Federal Register / Vol. 89, No. 246 / Monday, December 23, 2024 / Proposed Rules 104465 

2, of CFM SB LEAP–1A–72–00–0493–01A– 

930A–D, whichever occurs first after June 23, 

2023 (the effective date of AD 2023–09–06); 

or if the applicable CSN threshold has been 

exceeded as of June 23, 2023 (the effective 

date of AD 2023–09–06), within 50 FCs from 

June 23, 2023 (the effective date of AD 2023– 

09–06), remove the HPT stage 1 disk from 

service and replace with a part eligible for 

installation. 

(4) For engines with an installed HPT stage 

1 disk having a P/N and S/N identified in 

Compliance, paragraph 3.E., Tables 1 through 

2, of CFM SB LEAP–1A–72–00–0507–01A– 

930A–D, Issue 001, dated January 24, 2024 

(CFM SB LEAP–1A–72–00–0507–01A–930A– 

D): At the next piece-part exposure of the 

HPT stage 1 disk, or before exceeding the 

applicable CSN threshold identified in 

Compliance, paragraph 3.E., Tables 1 through 

2, of CFM SB LEAP–1A–72–00–0507–01A– 

930A–D, whichever occurs first after the 

effective date of this AD; or if the applicable 

CSN threshold has been exceeded as of the 

effective date of this AD, within 50 FCs from 

the effective date of this AD; remove the HPT 

stage 1 disk from service and replace with a 

part eligible for installation. 

(h) Definition 

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

for installation’’ is an HPT stage 1 disk, 

forward outer seal, or compressor rotor stages 

6–10 spool that does not have a P/N and S/ 

N identified in the service information listed 

in paragraphs (g)(1) through (4) of this AD. 

(i) Installation Prohibition 

After the effective date of this AD, do not 

install an HPT stage 1 disk, forward outer 

seal, or compressor rotor stages 6–10 spool 

that has a P/N and S/N identified in the 

service information listed in paragraphs (g)(1) 

through (4) of this AD on any engine. 

(j) 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 (k) of this AD and email to: 

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 Mehdi Lamnyi, Aviation Safety 

Engineer, FAA, 2200 South 216th Street, Des 

Moines, WA 98198; phone: (781) 238–7743; 

email: mehdi.lamnyi@faa.gov. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the material listed in this paragraph 

under 5 U.S.C. 552(a) and 1 CFR part 51. 

(2) You must use this material as 

applicable to do the actions required by this 

AD, unless the AD specifies otherwise. 

(3) The following material was approved 

for IBR on [DATE 35 DAYS AFTER 

PUBLICATION OF THE FINAL RULE]. 

(i) CFM Service Bulletin LEAP–1A–72–00– 

0507–01A–930A–D, Issue 001, dated January 

24, 2024. 

(ii) [Reserved] 

(4) The following material was approved 

for IBR on June 23, 2023 (88 FR 32092, May 

19, 2023). 

(i) CFM Service Bulletin LEAP–1A–72–00– 

0470–01A–930A–D, Issue 003, dated March 

3, 2023. 

(ii) CFM Service Bulletin LEAP–1A–72– 

00–0493–01A–930A–D, Issue 002, dated 

November 17, 2022. 

(iii) CFM Service Bulletin LEAP–1A–72– 

00–0496–01A–930A–D, Issue 001, dated 

March 7, 2023. 

(5) For CFM material identified in this AD, 

contact CFM International, S.A., GE Aviation 

Fleet Support, 1 Neumann Way, M/D Room 

285, Cincinnati, OH 45215; phone: (877) 

432–3272; email: aviation.fleetsupport@

ge.com. 

(6) You may view this material 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. 

(7) 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-locations or email fr.inspection@nara.gov. 

Issued on December 17, 2024. 

Suzanne Masterson, 

Deputy Director, Integrated Certificate 

Management Division, Aircraft Certification 

Service. 

[FR Doc. 2024–30539 Filed 12–20–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2024–2663; Project 

Identifier MCAI–2023–00200–R] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Helicopters 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Notice of proposed rulemaking 

(NPRM). 

SUMMARY: The FAA proposes to adopt a 

new airworthiness directive (AD) for 

certain Airbus Helicopters Model 

EC225LP helicopters. This proposed AD 

was prompted by the identification of 

missing electrical bonding on a certain 

part-numbered additional and optional 

search light (search light). This 

proposed AD would require installing 

an electrical bonding braid modification 

and prohibit installing that partnumbered search light unless the 

modification is done. These actions are 

specified in a European Union Aviation 

Safety Agency (EASA) AD, which is 

proposed for incorporation by reference. 

The FAA is proposing this AD to 

address the unsafe condition on these 

products. 

DATES: The FAA must receive comments 

on this NPRM by February 6, 2025. 

ADDRESSES: You may send comments, 

using the procedures found in 14 CFR 

11.43 and 11.45, by any of the following 

methods: 

• Federal eRulemaking Portal: Go to 

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: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2024–2663; 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 NPRM, the mandatory 

continuing airworthiness information 

(MCAI), any comments received, and 

other information. The street address for 

Docket Operations is listed above. 

Material Incorporated by Reference: 

• For EASA material identified in this 

proposed AD, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne, 

Germany; phone: +49 221 8999 000; 

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

easa.europa.eu. You may find the EASA 

material on the EASA website at 

ad.easa.europa.eu. 

• You may view this material at the 

FAA, Office of the Regional Counsel, 

Southwest Region, 10101 Hillwood 

Pkwy., Room 6N 321, Fort Worth, TX 

76177. 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–2024–2663. 

FOR FURTHER INFORMATION CONTACT: Kurt 

Ladendorf, Aviation Safety Engineer, 

FAA, 1600 Stewart Avenue, Suite 410, 

Westbury, NY 11590; phone: (817) 222– 

5254; email: Kurt.D.Ladendorf@faa.gov. 


khammond on DSK9W7S144PROD with PROPOSALS
104466 Federal Register / Vol. 89, No. 246 / Monday, December 23, 2024 / Proposed Rules 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

The FAA invites you to send any 

written relevant data, views, or 

arguments about this proposal. Send 

your comments to an address listed 

under ADDRESSES. Include ‘‘Docket No. 

FAA–2024–2663; Project Identifier 

MCAI–2023–00200–R’’ at the beginning 

of your comments. The most helpful 

comments reference a specific portion of 

the proposal, explain the reason for any 

recommended change, and include 

supporting data. The FAA will consider 

all comments received by the closing 

date and may amend this proposal 

because of those comments. 

Except for Confidential Business 

Information (CBI) as described in the 

following paragraph, and other 

information as described in 14 CFR 

11.35, the FAA will post all comments 

received, without change, to 

regulations.gov, including any personal 

information you provide. The agency 

will also post a report summarizing each 

substantive verbal contact received 

about this NPRM. 

Confidential Business Information 

CBI is commercial or financial 

information that is both customarily and 

actually treated as private by its owner. 

Under the Freedom of Information Act 

(FOIA) (5 U.S.C. 552), CBI is exempt 

from public disclosure. If your 

comments responsive to this NPRM 

contain commercial or financial 

information that is customarily treated 

as private, that you actually treat as 

private, and that is relevant or 

responsive to this NPRM, it is important 

that you clearly designate the submitted 

comments as CBI. Please mark each 

page of your submission containing CBI 

as ‘‘PROPIN.’’ The FAA will treat such 

marked submissions as confidential 

under the FOIA, and they will not be 

placed in the public docket of this 

NPRM. Submissions containing CBI 

should be sent to Kurt Ladendorf, 

Aviation Safety Engineer, FAA, 1600 

Stewart Avenue, Suite 410, Westbury, 

NY 11590; phone: (817) 222–5254; 

email: Kurt.D.Ladendorf@faa.gov. Any 

commentary that the FAA receives 

which is not specifically designated as 

CBI will be placed in the public docket 

for this rulemaking. 

Background 

EASA, which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2023–0030, 

dated February 2, 2023 (EASA AD 

2023–0030) (also referred to as the 

MCAI), to correct an unsafe condition 

on Airbus Helicopters Model EC 225 LP 

helicopters, except helicopters having 

Airbus Helicopters modification 

MC29201 embodied in production. The 

MCAI states missing electrical bonding 

was identified on a certain partnumbered search light installed on some 

Model EC 225 LP helicopters. The MCAI 

further states that the location where the 

search light is installed is an area that 

could get struck by lightning, which, in 

case of a lightning strike, could lead to 

potential total loss of electrical 

distribution, with loss of electrically 

supplied systems, and subsequent 

reduced control of the helicopter. 

The FAA is proposing this AD to 

address the unsafe condition on these 

products. You may examine the MCAI 

in the AD docket at regulations.gov 

under Docket No. FAA–2024–2663. 

Material Incorporated by Reference 

Under 1 CFR Part 51 

EASA AD 2023–0030 requires 

installing an electrical bonding braid 

modification for a certain partnumbered search light under the 

sponson. EASA AD 2023–0030 also 

prohibits installing that part-numbered 

search light from being installed unless 

its requirements are met. 

This material 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. 

FAA’s Determination 

These products have been approved 

by the aviation authority of another 

country and are approved for operation 

in the United States. Pursuant to the 

FAA’s bilateral agreement with this 

State of Design Authority, it has notified 

the FAA of the unsafe condition 

described in the MCAI referenced 

above. The FAA is issuing this NPRM 

after determining that the unsafe 

condition described previously is likely 

to exist or develop on other products of 

the same type design. 

Proposed AD Requirements in This 

NPRM 

This proposed AD would require 

accomplishing the actions specified in 

EASA AD 2023–0030, described 

previously, as incorporated by 

reference, except for any differences 

identified as exceptions in the 

regulatory text of this proposed AD and 

except as discussed under ‘‘Differences 

Between this Proposed AD and the 

MCAI.’’ 

Explanation of Required Compliance 

Information 

In the FAA’s ongoing efforts to 

improve the efficiency of the AD 

process, the FAA developed a process to 

use some civil aviation authority (CAA) 

ADs as the primary source of 

information for compliance with 

requirements for corresponding FAA 

ADs. The FAA has been coordinating 

this process with manufacturers and 

CAAs. As a result, the FAA proposes to 

incorporate EASA AD 2023–0030 by 

reference in the FAA final rule. This 

proposed AD would, therefore, require 

compliance with EASA AD 2023–0030 

in its entirety through that 

incorporation, except for any differences 

identified as exceptions in the 

regulatory text of this proposed AD. 

Using common terms that are the same 

as the heading of a particular section in 

EASA AD 2023–0030 does not mean 

that operators need comply only with 

that section. For example, where the AD 

requirement refers to ‘‘all required 

actions and compliance times,’’ 

compliance with this AD requirement is 

not limited to the section titled 

‘‘Required Action(s) and Compliance 

Time(s)’’ in EASA AD 2023–0030. 

Material referenced in EASA AD 2023– 

0030 for compliance will be available at 

regulations.gov under Docket No. FAA– 

2024–2663 after the FAA final rule is 

published. 

Differences Between This Proposed AD 

and the MCAI 

The MCAI allows a +10% tolerance to 

the calendar compliance time to install 

the electrical bonding braid 

modification, whereas this proposed AD 

would not allow that tolerance. If the 

insulation resistance value is 8 or more 

ohms as a result of the continuity test 

that is specified in the material 

referenced in EASA AD 2023–0030, this 

proposed AD would require 

accomplishing corrective action in 

accordance with a method approved by 

the FAA, EASA, or Airbus Helicopters’ 

EASA Design Organization Approval, 

whereas the MCAI and the material 

referenced in the MCAI are not specific 

about the continuity test. 

Costs of Compliance 

The FAA estimates that this AD, if 

adopted as proposed, would affect 9 

helicopters of U.S. Registry. Labor rates 

are estimated at $85 per work-hour. 

Based on these numbers, the FAA 

estimates the following costs to comply 

with this proposed AD. 

Installing an electrical bonding braid 

modification would take 14 work-hours 

and parts would cost $16,370 for an 

estimated cost of $17,560 per helicopter 

and up to $158,040 for the U.S. fleet. 

Performing a continuity test would 

take a minimal amount of time for a 

nominal cost. Depending on the results, 


khammond on DSK9W7S144PROD with PROPOSALS
Federal Register / Vol. 89, No. 246 / Monday, December 23, 2024 / Proposed Rules 104467 

corrective action could vary 

significantly from helicopter to 

helicopter. The FAA has no data to 

determine the costs to accomplish the 

corrective action. 

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 

The FAA determined that this 

proposed AD would not have federalism 

implications under Executive Order 

13132. This proposed AD would 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 proposed regulation: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Would not affect intrastate 

aviation in Alaska, and 

(3) Would 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 Proposed Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA proposes to amend 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: 

Airbus Helicopters: Docket No. FAA–2024– 

2663; Project Identifier MCAI–2023– 

00200–R. 

(a) Comments Due Date 

The FAA must receive comments on this 

airworthiness directive (AD) by February 6, 

2025. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Airbus Helicopters 

Model EC225LP helicopters, certificated in 

any category, as identified in European 

Union Aviation Safety Agency AD 2023– 

0030, dated February 2, 2023 (EASA AD 

2023–0030). 

(d) Subject 

Joint Aircraft System Component (JASC) 

Code: 1420, electrical connectors; and 2497, 

electrical power system wiring. 

(e) Unsafe Condition 

This AD was prompted by the 

identification of missing electrical bonding 

on additional and optional search lights. The 

FAA is issuing this AD to prevent a lightning 

current evacuating to the aircraft structure. In 

the event of a lightning strike, the unsafe 

condition, if not addressed, could result in 

potential total loss of electrical distribution, 

with loss of electrically supplied systems, 

and subsequent reduced control of the 

helicopter. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Requirements 

Except as specified in paragraphs (h) and 

(i) of this AD: Comply with all required 

actions and compliance times specified in, 

and in accordance with, EASA AD 2023– 

0030. 

Note 1 to paragraph (g): Appendix 4 of 

Airbus Helicopters Alert Service Bulletin No. 

EC225–33A018, dated December 15, 2023, 

which is referenced in EASA AD 2023–0030, 

identifies helicopter configurations (righthand column of the table) by helicopter serial 

number (left-hand column of the table). 

(h) Exceptions to EASA AD 2023–0030 

(1) Where EASA AD 2023–0030 requires 

compliance in terms of flight hours, this AD 

requires using hours time-in-service. 

(2) Where EASA AD 2023–0030 refers to its 

effective date, this AD requires using the 

effective date of this AD. 

(3) Where Note 1 of EASA AD 2023–0030 

specifies that a tolerance of +10% may be 

applied to the calendar compliance time 

specified in paragraph (1) of EASA AD 2023– 

0030, this AD does not allow that tolerance. 

(4) Where the material referenced in EASA 

AD 2023–0030 specifies discarding parts, this 

AD requires removing those parts from 

service. 

(5) This AD requires replacing text as 

specified in paragraphs (h)(5)(i) though (v) of 

this AD. 

(i) Where the material referenced in EASA 

AD 2023–0030 specifies to ‘‘do the electrical 

bonding,’’ this AD requires replacing that text 

with ‘‘install the electrical bonding braid.’’ 

(ii) Where the material referenced in EASA 

AD 2023–0030 specifies to ‘‘bond the labels 

‘‘741VN’’ and ‘‘742VN’’ of the set of labels (8) 

as close as possible from the equipment 

(SECTION A–A and B–B),’’ this AD requires 

replacing that text with ‘‘apply labels 

‘‘741VN’’ and ‘‘742VN’’ of the set of labels (8) 

directly adjacent to the grounding point as 

depicted in Figure 6, Section A–A and 

Section B–B.’’ 

(iii) Where the material referenced in 

EASA AD 2023–0030 specifies to ‘‘remove 

and keep,’’ this AD requires replacing that 

text with, ‘‘remove.’’ 

(iv) Where the material referenced in EASA 

AD 2023–0030 specifies to ‘‘locate the hole 

(A) in accordance to the position,’’ this AD 

requires replacing that text with ‘‘determine 

the position of hole (A) in Figure 4, Detail B.’’ 

(v) Where the material referenced in EASA 

AD 2023–0030 specifies to paint strip the 

hole on ‘‘the both face,’’ this AD requires 

replacing the text ‘‘the both face’’ with ‘‘each 

side.’’ 

(6) Where the material referenced in EASA 

AD 2023–0030 specifies to do a continuity 

test, if the insulation resistance value is 8 or 

more ohms as a result of the continuity test, 

this AD requires, before further flight, 

accomplishing corrective action in 

accordance with a method approved by the 

Manager, International Validation Branch, 

FAA; or EASA; or Airbus Helicopters’ EASA 

Design Organization Approval (DOA). If 

approved by the DOA, the approval must 

include the DOA-authorized signature. 

(7) This AD does not adopt the ‘‘Remarks’’ 

section of EASA AD 2023–0030. 

(i) No Reporting Requirement 

Although the material referenced in EASA 

AD 2023–0030 specifies to submit certain 

information to the manufacturer, this AD 

does not include that requirement. 

(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)(1) of this AD. 

Information may be emailed to: 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. 


khammond on DSK9W7S144PROD with PROPOSALS
104468 Federal Register / Vol. 89, No. 246 / Monday, December 23, 2024 / Proposed Rules 

(k) Related Information 

(1) For more information about this AD, 

contact Kurt Ladendorf, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; phone: (817) 222– 

5254; email: Kurt.D.Ladendorf@faa.gov. 

(2) For Airbus Helicopters material 

identified in this AD that is not incorporated 

by reference, contact Airbus Helicopters, 

2701 North Forum Drive, Grand Prairie, TX 

75052; phone: (972) 641–0000 or (800) 232– 

0323; fax: (972) 641–3775; website: 

airbus.com/en/products-services/helicopters/ 

hcare-services/airbusworld. 

(l) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the material listed in this paragraph 

under 5 U.S.C. 552(a) and 1 CFR part 51. 

(2) You must use this material as 

applicable to do the actions required by this 

AD, unless the AD specifies otherwise. 

(i) European Union Aviation Safety Agency 

(EASA) AD 2023–0030, dated February 2, 

2023. 

(ii) [Reserved] 

(3) For EASA material identified in this 

AD, 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 the 

EASA material on the EASA website at 

ad.easa.europa.eu. 

(4) You may view this material at the FAA, 

Office of the Regional Counsel, Southwest 

Region, 10101 Hillwood Pkwy., Room 6N– 

321, Fort Worth, TX 76177. 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-locations or email fr.inspection@nara.gov. 

Issued on December 16, 2024. 

Victor Wicklund, 

Deputy Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2024–30374 Filed 12–20–24; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2024–2048; Airspace 

Docket No. 24–AWP–101] 

RIN 2120–AA66 

Modification of Class E Airspace; 

Colusa County Airport, Colusa, CA 

Correction 

Proposed Rule Document 2024– 

27837, appearing on pages 94601– 

94603, in the issue of Friday, November 

29, 2024, was incorrectly published in 

the Rules section and should have 

appeared in the Proposed Rules section. 

[FR Doc. C1–2024–27837 Filed 12–19–24; 2:00 pm] 

BILLING CODE 0099–10–P 

DEPARTMENT OF THE TREASURY 

Internal Revenue Service 

26 CFR Part 1 

[REG–106595–22] 

RIN 1545–BQ83 

Substantiation Requirements and 

Qualified Nonpersonal Use Vehicles; 

Correction 

AGENCY: Internal Revenue Service (IRS), 

Treasury. 

ACTION: Notice of proposed rulemaking; 

correction. 

SUMMARY: This document corrects a 

notice of proposed rulemaking (REG– 

106595–22), published in the Federal 

Register on December 3, 2024, 

containing proposed regulations relating 

to the definition of qualified 

nonpersonal use vehicles. 

DATES: Written or electronic comments 

and requests for a public hearing must 

be received by March 3, 2025. 

ADDRESSES: Commenters are strongly 

encouraged to submit public comments 

electronically via the Federal 

eRulemaking Portal at http://

www.regulations.gov (indicate IRS and 

REG–106595–22) by following the 

online instructions for submitting 

comments. Requests for a public hearing 

must be submitted as prescribed in the 

‘‘Comments and Requests for a Public 

Hearing’’ section. Once submitted to the 

Federal Rulemaking Portal, comments 

cannot be edited or withdrawn. The 

Department of the Treasury (Treasury 

Department) and the IRS will publish 

for public availability any comment 

submitted electronically or on paper, to 

the IRS’s public docket. Send paper 

submissions to CC:PA:01:PR (REG– 

106595–22), Room 5203, Internal 

Revenue Service, P.O. Box 7604, Ben 

Franklin Station, Washington, DC 

20044. 

FOR FURTHER INFORMATION CONTACT: 

Concerning the proposed regulations, 

Stephanie Caden at (202) 317–4774; 

concerning submissions of comments or 

requests for a public hearing, the 

Publications and Regulations section by 

email at publichearings@irs.gov 

(preferred) or (202) 317–6901 (not tollfree numbers). 

SUPPLEMENTARY INFORMATION: 

Background 

The notice of proposed rulemaking 

(REG–106595–22) that is subject to this 

correction contains proposed 

regulations issued under the authority 

granted to the Secretary of the Treasury 

or her delegate (Secretary) by sections 

274(p) and 132(o) of the Internal 

Revenue Code (Code) that would amend 

the Income Tax Regulations (26 CFR 

part 1) under sections 274(i) and 132(d) 

related to qualified nonpersonal use 

vehicles. 

Correction of Publication 

Accordingly, FR Doc. 2024–28040 

(REG–106595–22), appearing on page 

95727 in the Federal Register on 

Tuesday, December 3, 2024, is corrected 

on page 95727, in the second column, 

under the caption FOR FURTHER

INFORMATION CONTACT, the second line is 

corrected to read ‘‘Stephanie Caden at 

(202) 317–4774;’’. 

Aron L. Cosby, 

Federal Register Liaison, Publications and 

Regulations Branch, Legal Processing 

Division, Associate Chief Counsel (Procedure 

and Administration). 

[FR Doc. 2024–30280 Filed 12–20–24; 8:45 am] 

BILLING CODE 4830–01–P 

DEPARTMENT OF DEFENSE 

Office of the Secretary 

32 CFR Part 310 

[Docket ID: DoD–2024–OS–0135] 

RIN 0790–AL55 

Privacy Act of 1974; Implementation 

AGENCY: Office of the Secretary of 

Defense (OSD), Department of Defense 

(DoD). 

ACTION: Proposed rule. 

SUMMARY: The Department of Defense 

(Department or DoD) is giving 

concurrent notice of a new Departmentwide system of records pursuant to the 

Privacy Act of 1974 for the DoD–0023, 

‘‘Military Corrections and Parole Board 

Records’’ system of records and this 

proposed rulemaking. In this proposed 

rulemaking, the Department proposes to 

exempt portions of this system of 

records from certain provisions of the 

Privacy Act because of national security 

and law enforcement requirements. 

DATES: Send comments on or before 

February 21, 2025. 

ADDRESSES: You may submit comments, 

identified by docket number and title, 

by any of the following methods. 


khammond on DSK9W7S144PROD with PROPOSALS