FAA-2026-18423

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-2025-2555; Project Identifier AD-2025-00433-E; Amendment 39-23446; AD 2026-17-03] • RIN 2120-AA64 ( printed page 57491) 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 . That AD applies to certain International Aero Engines AG (IAE AG) Model V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines. As published, paragraph (g) of the regulatory text contains a typographical error. This document corrects that error. In all other respects, the original document remains the same. DATES: This correction is effective September 24, 2026. The effective date of AD 2026-17-03 remains September 24, 2026. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2025-2555; 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; correction, 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. FOR FURTHER INFORMATION CONTACT: Carol Nguyen, Aviation Safety Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone: (781) 238-7655; email: carol.nguyen@faa.gov. SUPPLEMENTARY INFORMATION: Background AD 2026-17-03, Amendment 39-23446 (91 FR 53713, August 20, 2026) (AD 2026-17-03), requires replacement of affected 3rd stage High Pressure Compressor (HPC) rotor blades with parts eligible for installation for certain IAE AG Model V2522-A5, V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, V2531-E5, and V2533-A5 engines. Need for the Correction As published, paragraph (g) of AD 2026-17-03 contains a typographical error. The word “blade” was inadvertently omitted from the final regulatory text. Paragraph (g) of AD 2026-17-03 should read, “. . . where the 3rd stage HPC rotor blade is exposed . . .,” which is consistent with the intent of the proposed AD (90 FR 51600, November 18, 2025). Correction of Publication This document corrects an error and correctly adds the AD as an amendment to 14 CFR 39.13. Although no other part of the preamble or regulatory information has been corrected, the FAA is publishing the entire rule in the Federal Register . The effective date of this AD remains September 24, 2026. Since this action only corrects the typographical error, it has no adverse economic impact and imposes no additional burden on any person. Therefore, the FAA has determined that notice and public procedures are unnecessary. List of Subjects in 14 CFR Part 39 • Air transportation • Aircraft • Aviation safety • Incorporation by reference • Safety Adoption of the…

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