[4910-13-P]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1694; Project Identifier MCAI-2024-00016-T]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 2023-12-03
and AD 2023-04-05, which apply to certain Airbus SAS Model A350-941 and -1041
airplanes. AD 2023-12-03 and AD 2023-04-05 require revising the existing maintenance
or inspection program, as applicable, to incorporate new or more restrictive airworthiness
limitations. Since the FAA issued AD 2023-12-03 and AD 2023-04-05, the FAA has
determined that new or more restrictive airworthiness limitations are necessary. This
proposed AD would continue to require all actions in AD 2023-12-03 and certain actions
in AD 2023-04-05 and would require revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive airworthiness limitations,
as specified in a European Union Aviation Safety Agency (EASA) AD, which is
proposed for incorporation by reference (IBR). The FAA is proposing this AD to address
the unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by [INSERT DATE 45
DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL REGISTER].
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. FAA2024-1694; 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, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; website
easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu.
• You may view this service information at the FAA, Airworthiness Products
Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call 206-231-3195. It is also
available at regulations.gov under Docket No. FAA-2024-1694.
FOR FURTHER INFORMATION CONTACT: Dat Le, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7917;
email dat.v.le@faa.gov.

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-2024-1694; Project Identifier MCAI-2024-00016-T” 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 Dat Le, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone

516-228-7317; email dat.v.le@faa.gov. Any commentary that the FAA receives that is
not specifically designated as CBI will be placed in the public docket for this rulemaking.
Background
The FAA issued AD 2023-12-03, Amendment 39-22461 (88 FR 42598, July 3,
2023; corrected August 7, 2023 (88 FR 52024)) (AD 2023-12-03), for certain Airbus
SAS Model A350-941 and -1041 airplanes. AD 2023-12-03 was prompted by an MCAI
originated by EASA, which is the Technical Agent for the Member States of the
European Union. EASA issued AD 2023-0004, dated January 6, 2023 (EASA AD 20230004) (which corresponds to FAA AD 2023-12-03), to correct an unsafe condition.
AD 2023-12-03 requires revising the existing maintenance or inspection program,
as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA
issued AD 2023-12-03 to address reduced structural integrity of the airplane.
AD 2023-12-03 specifies that accomplishing the revision required by that AD terminates
certain requirements of AD 2023-04-05, Amendment 39-22352 (88 FR 13668, March 6,
2023) (AD 2023-04-05). This proposed AD would therefore continue to allow that
terminating action. AD 2023-04-05 corresponds to EASA AD 2022-0125, dated June 28,
2022 (EASA AD 2022-0125) and requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more restrictive airworthiness
limitations. The FAA issued AD 2023-04-05 to address reduced structural integrity of the
airplane.
Actions Since ADs 2023-12-03 and 2023-04-05 Were Issued
Since the FAA issued ADs 2023-12-03 and 2023-04-05, EASA superseded ADs
2023-0004 and 2022-0125 and issued EASA AD 2024-0005, dated January 5, 2024
(EASA AD 2024-0005) (referred to after this as the MCAI), for all Airbus SAS Model
A350-941 and -1041 airplanes. The MCAI states that new or more restrictive
airworthiness limitations have been developed.

Airplanes with an original airworthiness certificate or original export certificate of
airworthiness issued after November 30, 2023, must comply with the airworthiness
limitations specified as part of the approved type design and referenced on the type
certificate data sheet; this proposed AD therefore does not include those airplanes in the
applicability.
The FAA is proposing this AD to address reduced structural integrity of the
airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket
No. FAA-2024-1694.
Related Service Information Under 1 CFR Part 51
The FAA reviewed EASA AD 2024-0005. This service information specifies new
or more restrictive airworthiness limitations for airplane structures and safe life limits.
This proposed AD would also require EASA AD 2023-0004, which the Director
of the Federal Register approved for incorporation by reference as of August 7, 2023 (88
FR 42598, July 3, 2023; corrected August 7, 2023 (88 FR 52024)).
This proposed AD would also require EASA 2022-0125, which the Director of
the Federal Register approved for incorporation by reference as of April 10, 2023 (88 FR
13668, March 6, 2023).
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 ADDRESSES.
FAA’s Determination
This product has been approved by the aviation authority of another country and
is 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 in
other products of the same type design.

Proposed AD Requirements in this NPRM
This proposed AD would retain all requirements of AD 2023-12-03 and certain
requirements of AD 2023-04-05. This proposed AD would also require revising the
existing maintenance or inspection program, as applicable, to incorporate additional new
or more restrictive airworthiness limitations, which are specified in EASA AD 2024-0005
already described, as proposed for incorporation by reference. Any differences with
EASA AD 2024-0005 are identified as exceptions in the regulatory text of this AD.
This proposed AD would require revisions to certain operator maintenance
documents to include new actions (e.g., inspections). Compliance with these actions is
required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered,
or repaired in the areas addressed by this proposed AD, the operator may not be able to
accomplish the actions described in the revisions. In this situation, to comply with 14
CFR 91.403(c), the operator must request approval for an alternative method of
compliance (AMOC) according to paragraph (q)(1) of this proposed AD.
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 retain the IBR of EASA AD 2022-0125 and EASA AD 2023-0004
and incorporate EASA AD 2024-0005 by reference in the FAA final rule. This proposed
AD would, therefore, require compliance with EASA AD 2022-0125, EASA AD 20230004, and EASA AD 2024-0005 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 2022-0125, EASA
AD 2023-0004, or EASA AD 2024-0005 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 2024-0005. Service
information required by EASA AD 2024-0005 for compliance will be available at
regulations.gov by searching for and locating Docket No. FAA-2024-1694 after the FAA
final rule is published.
Airworthiness Limitation ADs Using the New Process
The FAA’s process of incorporating by reference MCAI ADs as the primary
source of information for compliance with corresponding FAA ADs has been limited to
certain MCAI ADs (primarily those with service bulletins as the primary source of
information for accomplishing the actions required by the FAA AD). However, the FAA
is now expanding the process to include MCAI ADs that require a change to
airworthiness limitation documents, such as airworthiness limitation sections.
For these ADs that incorporate by reference an MCAI AD that changes
airworthiness limitations, the FAA requirements are unchanged. Operators must revise
the existing maintenance or inspection program, as applicable, to incorporate the
information specified in the new airworthiness limitation document. The airworthiness
limitations must be followed according to 14 CFR 91.403(c) and 91.409(e).
The previous format of the airworthiness limitation ADs included a paragraph that
specified that no alternative actions (e.g., inspections) or intervals may be used unless the
actions and intervals are approved as an AMOC in accordance with the procedures
specified in the AMOCs paragraph under “Additional AD Provisions.” This new format
includes a “New Provisions for Alternative Actions and Intervals” paragraph that does
not specifically refer to AMOCs, but operators may still request an AMOC to use an
alternative action or interval.

Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would affect 31
airplanes of U.S. registry. The FAA estimates the following costs to comply with this
proposed AD:
The FAA estimates the total cost per operator for the retained actions from AD
2023-12-03 to be $7,650 (90 work-hours x $85 per work-hour).
The FAA has determined that revising the existing maintenance or inspection
program takes an average of 90 work-hours per operator, although the agency recognizes
that this number may vary from operator to operator. Since operators incorporate
maintenance or inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-airplane estimate.
The FAA estimates the total cost per operator for the new proposed actions to be
$7,650 (90 work-hours x $85 per work-hour).
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:
a. Removing Airworthiness Directive (AD) 2023-04-05, Amendment 39-22352
(88 FR 13668, March 6, 2023); and AD 2023-12-03, Amendment 39-22461 (88 FR
42598, July 3, 2023; corrected August 7, 2023 (88 FR 52024)); and
b. Adding the following new AD:
Airbus SAS: Docket No. FAA-2024-1694; Project Identifier MCAI-2024-00016-T.

(a) Comments Due Date
The FAA must receive comments on this airworthiness directive (AD) by
[INSERT DATE 45 DAYS AFTER DATE OF PUBLICATION IN THE FEDERAL
REGISTER].
(b) Affected ADs
This AD replaces AD 2023-04-05, Amendment 39-22352 (88 FR 13668,
March 6, 2023) (AD 2023-04-05); and AD 2023-12-03, Amendment 39-22461 (88 FR
42598, July 3, 2023; corrected August 7, 2023 (88 FR 52024)) (AD 2023-12-03).
(c) Applicability
This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated
in any category, with an original airworthiness certificate or original export certificate of
airworthiness issued on or before November 30, 2023.
(d) Subject
Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance
Checks.
(e) Unsafe Condition
This AD was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The FAA is issuing this AD to address reduced
structural integrity of the airplane. The unsafe condition, if not addressed, could result in
loss of structural integrity of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Retained Revision of the Existing Maintenance or Inspection Program from AD
2023-04-05, with New Terminating Action
This paragraph restates the requirements of paragraph (j) of AD 2023-04-05, with
new terminating action. For airplanes with an original airworthiness certificate or original
export certificate of airworthiness issued on or before May 2, 2022: Except as specified

in paragraph (h) of this AD: Comply with all required actions and compliance times
specified in, and in accordance with, European Union Aviation Safety Agency (EASA)
AD 2022-0125, dated June 28, 2022 (EASA AD 2022-0125). Accomplishing the revision
of the existing maintenance or inspection program required by paragraph (n) of this AD
terminates the requirements of this paragraph.
(h) Retained Exceptions to EASA AD 2022-0125
This paragraph restates the exceptions specified in paragraph (k) of AD 2023-0405, with no changes.
(1) Where EASA AD 2022-0125 refers to its effective date, this AD requires
using April 10, 2023 (the effective date of AD 2023-04-05).
(2) The requirements specified in paragraphs (1) and (2) of EASA AD 2022-0125
do not apply to this AD.
(3) Paragraph (3) of EASA AD 2022-0125 specifies revising “the approved
AMP” within 12 months after its effective date, but this AD requires revising the existing
maintenance or inspection program, as applicable, within 90 days after April 10, 2023
(the effective date of AD 2023-04-05).
(4) The initial compliance time for doing the tasks specified in paragraph (3) of
EASA AD 2022-0125 is at the applicable “thresholds” as incorporated by the
requirements of paragraph (3) of EASA AD 2022-0125, or within 90 days after April 10,
2023 (the effective date of AD 2023-04-05), whichever occurs later.
(5) The provisions specified in paragraphs (4) and (5) of EASA AD 2022-0125 do
not apply to this AD.
(6) The “Remarks” section of EASA AD 2022-0125 does not apply to this AD.
(i) Retained Provisions for Alternative Actions and Intervals from AD 2023-04-05,
with No Changes
This paragraph restates the requirements of paragraph (l) of AD 2023-04-05, with
no changes. Except as required by paragraphs (j) and (n) of this AD, after the existing

maintenance or inspection program has been revised as required by paragraph (g) of this
AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are
approved as specified in the provisions of the “Ref. Publications” section of EASA AD
2022-0125.
(j) Retained Revision of the Existing Maintenance or Inspection Program from AD
2023-12-03, with New Terminating Action
This paragraph restates the requirements of paragraph (g) of AD 2023-12-03, with
new terminating action. For airplanes with an original airworthiness certificate or original
export certificate of airworthiness issued on or before November 1, 2022: Except as
specified in paragraph (k) of this AD, comply with all required actions and compliance
times specified in, and in accordance with, EASA AD 2023-0004, dated January 6, 2023
(EASA AD 2023-0004). Accomplishing the revision of the existing maintenance or
inspection program required by paragraph (n) of this AD terminates the requirements of
this paragraph.
(k) Retained Exceptions to EASA AD 2023-0004, with No Changes
This paragraph restates the exceptions specified in paragraph (h) of AD
2023-12-03, with no changes.
(1) This AD does not adopt the requirements specified in paragraphs (1) and (2)
of EASA AD 2023-0004.
(2) Paragraph (3) of EASA AD 2023-0004 specifies revising “the approved
AMP” within 12 months after its effective date, but this AD requires revising the existing
maintenance or inspection program, as applicable, within 90 days after August 7, 2023
(the effective date of AD 2023-12-03).
(3) The initial compliance time for doing the tasks specified in paragraph (3) of
EASA 2023-0004 is on or before the applicable “associated thresholds” as incorporated
by the requirements of paragraph (3) of EASA AD 2023-0004, or within 90 days after
August 7, 2023 (the effective date of AD 2023-12-03), whichever occurs later.

(4) This AD does not adopt the provisions specified in paragraphs (4) of EASA
AD 2023-0004.
(5) This AD does not adopt the “Remarks” section of EASA AD 2023-0004.
(l) Retained Provisions for Alternative Actions and Intervals from AD 2023-12-03,
with No Changes
This paragraph restates the requirements of paragraph (i) of AD 2023-12-03, with
no changes. Except as required by paragraph (n) of this AD, after the existing
maintenance or inspection program has been revised as required by paragraph (j) of this
AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are
approved as specified in the provisions of the “Ref. Publications” section of EASA AD
2023-0004.
(m) Retained Terminating Action from AD 2023-12-03, with No Changes
This paragraph restates the terminating action specified in paragraph (j) of AD
2023-12-03, with no changes. Accomplishing the actions required by paragraph (j) of this
AD terminates the corresponding requirements of paragraph (g) of this AD, for the tasks
identified in the service information referenced in EASA AD 2023-0004 only.
(n) New Revision of the Existing Maintenance or Inspection Program
Except as specified in paragraph (o) of this AD: Comply with all required actions
and compliance times specified in, and in accordance with, EASA AD 2024-0005, dated
January 5, 2024 (EASA AD 2024-0005). Accomplishing the revision of the existing
maintenance or inspection program required by this paragraph terminates the
requirements of paragraphs (g) and (j) of this AD.
(o) Exceptions to EASA AD 2024-0005
(1) This AD does not adopt the requirements specified in paragraphs (1) and (2)
of EASA AD 2024-0005.
(2) Paragraph (3) of EASA AD 2024-0005 specifies revising “the approved
AMP,” within 12 months after its effective date, but this AD requires revising the

existing maintenance or inspection program, as applicable, within 90 days after the
effective date of this AD.
(3) The initial compliance time for doing the tasks specified in paragraph (3) of
EASA AD 2024-0005 is at the applicable “limitations” and “associated thresholds” as
incorporated by the requirements of paragraph (3) of EASA AD 2024-0005, or within 90
days after the effective date of this AD, whichever occurs later.
(4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of
EASA AD 2024-0005.
(5) This AD does not adopt the “Remarks” section of EASA AD 2024-0005.
(p) New Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been revised as required
by paragraph (n) of this AD, no alternative actions (e.g., inspections) and intervals are
allowed unless they are approved as specified in the provisions of the “Ref. Publications”
section of EASA AD 2024-0005.
(q) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): 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 responsible Flight Standards Office, as
appropriate. If sending information directly to the manager of the International Validation
Branch, mail it to the address identified in paragraph (r) of this AD. Information may be
emailed to: 9-AVS-AIR-730-AMOC@faa.gov. Before using any approved AMOC,
notify your appropriate principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.

(2) Contacting the Manufacturer: For any requirement in this AD to obtain
instructions from a manufacturer, the instructions must be accomplished using a method
approved by the Manager, International Validation Branch, FAA; or EASA; or Airbus
SAS’s EASA Design Organization Approval (DOA). If approved by the DOA, the
approval must include the DOA-authorized signature.
(r) Additional Information
For more information about this AD, contact Dat Le, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7317;
email dat.v.le@faa.gov.
(s) 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 this AD specifies otherwise.
(3) The following service information was approved for IBR on [DATE 35 DAYS
AFTER PUBLICATION OF THE FINAL RULE].
(i) European Union Aviation Safety Agency (EASA) AD 2024-0005, dated
January 5, 2024.
(ii) [Reserved]
(4) The following service information was approved for IBR on August 7, 2023
(88 FR 42598, July 3, 2023; corrected August 7, 2023 (88 FR 52024)).
(i) EASA AD 2023-0004, dated January 6, 2023.
(ii) [Reserved]
(5) The following service information was approved for IBR on April 10, 2023
(88 FR 13668, March 6, 2023).

(i) EASA 2022-0125, dated June 28, 2022.
(ii) [Reserved]
(6) For EASA ADs 2022-0125, 2023-0004, and 2024-0005 contact EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
ADs@easa.europa.eu; website easa.europa.eu. You may find these EASA ADs on the
EASA website at ad.easa.europa.eu.
(7) You may view this material at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on
the availability of this material at the FAA, call 206-231-3195.
(8) 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 June 18, 2024.

Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division,
Aircraft Certification Service.
[FR Doc. 2024-13780 Filed: 6/25/2024 8:45 am; Publication Date: 6/26/2024]