to a license 

requirement. Finally, pursuant to 

§ 758.1(b)(8), Electronic Export 

Information (EEI) must be filed in the 

Automated Export System (AES) for all 

exports of tangible items subject to the 

EAR where any party to the transaction, 

as described in § 748.5(d) through (f), is 

listed on the UVL. 

Requests for the removal of a UVL 

entry must be made in accordance with 

§ 744.15(d) of the EAR. Decisions 

regarding the removal or modification of 

a UVL entry will be made by the Deputy 

Assistant Secretary for Export 

Enforcement, based on a demonstration 

by the listed person of their bona fides. 

Removals From the UVL 

This final rule removes three persons 

from the UVL because BIS was able to 

verify their bona fides. This rule 


khammond on DSKJM1Z7X2PROD with RULES