AD 2026-13-06

This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Rules and Regulations Federal Register 40353 Vol. 91, No. 126 Thursday, July 2, 2026 DEPARTMENT OF AGRICULTURE 7 CFR Part 1b [USDA–2025–0008] RIN 0503–AA86 National Environmental Policy Act AGENCY : Department of Agriculture (USDA). ACTION : Final rule; correcting amendment. SUMMARY : This document corrects a technical error in the final rule that appeared in the April 3, 2026, Federal Register , titled ‘‘National Environmental Policy Act.’’ DATES : Effective July 2, 2026. SUPPLEMENTARY INFORMATION : The Department of Agriculture is correcting its final rule that published April 3, 2026 at 91 FR 17062 by amending an incorrect cross-reference. List of Subjects in 7 CFR Part 1b Environmental impact statements. Accordingly, 7 CFR part 1b is corrected by making the following correcting amendment: ■ 1. The authority citation for part 1b continues to read: Authority: 5 U.S.C. 301; 42 U.S.C. 4321– 4347; E.O. 11514, 3 CFR, 1966–1970 Comp., p. 902, as amended by E.O. 11991, 3 CFR, 1978 Comp., p. 123; E.O. 12114, 3 CFR, 1980 Comp., p. 356; 40 CFR 1507.3. § 1b.9 [Corrected] ■ 2. Amend § 1b.9(e)(2) by removing the citation ‘‘(c)(7)’’ and adding in its place the citation ‘‘(e)(7)’’. Tera Graelyn, Environmental Review Specialist, Office of the Secretary. [FR Doc. 2026–13372 Filed 7–1–26; 8:45 am] BILLING CODE 3410–90–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2026–4661; Project Identifier MCAI–2025–01530–E; Amendment 39–23388; AD 2026–13–06] RIN 2120–AA64 Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule; request for comments. SUMMARY : The FAA is superseding Airworthiness Directive (AD) 2024–25– 10, which applied to certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Model Trent XWB–97 engines. AD 2024–25–10 required a one-time set of visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire; and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. Since the FAA issued AD 2024–25–10, the FAA has determined that additional engine models are affected by the unsafe condition and that the required inspections should be repetitive. This AD requires, for certain engines, a one-time set of on-wing visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. This AD also requires, for certain other engines, on-wing and in-shop repetitive visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. This AD also expands the applicability to include certain RRD Model Trent XWB– 75, Trent XWB–79, Trent XWB–79B, and Trent XWB–84 engines. This AD also provides criteria for installation of an affected part and optional terminating action for the repetitive visual and dimensional inspections. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD is effective July 17, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 17, 2026. The FAA must receive comments on this AD by August 17, 2026. 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–2026–4661; 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, 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 European Union Aviation Safety Agency (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 this material on the EASA website at ad.easa.europa.eu. • You may view this material at the FAA, 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– 2026–4661. VerDate Sep<11>2014 16:02 Jul 01, 2026 Jkt 268001 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 E:\FR\FM\02JYR1.SGM 02JYR1 khammond on DSK9W7S144PROD with RULES

40354 Federal Register / Vol. 91, No. 126 / Thursday, July 2, 2026 / Rules and Regulations FOR FURTHER INFORMATION CONTACT : Barbara Caufield, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (781) 238–7146; email: barbara.caufield@ faa.gov. SUPPLEMENTARY INFORMATION : Comments Invited The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments using a method listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2026–4661; Project Identifier MCAI–2025–01530–E’’ at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, 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 final rule 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 final rule. 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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Barbara Caufield, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking. Background The FAA issued AD 2024–25–10, Amendment 39–22912 (90 FR 8661, January 31, 2025) (AD 2024–25–10), for certain RRD Model Trent XWB–97 engines. AD 2024–25–10 was prompted by an emergency AD originated by EASA, which is the Technical Agent for the Member States of the European Union. EASA issued EASA Emergency AD 2024–0174–E, dated September 5, 2024 (EASA Emergency AD 2024–0174– E) to correct an unsafe condition identified as damage to the main fuel hose assembly of the fuel manifold. AD 2024–25–10 required a one-time set of visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire; and, if necessary, replacement of the main fuel hose assembly of the fuel manifold. The FAA issued AD 2024–25–10 to prevent damage to the main fuel hose assembly of the fuel manifold. Actions Since EASA Emergency AD 2024–0174–E Was Issued EASA superseded EASA Emergency AD 2024–0174–E and issued EASA AD 2024–0182, dated September 19, 2024 (later revised) (EASA AD 2024–0182); EASA AD 2024–0182R1, dated October 9, 2024 (superseded) (EASA AD 2024– 0182R1); EASA AD 2025–0128, dated June 3, 2025 (later revised) (EASA AD 2025–0128); and EASA AD 2025– 0128R1, dated June 17, 2025 (EASA AD 2025–0128R1) (also referred to as the MCAI). EASA AD 2024–0182 included new service material, specified that a certain cleaning process available during engine refurbishment may lead to degradation of the main fuel hose assembly of the fuel manifold, that additional engine model groups were affected by the unsafe condition, and that repetitive inspections were necessary. EASA AD 2024–0182R1 included a revision to the service material and clarified the terminating action for the repetitive inspections. EASA AD 2025–0128, included a revision to the service material and identified an additional population of engines affected by the unsafe condition and required repetitive inspections and corrective actions for those engines. The MCAI states that damage to a fuel manifold main fuel hose was reported, which led to a controlled, temporary engine fire and heat damage to the exterior and interior of the engine nacelle (thrust reverser C-ducts). The occurrence resulted in an in-flight shutdown. In-service and in-shop inspections identified a specific cleaning process available during engine refurbishment that may lead to degradation of the main fuel hose assembly of the fuel manifold. Additionally, multiple additional populations of affected engines were identified, and a determination was made that the initial population of affected engines could be reduced to exclude certain engine serial numbers. To address this potential unsafe condition, the manufacturer published service information that specifies procedures for a one-time set of visual and dimensional inspections of the fuel manifold main fuel hoses and corrective action instructions. This condition, if not addressed, in combination with additional failures, could lead to an engine fire and damage to the airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2026–4661. Material Incorporated by Reference Under 1 CFR Part 51 The FAA reviewed EASA AD 2025– 0128R1, which specifies procedures for a one-time set of on-wing visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire and, if necessary, replacement of the main fuel hose assembly of the fuel manifold, and reporting the inspection results to RRD. EASA AD 2025–0128R1 also specifies procedures for on-wing and in-shop repetitive visual and dimensional inspections of the main fuel hose assembly of the fuel manifold to confirm softness, compliance, and lack of resistance, and for shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire and, if necessary, replacement of the main fuel hose assembly of the fuel manifold, and reporting the inspection results to RRD. EASA AD 2025–0128R1 also allows installation of an affected part on any airplane provided that the part is serviceable and allows installation of an affected engine provided that the engine passed the required inspections, or the findings were corrected. EASA AD 2025–0128R1 also includes optional terminating action for the repetitive visual and dimensional inspections provided that the engine has passed an inspection with no findings or the findings are corrected, or the engine has not yet reached the threshold of the required inspections. 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. VerDate Sep<11>2014 16:02 Jul 01, 2026 Jkt 268001 PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 E:\FR\FM\02JYR1.SGM 02JYR1 khammond on DSK9W7S144PROD with RULES

40355 Federal Register / Vol. 91, No. 126 / Thursday, July 2, 2026 / Rules and Regulations FAA’s Determination These products have been approved by the civil aviation authority (CAA) 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, that authority has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA is issuing this AD after determining that the unsafe condition described previously is likely to exist or develop on other products of the same type design. AD Requirements This AD requires accomplishing the actions specified in EASA AD 2025– 0128R1, described previously, as incorporated by reference, except for any differences identified as exceptions in the regulatory text of this 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 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, EASA AD 2025–0128R1 is incorporated by reference in this AD. This AD requires compliance with EASA AD 2025–0128R1 in its entirety through that incorporation, except for any differences identified as exceptions in the regulatory text of this AD. Using common terms that are the same as the heading of a particular section in EASA AD 2025–0128R1 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 2025–0128R1. Material required by EASA AD 2025– 0128R1 for compliance will be available at regulations.gov under Docket No. FAA–2026–4661 after this AD is published. Interim Action The preamble to AD 2024–25–10 specifies that the FAA considers that AD to be an ‘‘interim action’’ and that the FAA might consider further rulemaking depending on the results of the investigation. The manufacturer has since developed such repetitive inspections and, if necessary, replacement of the main fuel hose assembly of the fuel manifold for certain engines, which is optional terminating action to the repetitive inspections required by AD 2024–25–10. The FAA has determined that these actions must be required to mitigate the unsafe condition. Justification for Immediate Adoption and Determination of the Effective Date Section 553(b) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq. ) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for ‘‘good cause,’’ finds that those procedures are ‘‘impracticable, unnecessary, or contrary to the public interest.’’ Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than thirty days, upon a finding of good cause. The FAA justifies waiving notice and comment prior to adoption of this rule because no domestic operators use this product. It is unlikely that the FAA will receive any adverse comments or useful information about this AD from any U.S. operator. Accordingly, notice and opportunity for prior public comment are unnecessary, pursuant to 5 U.S.C. 553(b). In addition, for the foregoing reason(s), the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days. Regulatory Flexibility Act The requirements of the Regulatory Flexibility Act (RFA) do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because FAA has determined that it has good cause to adopt this rule without prior notice and comment, RFA analysis is not required. Costs of Compliance There are no costs of compliance with this AD because there are no engines with this type certificate on the U.S. Registry. 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: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, and (2) Will not affect intrastate aviation in Alaska. 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: ■ a. Removing Airworthiness Directive 2024–25–10, Amendment 39–22912 (90 FR 8661, January 31, 2025); and ■ b. Adding the following new airworthiness directive: 2026–13–06 Rolls-Royce Deutschland Ltd & Co KG: Amendment 39–23388; Docket No. FAA–2026–4661; Project Identifier MCAI–2025–01530–E. (a) Effective Date This airworthiness directive (AD) is effective July 17, 2026. (b) Affected ADs This AD replaces AD 2024–25–10, Amendment 39–22912 (90 FR 8661, January 31, 2025) (AD 2024–25–10). VerDate Sep<11>2014 16:02 Jul 01, 2026 Jkt 268001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\02JYR1.SGM 02JYR1 khammond on DSK9W7S144PROD with RULES

40356 Federal Register / Vol. 91, No. 126 / Thursday, July 2, 2026 / Rules and Regulations (c) Applicability This AD applies to certain Rolls-Royce Deutschland Ltd & Co KG Model Trent XWB– 75, Trent XWB–79, Trent XWB–79B, Trent XWB–84, and Trent XWB–97 engines, as identified in European Union Aviation Safety Agency (EASA) AD 2025–0128R1, dated June 17, 2025 (EASA AD 2025–0128R1). (d) Subject Joint Aircraft System Component (JASC) Code 7200, Engine (Turbine/Turboprop); 7310, Engine Fuel Distribution. (e) Unsafe Condition This AD was prompted by a report of damage to the main fuel hose assembly of the fuel manifold, which led to a controlled, temporary engine fire and heat damage to the exterior and interior of the engine nacelle (thrust reverser C-ducts), and resulted in a commanded in-flight engine shut down. The FAA is issuing this AD to prevent damage to the main fuel hose assembly of the fuel manifold. The unsafe condition, if not addressed, in combination with additional failures, could lead to an engine fire and result in damage to the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Except as specified in paragraphs (h) and (i) of this AD: Do all required actions within the compliance times specified in, and in accordance with, EASA AD 2025–0128R1. (h) Exceptions to EASA AD 2025–0128R1 (1) Where EASA AD 2025–0128R1 refers to its effective date, this AD requires using the effective date of this AD. (2) Where EASA AD 2025–0128R1 refers to September 1, 2024, this AD requires using the effective date of this AD. (3) Where EASA AD 2025–0128R1 refers to September 9, 2024 (the effective date of EASA Emergency AD 2024–0174–E), this AD requires using February 18, 2025 (the effective date of AD 2024–25–10). (4) Where EASA AD 2025–0128R1 refers to October 3, 2024 (the effective date of the original issue of EASA AD 2024–0182), this AD requires using the effective date of this AD. (5) Where EASA AD 2025–0128R1 refers to June 10, 2025 (the effective date of the EASA AD 2025–0128, dated June 3, 2025), this AD requires using the effective date of this AD. (6) Where EASA AD 2025–0128R1 refers to the applicable date listed in Appendix 1 of the Non-Modification Service Bulletin for Group B engines, this AD requires using the effective date of this AD. (7) Where EASA AD 2025–0128R1 states ‘‘engine flying hours (EFH)’’, this AD requires replacing that text with ‘‘engine flight hours (EFH)’’. (8) Where EASA AD 2025–0128R1 states ‘‘engine flying cycles (EFC)’’, this AD requires replacing that text with ‘‘engine flight cycles (EFC)’’. (9) This AD does not adopt the ‘‘Remarks’’ paragraph of EASA AD 2025–0128R1. (i) No Reporting Requirement Although EASA AD 2025–0128R1 specifies to submit certain information to the manufacturer, this AD does not include that requirement. (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 the 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 Barbara Caufield, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; 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 (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 2025–0128R1, dated June 17, 2025. (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 this material on the EASA website at ad.easa.europa.eu. (4) You may view this material at the FAA, 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-locations or email fr.inspection@nara.gov . Issued on June 18, 2026. Lona C. Saccomando, Acting Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service. [FR Doc. 2026–13481 Filed 7–1–26; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2025–3428; Project Identifier AD–2024–00428–T; Amendment 39–23389; AD 2026–13–07] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes AGENCY : Federal Aviation Administration (FAA), DOT. ACTION : Final rule. SUMMARY : The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787–8, 787–9, and 787–10 airplanes. This AD was prompted by reports of door assist handles pulled loose from their lower attach point in the doorway support bracket during pre-flight checks. This AD requires, for certain airplanes, installing a new retainer above the lower keyway of the support bracket assembly and installing a placard on certain support bracket assemblies or marking the part, and for certain airplanes, requires an inspection of the forward and aft door assist handles and applicable on-condition actions. For certain other airplanes, this AD requires installing a new retainer above the lower keyway of the support bracket assembly at certain locations and reidentifying the support bracket assembly. The FAA is issuing this AD to address the unsafe condition on these products. DATES : This AD is effective August 6, 2026. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 6, 2026. ADDRESSES : AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2025–3428; 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 Boeing material identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster VerDate Sep<11>2014 16:02 Jul 01, 2026 Jkt 268001 PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 E:\FR\FM\02JYR1.SGM 02JYR1 khammond on DSK9W7S144PROD with RULES