AD 2026-10-17

This AD is effective July 6, 2026.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of July 6, 2026.

AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-2286; 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 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 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; email ADs@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 at regulations.gov under Docket No. FAA-2026-2286.

Camille L. Seay, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone 817-222-5149; email Camille.L.Seay@faa.gov.

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply 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. The NPRM was published in the Federal Register on March 10, 2026 (91 FR 11478). The NPRM was prompted by EASA AD 2025-0207R1, dated October 30, 2025 (EASA AD 2025-0207R1) (also referred to as the MCAI), issued by EASA, which is the Technical Agent for the Member States of the European Union. The MCAI states reports were received of broken bolts in the seat rail connections in the area of frame (FR) 47 (for Model A320 and A321 series airplanes), FR47/51 (for Model A319 series airplanes), FR47/54 (for Model A318 series airplanes), FR35 (for Model A318, A319, and A320 series airplanes), and FR35.8 (for A321 series airplanes), as applicable. This condition, if not corrected, could lead to seat detachment and passenger injuries under emergency landing loads.

In the NPRM, the FAA proposed to require replacement of the nylon bushes with bronze bushes in the affected areas and to prohibit the installation of affected parts in those areas, as specified in EASA AD 2025-0207R1. The FAA is issuing this AD to address the unsafe condition on these products.

You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA-2026-2286.

The FAA received a comment from the Airline Pilots Association, International (ALPA) who supported the NPRM without change.

These products have been approved by the civil aviation authority 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 reviewed the relevant data, considered any comments received, and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products. Except for minor editorial changes, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator.

EASA AD 2025-0207R1 specifies procedures for replacement of the nylon bushes with bronze bushes in the affected areas. The replacement includes doing a rotating probe inspection of the fastener holes for cracking, checking the hole diameter of the bracket assemblies, seat track, and long beam, as applicable, to determine if it is within tolerance, checking the inner diameter of the bushing to determine if it is within tolerance, and contacting the manufacturer for repair instructions and doing the repair. EASA AD 2025-0207R1 also prohibits the installation of affected parts in those areas. 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.

The FAA estimates that this AD affects 1,404 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:

The FAA has received no definitive data on which to base the cost estimates for the on-condition repairs specified in this AD.

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.

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,

(2) Will not affect intrastate aviation in Alaska, and

(3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by adding the following new airworthiness directive: