{"description":"Documents matching 'refers required actions compliance times'","count":10000,"total_pages":50,"next_page_url":"https://www.federalregister.gov/api/v1/documents?conditions%5Bterm%5D=refers+required+actions+compliance+times&format=json&page=2","results":[{"title":"Airworthiness Directives; Airbus Helicopters","type":"Rule","abstract":"The FAA is superseding Airworthiness Directive (AD) 2025-06-04 for all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. AD 2025-06-04 required repetitively inspecting the main gearbox (MGB) bevel wheel and the MGB magnetic plug for particles and performing corrective actions if applicable and prohibited installing an affected MGB unless certain requirements were met. Since the FAA issued AD 2025-06-04, the FAA determined that AD 2025-06-04 contains errors in the interval compliance times. This AD continues to require the actions of AD 2025-06-04 and corrects the interval compliance times. The FAA is issuing this AD to address the unsafe condition on these products.","document_number":"2026-11560","html_url":"https://www.federalregister.gov/documents/2026/06/09/2026-11560/airworthiness-directives-airbus-helicopters","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2026-06-09/pdf/2026-11560.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2026-11560.pdf?1780922718","publication_date":"2026-06-09","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"maintenance <span class=\"match\">actions</span> are necessary to improve detection of particles in the main gearbox (MGB) with certain part-numbered planet gear bearings installed. The FAA is issuing this AD to detect and correct particles in the MGB. The unsafe condition, if not addressed, could result in reduced or loss of control of the helicopter. \n (f) <span class=\"match\">Compliance</span> \n Comply with this AD within the <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified, unless already done. \n (g) <span class=\"match\">Required</span> <span class=\"match\">Actions</span> \n Except as specified in paragraphs (h) and (i) of this AD: Comply with all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> times"},{"title":"Airworthiness Directives; Airbus Helicopters","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2025-06-04, which applies to all Airbus Helicopters Model AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350D, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, EC130B4, and EC130T2 helicopters. AD 2025-06-04 requires repetitively inspecting the main gearbox (MGB) bevel wheel and the MGB magnetic plug for particles and performing corrective actions if applicable and prohibits installing an affected MGB unless certain requirements are met. Since the FAA issued AD 2025-06-04, the FAA determined that AD 2025-06-04 contains errors in the interval compliance times. This proposed AD would continue to require the actions of AD 2025-06-04 and revise the interval compliance times. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-20852","html_url":"https://www.federalregister.gov/documents/2025/11/25/2025-20852/airworthiness-directives-airbus-helicopters","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-11-25/pdf/2025-20852.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-20852.pdf?1763991917","publication_date":"2025-11-25","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"need comply only with that section. For example, where the AD requirement <span class=\"match\">refers</span> to “all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span>,” <span class=\"match\">compliance</span> with this AD requirement is not limited to the section titled “<span class=\"match\">Required</span> <span class=\"match\">Action</span>(s) and <span class=\"match\">Compliance</span> Time(s)” in EASA AD 2023-0044. Material <span class=\"match\">required</span> by EASA AD 2023-0044 for <span class=\"match\">compliance</span> will be available at \n www.regulations.gov \n by searching for and locating Docket No. FAA-2025-5032 after the FAA final rule is published.\n \n Costs of <span class=\"match\">Compliance</span> \n The FAA estimates that this AD, if adopted as proposed, would affect"},{"title":"Airworthiness Directives; The Boeing Company Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2013-08-15, which applies to certain The Boeing Company Model 737-800 series airplanes. AD 2013-08-15 requires repetitive inspections for cracking of the fuselage skin along chem-mill steps at certain crown skin and shear wrinkle areas and repair if necessary. Since the FAA issued AD 2013-08-15, the FAA has determined that the compliance times are not adequate. This proposed AD would continue to require the actions in AD 2013-08-15 but at reduced compliance times and would require post-modification inspections if an optional terminating action is accomplished. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-13714","html_url":"https://www.federalregister.gov/documents/2025/07/22/2025-13714/airworthiness-directives-the-boeing-company-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-07-22/pdf/2025-13714.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-13714.pdf?1753101910","publication_date":"2025-07-22","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"<span class=\"match\">ACTION</span>: \n Notice of proposed rulemaking (NPRM). \n \n \n SUMMARY: \n The FAA proposes to supersede Airworthiness Directive (AD) 2013-08-15, which applies to certain The Boeing Company Model 737-800 series airplanes. AD 2013-08-15 <span class=\"match\">requires</span> repetitive inspections for cracking of the fuselage skin along chem-mill steps at certain crown skin and shear wrinkle areas and repair if necessary. Since the FAA issued AD 2013-08-15, the FAA has determined that the <span class=\"match\">compliance</span> <span class=\"match\">times</span> are not adequate. This proposed AD would continue to <span class=\"match\">require</span> the <span class=\"match\">actions</span> in AD 2013-08-15"},{"title":"Airworthiness Directives; Airbus SAS Airplanes","type":"Rule","abstract":"The FAA is superseding Airworthiness Directive (AD) 2017-14- 14, which applied to all Airbus SAS Model A321-111, -112, -131, -211, - 212, -213, -231, and -232 airplanes. AD 2017-14-14 required repetitive inspections for cracking in the cabin floor beam junction at certain fuselage frame locations and repair if necessary. Since the FAA issued AD 2017-14-14, further analysis determined that the compliance times for the inspections must also be based on flight hours. This AD continues to require the actions in AD 2017-14-14, revises compliance times, and adds a provision for optional modifications. The FAA is issuing this AD to address the unsafe condition on these products.","document_number":"2025-16404","html_url":"https://www.federalregister.gov/documents/2025/08/27/2025-16404/airworthiness-directives-airbus-sas-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-08-27/pdf/2025-16404.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-16404.pdf?1756212320","publication_date":"2025-08-27","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"the airplane. \n (f) <span class=\"match\">Compliance</span> \n Comply with this AD within the <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified, unless already done. \n (g) Requirements \n Except as specified in paragraphs (h) and (i) of this AD: Comply with all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2024-0128, dated July 3, 2024 (EASA AD 2024-0128). \n (h) Exceptions to EASA AD 2024-0128 \n (1) Where EASA AD 2024-0128 <span class=\"match\">refers</span> to “13 June 2016 [the effective date of EASA AD 2016-0105],” this AD <span class=\"match\">requires</span> using August 23, 2017"},{"title":"Airworthiness Directives; The Boeing Company Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2013-08-16, which applies to certain The Boeing Company Model 737-700 and -700C series airplanes. AD 2013-08-16 requires repetitive inspections for cracking of the fuselage skin at certain locations at chem-mill areas and repair if necessary. Since the FAA issued AD 2013- 08-16, the FAA has determined that the compliance times are not adequate. This proposed AD would continue to require the actions in AD 2013-08-16 but at reduced compliance times and would require post- modification inspections if an optional modification is accomplished. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-13920","html_url":"https://www.federalregister.gov/documents/2025/07/24/2025-13920/airworthiness-directives-the-boeing-company-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-07-24/pdf/2025-13920.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-13920.pdf?1753274711","publication_date":"2025-07-24","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"applicable <span class=\"match\">times</span> specified in paragraph 1.E., “<span class=\"match\">Compliance</span>,” of Boeing Special Attention Service Bulletin 737-53-1310, Revision 1, dated May 22, 2024. \n (h) Exception to Service Bulletin Specifications \n Where the <span class=\"match\">Compliance</span> Time column in the tables under the “<span class=\"match\">Compliance</span>” paragraph of Boeing Special Attention Service Bulletin 737-53-1310, Revision 1, dated May 22, 2024, <span class=\"match\">refers</span> to the Revision 1 date of the service bulletin, this AD <span class=\"match\">requires</span> using the effective date of this AD. \n (i) Repair \n If any cracking is found during any inspection <span class=\"match\">required</span> by paragraph"},{"title":"Airworthiness Directives; The Boeing Company Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2017-19-26, which applies to certain The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes. AD 2017-19-26 requires repetitive inspections for cracks along the chem-milled steps of the fuselage skin and missing or loose fasteners in the area of the preventive modification or repairs; replacement of the time-limited repair with a permanent repair, if applicable; and applicable corrective actions that end certain repetitive inspections. AD 2017-19- 26 also requires repetitive inspections for modified airplanes. Since the FAA issued AD 2017-19-26, the FAA has determined that the compliance times are not adequate. This proposed AD would continue to require certain actions in AD 2017-19-26 but at reduced compliance times. This proposed AD would also revise instructions for the preventative modification and remove instructions for the permanent and time-limited repairs. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-20061","html_url":"https://www.federalregister.gov/documents/2025/11/18/2025-20061/airworthiness-directives-the-boeing-company-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-11-18/pdf/2025-20061.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-20061.pdf?1763387120","publication_date":"2025-11-18","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"AD. \n (2) Where the <span class=\"match\">Compliance</span> Time column in the tables under the “<span class=\"match\">Compliance</span>” paragraph of Boeing Alert Service Bulletin 737-53A1232, Revision 4, dated May 22, 2024, <span class=\"match\">refers</span> to the Revision 4 date of this service bulletin, this AD <span class=\"match\">requires</span> using the effective date of this AD. \n (3) For airplanes on which the <span class=\"match\">actions</span> specified in paragraph (g) of this AD are <span class=\"match\">required</span>: Inspections specified in table 1 of paragraph 1.E., “<span class=\"match\">Compliance</span>,” of Boeing Alert Service Bulletin 737-53A1232, Revision 4, dated May 22, 2024, are not <span class=\"match\">required</span> in areas that are spanned"},{"title":"Airworthiness Directives; The Boeing Company Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2013-08-11, which applies to certain The Boeing Company Model 737-900 and -900ER series airplanes. AD 2013-08-11 requires repetitive inspections for cracking of the fuselage skin along chem-mill steps at certain crown skin and shear wrinkle areas and repair if necessary. Since the FAA issued AD 2013-08-11, the FAA has determined that the compliance times are not adequate. This proposed AD would continue to require the actions in AD 2013-08-11 but at reduced compliance times and would require post-modification inspections if an optional modification is accomplished. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-11032","html_url":"https://www.federalregister.gov/documents/2025/06/16/2025-11032/airworthiness-directives-the-boeing-company-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-06-16/pdf/2025-11032.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-11032.pdf?1749818730","publication_date":"2025-06-16","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"proposed AD would <span class=\"match\">require</span> accomplishing the <span class=\"match\">actions</span> specified in the material already described, except for any differences identified as exceptions in the regulatory text of this proposed AD. For information on the procedures and <span class=\"match\">compliance</span> <span class=\"match\">times</span>, see this material at \n regulations.gov \n under Docket No. FAA-2025-1105.\n \n Costs of <span class=\"match\">Compliance</span> \n The FAA estimates that this AD, if adopted as proposed, would affect 56 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD: \n \n Estimated Costs \n \n <span class=\"match\">Action</span> \n Labor cost"},{"title":"Required Use by Foreign Applicants and Patent Owners of a Patent Practitioner","type":"Rule","abstract":"The United States Patent and Trademark Office (USPTO or Office) is amending the Rules of Practice in Patent Cases to require patent applicants and patent owners whose domicile is not located within the United States (U.S.) or its territories (hereinafter foreign applicants/inventors and patent owners) to be represented by a registered patent practitioner. A requirement that foreign applicants/ inventors and patent owners be represented by a registered patent practitioner will bring the U.S. in line with most other countries that require that such parties be represented by a licensed or registered person of that country. Additionally, this requirement will increase efficiency and enable the USPTO to more effectively use available mechanisms to enforce compliance by all foreign applicants/inventors and patent owners with U.S. statutory and regulatory requirements in patent matters, and enhance the USPTO's ability to respond to false certifications, misrepresentations, and fraud.","document_number":"2026-05564","html_url":"https://www.federalregister.gov/documents/2026/03/20/2026-05564/required-use-by-foreign-applicants-and-patent-owners-of-a-patent-practitioner","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2026-03-20/pdf/2026-05564.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2026-05564.pdf?1773924326","publication_date":"2026-03-20","agencies":[{"raw_name":"DEPARTMENT OF COMMERCE","name":"Commerce Department","id":54,"url":"https://www.federalregister.gov/agencies/commerce-department","json_url":"https://www.federalregister.gov/api/v1/agencies/54","parent_id":null,"slug":"commerce-department"},{"raw_name":"Patent and Trademark Office","name":"Patent and Trademark Office","id":402,"url":"https://www.federalregister.gov/agencies/patent-and-trademark-office","json_url":"https://www.federalregister.gov/api/v1/agencies/402","parent_id":54,"slug":"patent-and-trademark-office"}],"excerpts":" \n Pro se \n applications generally <span class=\"match\">require</span> additional processing by the OPAP because the application papers are often not in condition for publication, examination, or both. Additionally, \n pro se \n applications usually <span class=\"match\">require</span> patent examiners to spend additional examination time on procedural matters, thereby increasing overall patent application pendency. This final rule will help allocate USPTO resources to the merits of examination and, accordingly, decrease patent application processing <span class=\"match\">times</span>. <span class=\"match\">Requiring</span> foreign applicants/inventors and patent"},{"title":"Required Use by Foreign Applicants and Patent Owners of a Patent Practitioner","type":"Proposed Rule","abstract":"The United States Patent and Trademark Office (USPTO or Office) is proposing to amend the Rules of Practice in Patent Cases to require patent applicants and patent owners whose domicile is not located within the United States (U.S.) or its territories (hereinafter foreign applicants/inventors and patent owners) to be represented by a registered patent practitioner. A requirement that foreign applicants/ inventors and patent owners be represented by a registered patent practitioner would bring the United States in line with most other countries that require that such parties be represented by a licensed or registered person of that country. Additionally, this requirement would increase efficiency and enable the USPTO to more effectively use available mechanisms to enforce compliance by all foreign applicants/ inventors and patent owners with U.S. statutory and regulatory requirements in patent matters, and enhance the USPTO's ability to respond to false certifications, misrepresentations, and fraud.","document_number":"2025-23917","html_url":"https://www.federalregister.gov/documents/2025/12/29/2025-23917/required-use-by-foreign-applicants-and-patent-owners-of-a-patent-practitioner","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-12-29/pdf/2025-23917.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-23917.pdf?1766497523","publication_date":"2025-12-29","agencies":[{"raw_name":"DEPARTMENT OF COMMERCE","name":"Commerce Department","id":54,"url":"https://www.federalregister.gov/agencies/commerce-department","json_url":"https://www.federalregister.gov/api/v1/agencies/54","parent_id":null,"slug":"commerce-department"},{"raw_name":"United States Patent and Trademark Office","name":"Patent and Trademark Office","id":402,"url":"https://www.federalregister.gov/agencies/patent-and-trademark-office","json_url":"https://www.federalregister.gov/api/v1/agencies/402","parent_id":54,"slug":"patent-and-trademark-office"}],"excerpts":"applications generally <span class=\"match\">require</span> additional processing by the Office of Patent Application Processing because the application papers are often not in condition for publication, examination, or both. Additionally, \n pro se \n applications usually <span class=\"match\">require</span> patent examiners to spend examination time on procedural matters, thereby increasing overall patent application pendency. This proposed rule would help allocate USPTO resources to the merits of examination and, accordingly, decrease patent application processing <span class=\"match\">times</span>. <span class=\"match\">Requiring</span> foreign applicants/inventors"},{"title":"Airworthiness Directives; The Boeing Company Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2013-08-08, which applies to certain The Boeing Company Model 737-600 series airplanes. AD 2013-08-08 requires repetitive inspections for cracking of the fuselage skin at certain locations at chem-mill steps, and repair if necessary. AD 2013-08-08 also provides optional terminating action for the repetitive inspections. Since the FAA issued AD 2013-08-08, Boeing has reported that the compliance times are not adequate because new fleet data indicates that crack growth is faster and more distributed between tear straps, resulting in longer cracks than originally observed in the test data that prompted AD 2013-08-08. This proposed AD would continue to require the actions in AD 2013-08- 08, at reduced initial compliance times and repetitive intervals for the inspections, and mandate post-modification inspections if the optional modification is accomplished. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-09770","html_url":"https://www.federalregister.gov/documents/2025/05/30/2025-09770/airworthiness-directives-the-boeing-company-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-05-30/pdf/2025-09770.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-09770.pdf?1748522711","publication_date":"2025-05-30","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"\n This proposed AD would reduce the initial <span class=\"match\">compliance</span> <span class=\"match\">times</span> and repetitive intervals for the inspections. This proposed AD would also mandate the optional post-modification inspections (if the operator chooses to perform the optional modification). This proposed AD would <span class=\"match\">require</span> accomplishing the <span class=\"match\">actions</span> specified in the material already described, except for any differences identified as exceptions in the regulatory text of this proposed AD. \n \n For information on the procedures and <span class=\"match\">compliance</span> <span class=\"match\">times</span>, see this material at \n regulations.gov \n under"},{"title":"Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) Airplanes","type":"Rule","abstract":"The FAA is superseding Airworthiness Directive (AD) 2020-12- 12, which applied to all Embraer S.A. Model ERJ 170 airplanes and Model ERJ 190-100 STD, -100 LR, -100 ECJ, -100 IGW, -200 STD, -200 LR, and - 200 IGW airplanes. AD 2020-12-12 required repetitive detailed inspections for cracking of the engine inboard and outboard engine pylon lower link lugs, and repair if necessary. This AD continues to require the actions in AD 2020-12-12 with certain reduced compliance times. The FAA is issuing this AD to address the unsafe condition on these products.","document_number":"2025-13596","html_url":"https://www.federalregister.gov/documents/2025/07/21/2025-13596/airworthiness-directives-embraer-sa-type-certificate-previously-held-by-yabor-indstria-aeronutica-sa","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-07-21/pdf/2025-13596.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-13596.pdf?1752842709","publication_date":"2025-07-21","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"Comply with all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified in, and in accordance with, ANAC AD 2020-01-02R3. \n (h) Exceptions to ANAC AD 2020-01-02R3 \n (1) Where ANAC AD 2020-01-02R3 <span class=\"match\">refers</span> to “28 January 2020, the effective date of original revision of this AD,” this AD <span class=\"match\">requires</span> using August 13, 2020 (the effective date of AD 2020-12-12). \n (2) Where ANAC AD 2020-01-02R3 <span class=\"match\">refers</span> to “July 18, 2023, the effective date of AD 2020-01-02R1,” this AD <span class=\"match\">requires</span> using the effective date of this AD. \n (3) Where ANAC AD 2020-01-02R3 <span class=\"match\">refers</span> to its effective"},{"title":"Airworthiness Directives; Airbus SAS Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2017-14-14, which applies to all Airbus SAS Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. AD 2017-14-14 requires repetitive inspections for cracking in the cabin floor beam junction at certain fuselage frame locations, and repair if necessary. Since the FAA issued AD 2017-14-14, further analysis determined that the compliance times for the inspections must also be based on flight hours. This proposed AD would continue to require the actions in AD 2017-14-14, and would require revised compliance times and add a provision for optional modifications, 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.","document_number":"2025-03159","html_url":"https://www.federalregister.gov/documents/2025/02/27/2025-03159/airworthiness-directives-airbus-sas-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-02-27/pdf/2025-03159.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-03159.pdf?1740577511","publication_date":"2025-02-27","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"therefore, <span class=\"match\">require</span> <span class=\"match\">compliance</span> with EASA AD 2024-0128 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 2024-0128 does not mean that operators need comply only with that section. For example, where the AD requirement <span class=\"match\">refers</span> to “all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span>,” <span class=\"match\">compliance</span> with this AD requirement is not limited to the section titled “<span class=\"match\">Required</span> <span class=\"match\">Action</span>(s) and <span class=\"match\">Compliance</span> Time(s)”"},{"title":"Airworthiness Directives; Airbus SAS Airplanes","type":"Rule","abstract":"The FAA is superseding Airworthiness Directive (AD) 2022-15- 05, which applied to certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. AD 2022-15-05 required repetitive high frequency eddy current (HFEC) inspections for cracks on the web horizontal flange and inner cap, and applicable corrective actions. Since the FAA issued AD 2022-15-05, additional cracks have been found at the door stop fitting number 1 holes at frame (FR) 68, after disassembly of the door stop fitting as part of the inspections required by AD 2022-15-05. This AD continues to require the actions in AD 2022-15-05, but with reduced compliances times for some inspections, and requires an additional inspection at door stop fitting number 1. The FAA is issuing this AD to address the unsafe condition on these products.","document_number":"2025-22348","html_url":"https://www.federalregister.gov/documents/2025/12/09/2025-22348/airworthiness-directives-airbus-sas-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-12-09/pdf/2025-22348.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-22348.pdf?1765201527","publication_date":"2025-12-09","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"\n (f) <span class=\"match\">Compliance</span> \n Comply with this AD within the <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified, unless already done. \n (g) Requirements \n Except as specified in paragraphs (h) and (i) of this AD: Comply with all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified in, and in accordance with, EASA AD 2024-0210. \n (h) Exceptions to EASA AD 2024-0210 \n (1) Where EASA AD 2024-0210 <span class=\"match\">refers</span> to “22 November 2021 [the effective date of EASA AD 2021-0242]”, this AD <span class=\"match\">requires</span> using August 31, 2022 (the effective date of AD 2022-15-05). \n (2) Where EASA AD 2024-0210 <span class=\"match\">refers</span> to its"},{"title":"Trichloroethylene; Regulation Under the Toxic Substances Control Act (TSCA); Compliance Date Extension","type":"Rule","abstract":"The Environmental Protection Agency (EPA or Agency) is taking interim final action on the Regulation of Trichloroethylene (TCE) under the Toxic Substances Control Act (TSCA) to revise certain compliance deadlines finalized in 2024. Specifically, EPA is amending the prohibition compliance date for the use of TCE as a processing aid in the manufacture of nuclear fuel, with corresponding changes to the compliance dates for the manufacturing, processing and distribution in commerce of TCE to support such use, to a prohibition on September 15, 2028. EPA is also amending the prohibition compliance date for the disposal of TCE to wastewater by processors of TCE and processors and industrial and commercial users of TCE as a processing aid, to begin on December 18, 2026. EPA is also amending the compliance deadline for downstream notification, and the text required to be present in Safety Data Sheets, to accurately reflect the new prohibition compliance deadline for TCE used as a processing aid in the manufacture of nuclear fuel. EPA is amending this compliance deadline to allow for 90 days after the publication of the final rule for manufacturers, processors, and distributors in commerce of TCE to make such a change. These revisions are necessary to address new information presented to EPA about inadvertent oversights in the original rulemaking and serious concerns that the facilities at issue will be unable to comply with the relevant requirements by the existing deadlines. EPA is requesting comments on all aspects of this interim final rule and will consider all comments received in determining whether amendments to this rule are appropriate after the conclusion of the comment period.","document_number":"2025-17948","html_url":"https://www.federalregister.gov/documents/2025/09/17/2025-17948/trichloroethylene-regulation-under-the-toxic-substances-control-act-tsca-compliance-date-extension","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-09-17/pdf/2025-17948.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-17948.pdf?1757967310","publication_date":"2025-09-17","agencies":[{"raw_name":"ENVIRONMENTAL PROTECTION AGENCY","name":"Environmental Protection Agency","id":145,"url":"https://www.federalregister.gov/agencies/environmental-protection-agency","json_url":"https://www.federalregister.gov/api/v1/agencies/145","parent_id":null,"slug":"environmental-protection-agency"}],"excerpts":"Specifically, there is insufficient time before the September 15, 2025, <span class=\"match\">compliance</span> dates to address the new information submitted by petitioners on <span class=\"match\">compliance</span> difficulties absent immediate <span class=\"match\">action</span>. It is urgent to address these <span class=\"match\">compliance</span> difficulties because of the expected negative consequences. Although the information available to EPA at the time of rulemaking indicated that the manufacture of nuclear fuel either did not involve TCE or did not <span class=\"match\">require</span> an extended <span class=\"match\">compliance</span> deadline to avoid disruption to national security and critical infrastructure"},{"title":"Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) Airplanes","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2020-12-12, which applies to all Embraer S.A. Model ERJ 170 airplanes and Model ERJ 190-100 STD, -100 LR, -100 ECJ, -100 IGW, -200 STD, -200 LR, and -200 IGW airplanes. AD 2020-12-12 requires repetitive detailed inspections for cracking of the engine inboard and outboard engine pylon lower link lugs, and repair if necessary. Since the FAA issued AD 2020-12-12, it was determined that certain compliance times must be reduced. This proposed AD would continue to require the actions in AD 2020-12-12, with revised compliance times, as specified in an Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2025-02244","html_url":"https://www.federalregister.gov/documents/2025/02/07/2025-02244/airworthiness-directives-embraer-sa-type-certificate-previously-held-by-yabor-indstria-aeronutica-sa","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-02-07/pdf/2025-02244.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-02244.pdf?1738849508","publication_date":"2025-02-07","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"This proposed AD would retain all requirements of AD 2020-12-12, at revised <span class=\"match\">compliance</span> <span class=\"match\">times</span>. This proposed AD would <span class=\"match\">require</span> accomplishing the <span class=\"match\">actions</span> specified in ANAC AD 2020-01-02R3 described previously. \n \n This proposed AD would allow optional terminating <span class=\"match\">action</span> to revise certain operator maintenance documents to include new <span class=\"match\">actions</span> (\n e.g., \n inspections) and Critical Design Configuration Control Limitations (CDCCLs). <span class=\"match\">Compliance</span> with these <span class=\"match\">actions</span> and CDCCLs is <span class=\"match\">required</span> by 14 CFR 91.403(c). For airplanes that have been previously modified, altered"},{"title":"Investment Company Names Form N-PORT Reporting; Extension of Compliance Date","type":"Rule","abstract":"The Securities and Exchange Commission (the \"Commission\") is extending the compliance date for the amendments to Form N-PORT that were adopted on September 20, 2023 and relate to the rule under the Investment Company Act of 1940 (the \"Investment Company Act\") that addresses certain broad categories of investment company names that are likely to mislead investors about an investment company's investments and risks. The compliance dates for those Form N-PORT amendments are extended to November 17, 2027, for fund groups with net assets of $10 billion or more as of the end of their most recent fiscal year; and to May 18, 2028, for fund groups with less than $10 billion in net assets as of the end of their most recent fiscal year.","document_number":"2026-03459","html_url":"https://www.federalregister.gov/documents/2026/02/23/2026-03459/investment-company-names-form-n-port-reporting-extension-of-compliance-date","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2026-02-23/pdf/2026-03459.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2026-03459.pdf?1771595112","publication_date":"2026-02-23","agencies":[{"raw_name":"SECURITIES AND EXCHANGE COMMISSION","name":"Securities and Exchange Commission","id":466,"url":"https://www.federalregister.gov/agencies/securities-and-exchange-commission","json_url":"https://www.federalregister.gov/api/v1/agencies/466","parent_id":null,"slug":"securities-and-exchange-commission"}],"excerpts":"funds would incur costs to take <span class=\"match\">actions</span> to come into <span class=\"match\">compliance</span> with requirements that may change. Given the implementation activities associated with the upcoming <span class=\"match\">compliance</span> dates, a notice and comment period could not reasonably be completed prior to registered funds incurring burdens associated with meeting the <span class=\"match\">compliance</span> dates.\n 13 \n \n \n \n \n 13 \n  This rule does not <span class=\"match\">require</span> analysis under the Regulatory Flexibility Act. \n See \n 5 U.S.C. 604(a) (<span class=\"match\">requiring</span> a final regulatory flexibility analysis only for rules <span class=\"match\">required</span> by the APA or other law to undergo"},{"title":"Jurisdictional Separations and Referral to the Federal-State Joint Board","type":"Rule","abstract":"In this document, the Federal Communications Commission (Commission) extends, for up to an additional six years, the freeze of the jurisdictional separations category relationships and cost allocation factors (together, separations rules) for rate-of-return incumbent local exchange carriers (LECs). Further extending the freeze, which is set to expire on December 31, 2024, will enable the Commission to continue to work with the Federal-State Joint Board on Jurisdictional Separations (Joint Board) to determine the future of these rules. The Commission declines to provide carriers an opportunity to unfreeze their current category relationships and refers to the Joint Board to consider whether comprehensive reform is needed at this time or if the Commission should allow these rules to become obsolete over time and whether a permanent freeze is warranted, and if so, whether carriers still using separations should be given the chance to unfreeze their category relationships every few years.","document_number":"2024-27480","html_url":"https://www.federalregister.gov/documents/2024/11/25/2024-27480/jurisdictional-separations-and-referral-to-the-federal-state-joint-board","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2024-11-25/pdf/2024-27480.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2024-27480.pdf?1732283123","publication_date":"2024-11-25","agencies":[{"raw_name":"FEDERAL COMMUNICATIONS COMMISSION","name":"Federal Communications Commission","id":161,"url":"https://www.federalregister.gov/agencies/federal-communications-commission","json_url":"https://www.federalregister.gov/api/v1/agencies/161","parent_id":null,"slug":"federal-communications-commission"}],"excerpts":"Further Notice of Proposed Rulemaking, the Commission renewed the prior <span class=\"match\">referrals</span> to the Joint Board, including both the 1997 and 2009 comprehensive reform <span class=\"match\">referrals</span> and the 2018 interim reform measures <span class=\"match\">referral</span>. The Commission explained that it renewed these <span class=\"match\">referrals</span> in light of the need to achieve reform of the separations rules, given their declining applicability as a result of substantial telecommunications market and federal-state regulatory framework changes since these <span class=\"match\">referrals</span> were first made. \n \n 13. Four of the five parties that filed comments"},{"title":"Unsafe or Unsound Practices, Matters Requiring Attention","type":"Proposed Rule","abstract":"The Office of the Comptroller of the Currency (OCC) and the Federal Deposit Insurance Corporation (FDIC) propose to define the term \"unsafe or unsound practice\" for purposes of section 8 of the Federal Deposit Insurance Act and to revise the supervisory framework for the issuance of matters requiring attention and other supervisory communications.","document_number":"2025-19711","html_url":"https://www.federalregister.gov/documents/2025/10/30/2025-19711/unsafe-or-unsound-practices-matters-requiring-attention","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-10-30/pdf/2025-19711.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-19711.pdf?1761741908","publication_date":"2025-10-30","agencies":[{"raw_name":"DEPARTMENT OF THE TREASURY","name":"Treasury Department","id":497,"url":"https://www.federalregister.gov/agencies/treasury-department","json_url":"https://www.federalregister.gov/api/v1/agencies/497","parent_id":null,"slug":"treasury-department"},{"raw_name":"Office of the Comptroller of the Currency","name":"Comptroller of the Currency","id":80,"url":"https://www.federalregister.gov/agencies/comptroller-of-the-currency","json_url":"https://www.federalregister.gov/api/v1/agencies/80","parent_id":497,"slug":"comptroller-of-the-currency"},{"raw_name":"FEDERAL DEPOSIT INSURANCE CORPORATION","name":"Federal Deposit Insurance Corporation","id":164,"url":"https://www.federalregister.gov/agencies/federal-deposit-insurance-corporation","json_url":"https://www.federalregister.gov/api/v1/agencies/164","parent_id":null,"slug":"federal-deposit-insurance-corporation"}],"excerpts":" a matter <span class=\"match\">requiring</span> attention.\n \n \n (d) \n Tailored application <span class=\"match\">required</span>. \n The OCC will tailor its supervisory and enforcement <span class=\"match\">actions</span> under 12 U.S.C. 1818 and issuance of matters <span class=\"match\">requiring</span> attention based on the capital structure, riskiness, complexity, activities, asset size and any financial risk-related factor that the OCC deems appropriate. Tailoring <span class=\"match\">required</span> by this paragraph (d) includes tailoring with respect to the requirements or expectations set forth in such <span class=\"match\">actions</span> as well as whether, and the extent to which, such <span class=\"match\">actions</span> are taken"},{"title":"Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines","type":"Proposed Rule","abstract":"The FAA proposes to supersede Airworthiness Directive (AD) 2020-06-16, which applies to certain Rolls-Royce Deutschland Ltd & Co KG (RRD) Model RB211 Trent 768-60, 772-60, and 772B-60 engines. AD 2020-06-16 requires initial and repetitive ultrasonic inspections (UIs) of the affected low-pressure compressor (LPC) blades and, depending on the results of the UIs, replacement with a part eligible for installation. Since the FAA issued AD 2020-06-16, RRD issued updated service material providing improvements to the ultrasonic inspection procedures and updated initial inspection compliance times. This proposed AD would continue to require initial and repetitive UIs of the affected LPC blades for sub-surface anomalies and, depending on the results of the UIs, replacement with a part eligible for installation. The FAA is proposing this AD to address the unsafe condition on these products.","document_number":"2026-04148","html_url":"https://www.federalregister.gov/documents/2026/03/03/2026-04148/airworthiness-directives-rolls-royce-deutschland-ltd-and-co-kg-engines","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2026-03-03/pdf/2026-04148.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2026-04148.pdf?1772459109","publication_date":"2026-03-03","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"operators need comply only with that section. For example, where the AD requirement <span class=\"match\">refers</span> to “all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span>,” <span class=\"match\">compliance</span> with this AD requirement is not limited to the section titled “<span class=\"match\">Required</span> <span class=\"match\">Action</span>(s) and <span class=\"match\">Compliance</span> Time(s)” in EASA AD 2025-0144. Material <span class=\"match\">required</span> in EASA AD 2025-0144 for <span class=\"match\">compliance</span> will be available at \n regulations.gov \n under Docket No. FAA-2026-2287 after the FAA final rule is published.\n \n Costs of <span class=\"match\">Compliance</span> \n The FAA estimates that this AD, if adopted as proposed, would affect 140 engines installed"},{"title":"Airworthiness Directives; Airbus SAS Airplanes","type":"Rule","abstract":"The FAA is superseding Airworthiness Directive (AD) 2021-25- 14, which applied to all Airbus SAS Model A319-111, -112, -113, -114, - 115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, - 212, -213, -231, and -232 airplanes. AD 2021-25-14 required repetitive inspections for cracking at the wing manhole access panel attachment holes at certain wing skin panels, and corrective action if necessary. Since the FAA issued AD 2021-25-14, new investigation results determined that additional airplanes are subject to the unsafe condition and certain structural repair manual (SRM) tasks should not be used to accomplish repairs. This AD continues to require the actions in AD 2021-25-14. This AD also changes the applicability to both add and remove airplane models, updates the compliance times, and prohibits the use of certain SRM tasks for repair. The FAA is issuing this AD to address the unsafe condition on these products.","document_number":"2025-12894","html_url":"https://www.federalregister.gov/documents/2025/07/10/2025-12894/airworthiness-directives-airbus-sas-airplanes","pdf_url":"https://www.govinfo.gov/content/pkg/FR-2025-07-10/pdf/2025-12894.pdf","public_inspection_pdf_url":"https://public-inspection.federalregister.gov/2025-12894.pdf?1752065123","publication_date":"2025-07-10","agencies":[{"raw_name":"DEPARTMENT OF TRANSPORTATION","name":"Transportation Department","id":492,"url":"https://www.federalregister.gov/agencies/transportation-department","json_url":"https://www.federalregister.gov/api/v1/agencies/492","parent_id":null,"slug":"transportation-department"},{"raw_name":"Federal Aviation Administration","name":"Federal Aviation Administration","id":159,"url":"https://www.federalregister.gov/agencies/federal-aviation-administration","json_url":"https://www.federalregister.gov/api/v1/agencies/159","parent_id":492,"slug":"federal-aviation-administration"}],"excerpts":"structural integrity of the wings. \n (f) <span class=\"match\">Compliance</span> \n Comply with this AD within the <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified, unless already done. \n (g) Requirements \n Except as specified in paragraphs (h) and (i) of this AD: Comply with all <span class=\"match\">required</span> <span class=\"match\">actions</span> and <span class=\"match\">compliance</span> <span class=\"match\">times</span> specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2024-0230, dated December 2, 2024 (EASA AD 2024-0230). \n (h) Exceptions to EASA AD 2024-0230 \n (1) Where EASA AD 2024-0230 <span class=\"match\">refers</span> to its effective date, this AD <span class=\"match\">requires</span> using the effective date of this AD"}]}