FAA-2025-10316

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-2024-1301; Project Identifier AD-2024-00035-T; Amendment 39-23001; AD 2025-06-13] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. SUMMARY: The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register . The AD applies to certain The Boeing Company Model 787-9 and 787-10 airplanes. As published, a reference to the Alternative Methods of Compliance (AMOCs) paragraph in the regulatory text is incorrect. This document corrects that error. In all other respects, the original document remains the same. DATES: This correction is effective July 2, 2025. The effective date of AD 2025-06-13 remains July 2, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 2, 2025 (90 FR 22442, May 28, 2025). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov by searching for and locating Docket No. FAA-2024-1301; 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 street address for Docket Operations is listed above. Material Incorporated by Reference: • For Boeing material identified in this AD, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; websitemyboeingfleet.com. • 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 under Docket No. FAA-2024-1301. FOR FURTHER INFORMATION CONTACT: Joseph Hodgin, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3962; email: Joseph.J.Hodgin@faa.gov. SUPPLEMENTARY INFORMATION: Background AD 2025-06-13, Amendment 39-23001 (90 FR 22442, May 28, 2025) (AD 2025-06-13), requires replacing the incorrectly manufactured floor beam side-of-body fittings, inspecting the fuselage frame and fastener holes for damage, and repairing any damage for certain The Boeing Company Model 787-9 and 787-10 airplanes. For some repairs, AD 2025-06-13 requires using a method approved in accordance with the FAA's AMOC procedures. Need for Correction As published, a reference to the AMOC paragraph in the regulatory text of AD 2025-06-13 is incorrect. Paragraph (h)(2) of AD 2025-06-13 inadvertently referred to paragraph (i) of ( printed page 24063) the AD (“Credit for Previous Actions”) instead of paragraph (j) of the AD (“Alternative Methods of Compliance (AMOCs)”). Material Incorporated by Reference Under…

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