FAA-2026-09171

Document Headings Document headings vary by document type but may contain the following: • the agency or agencies that issued and signed a document • the number of the CFR title and the number of each part the document amends, proposes to amend, or is directly related to • the agency docket number / agency internal file number • the RIN which identifies each regulatory action listed in the Unified Agenda of Federal Regulatory and Deregulatory Actions See the Document Drafting Handbook for more details. Department of Transportation Federal Aviation Administration • 14 CFR Part 39 • [Docket No. FAA-2026-3871; Project Identifier MCAI-2026-00247-T; Amendment 39-23327; AD 2026-09-06] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A319-153N airplanes; Model A320-251N, -252N, and -271N airplanes; and Model A321-251NX, -252NX, -271NX and -272NX airplanes. This AD was prompted by an Airbus supplier identifying a quality issue in production, which could result in potential deviations from the specified thickness of various fuselage panels. This AD requires, for certain airplanes, doing a “local thickness mapping,” doing applicable additional instructions, a general visual inspection (GVI) of certain forward fuselage panels, a full panel thickness measurement, and applicable corrective actions. This AD also requires, for all airplanes, a dispatch restriction from using certain master minimum equipment list (MMEL) items, a prohibition to use certain structural repair manual (SRM) tasks. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective May 26, 2026. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of May 26, 2026. The FAA must receive comments on this AD by June 22, 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. ( printed page 25099) AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-3871; 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; telephone +49 221 8999 000; emailADs@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, 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 atregulations.gov …

Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.