FAA Proposes Airworthiness Directive Superseding AD 2025-10-12 for Airbus Aircraft

Proposed Rule

Airworthiness Directives; Airbus SAS Airplanes

A Proposed Rule by the Federal Aviation Administration on 04/10/2026

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• Public Inspection Published Document: 2026-06980 (91 FR 18333) Document Headings ###### Department of Transportation

Federal Aviation Administration

1. 14 CFR Part 39
2. [Docket No. FAA-2026-3480; Project Identifier MCAI-2025-01031-T]
3. RIN 2120-AA64

AGENCY:

Federal Aviation Administration (FAA), DOT.

ACTION:

Notice of proposed rulemaking (NPRM).

SUMMARY:

The FAA proposes to supersede Airworthiness Directive (AD) 2025-10-12, which applies to all Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320 series airplanes; Model A321-211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -272N, and -272NX airplanes; Airbus SAS Model A330-200 series airplanes; Model A330-300 series airplanes; Model A330-800 series airplanes; Model A330-900 series ( printed page 18334) airplanes; Model A350-941 and -1041 airplanes; and Model A380-800 series airplanes. AD 2025-10-12 requires repetitive general visual inspections of the broadband antenna adapter plate, skirt, vents, and attachment fittings, and applicable corrective actions, and limits the installation of affected parts under certain conditions. Since the FAA issued AD 2025-10-12, a new Model A321-271NY airplanes has been certified, on which the affected parts could be installed in service. This proposed AD continues to require the actions in AD 2025-10-12 and would add Model A321-271NY airplanes to the applicability. This proposed AD would also prohibit the installation of affected parts under certain conditions. The FAA is proposing this AD to address the unsafe condition on these products.

DATES:

The FAA must receive comments on this proposed AD by May 26, 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. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-3480; 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 NPRM, 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; email ADs@easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. It is also available at regulations.gov under Docket No. FAA-2026-3480.
• 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.

FOR FURTHER INFORMATION CONTACT:

Bill Ashforth, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3520; email: Bill.Ashforth@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments using a method listed under the ADDRESSES section. Include “Docket No. FAA-2026-3480; Project Identifier MCAI-2025-01031-T” at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this proposal because of those comments.

Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this NPRM.

Confidential Business Information

CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this NPRM contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this NPRM, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as “PROPIN.” The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this NPRM. Submissions containing CBI should be sent to Bill Ashforth, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3520; email: Bill.Ashforth@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.

Background

The FAA issued AD 2025-10-12, Amendment 39-23046 (90 FR 22457, May 28, 2025) (AD 2025-10-12), for all Airbus SAS Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes; Model A321-211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -272N, and -272NX airplanes; Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, -343, -841, and -941 airplanes; Model A350-941 and -1041 airplanes; and Model A380-841, -842, and -861 airplanes. AD 2025-10-12 was prompted by an MCAI originated by EASA, which is the Technical Agent for the Member States of the European Union. EASA issued AD 2024-0199, dated October 18, 2024 (EASA AD 2024-0199), to correct an unsafe condition.

AD 2025-10-12 requires repetitive general visual inspections of the broadband antenna adapter plate, skirt, vents, and attachment fittings, and applicable corrective actions, and limits the installation of affected parts under certain conditions. The FAA issued AD 2025-10-12 to address the corrosion and cracks on the broadband antenna adapter plate and skirt assembly-adapter. The unsafe condition, if not addressed, could lead to in-flight detachment of the radome, antenna, and affected parts (e.g., the broadband antenna adapter plate, skirt, vents and attachment fittings), which could impact the tail section of the airplane, possibly resulting in damage and reduced control of the airplane.

Actions Since AD 2025-10-12 Was Issued

Since the FAA issued AD 2025-10-12, EASA superseded EASA AD 2024-0199 and issued EASA AD 2025-0120, dated May 26, 2025 (EASA AD 2025-0120) (also referred to as the MCAI), to correct an unsafe condition for all Airbus SAS Model:

• A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes;
• A320-211, -212, -214, -215, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes;
• A321-211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -271NY, -272N, and -272NX airplanes;
• A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, ( printed page 18335) -341, -342, -343, -841, and -941 airplanes;
• A350-941 and -1041 airplanes; and
• A380-841, -842, and -861 airplanes. Model A320-215 airplanes are not certificated by the FAA and are not included on the U.S. type certificate data sheet; this AD therefore does not include those airplanes in the applicability.

The MCAI states a new Model, A321-271NY, has been certified, on which affected parts could be installed in service. Airbus has released Airbus Service Bulletin A320-44-1103 Revision 03, dated February 25, 2026, to include certain Model A321-271NY airplanes. EASA AD 2025-0120 is still considered to be an interim action, and further EASA AD action may follow.

The FAA is proposing 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-2026-3480.

Explanation of Retained Requirements

Although this proposed AD does not explicitly restate the requirements of AD 2025-10-12, this proposed AD would retain all of the requirements of AD 2025-10-12. Those requirements are referenced in EASA AD 2025-0120, which, in turn, is referenced in paragraph (g) of this proposed AD.

Material Incorporated by Reference Under 1 CFR Part 51

The FAA reviewed EASA AD 2025-0120, which specifies procedures for repetitive general visual inspections for cracks and corrosion of the broadband antenna adapter plate, skirt, vents, and attachment fittings, and, depending on findings, corrective actions including repair or replacement of the affected parts. EASA AD 2025-0120 also limits the installation of affected parts under certain conditions and requires reporting of both positive and negative inspection results after the initial inspection and thereafter reporting the positive inspection results after each subsequent inspection.

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.

FAA's Determination

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 is issuing this NPRM after determining that the unsafe condition described previously is likely to exist or develop in other products of the same type design.

Proposed AD Requirements in This NPRM

This proposed AD would require accomplishing the actions specified in EASA AD 2025-0120 described previously, except for any differences identified as exceptions in the regulatory text of this proposed AD.

Explanation of Required Compliance Information

In the FAA's ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, the FAA proposes to incorporate EASA AD 2025-0120 by reference in the FAA final rule. This proposed AD would, therefore, require compliance with EASA AD 2025-0120 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 2025-0120 does not mean that operators need comply only with that section. For example, where the AD requirement refers to “all required actions and compliance times,” compliance with this AD requirement is not limited to the section titled “Required Action(s) and Compliance Time(s)” in EASA AD 2025-0120. Material required by EASA AD 2025-0120 for compliance will be available at regulations.gov under Docket No. FAA-2026-3480 after the FAA final rule is published.

Interim Action

The FAA considers that this proposed AD would be an interim action. The FAA anticipates that further AD action will follow.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would affect 8 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD:

| Action | Labor cost | Parts cost | Cost per product | Cost on U.S.
operators |
| --- | --- | --- | --- | --- |
| Retained actions from AD 2025-10-12 (4 airplanes) | Up to 61 work-hours × $85 per hour = $5,185 | $0 | Up to $5,185 | Up to $20,740. |
| New proposed actions (4 airplanes) | Up to 61 work-hours × $85 per hour = $5,185 | 0 | Up to $5,185 | Up to $20,740. |
The FAA estimates the following costs to do any necessary on-condition action that would be required based on the results of any required actions. The FAA has no way of determining the number of aircraft that might need this on-condition action:

Labor cost	Parts cost	Cost per product
50 work-hours × $85 per hour = $4,250	$10,000	$14,250

( printed page 18336) The FAA has received no definitive data on which to base the cost estimates for the repairs specified in this proposed AD.

Paperwork Reduction Act

A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a currently valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to take approximately 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. All responses to this collection of information are mandatory. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to: Information Collection Clearance Officer, Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX 76177-1524.

Authority for This Rulemaking

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.

Regulatory Findings

The FAA determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 this proposed regulation:

(1) Is not a “significant regulatory action” under Executive Order 12866,

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

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

List of Subjects in 14 CFR Part 39

• Air transportation
• Aircraft
• Aviation safety
• Incorporation by reference
• Safety

The Proposed Amendment

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

PART 39—AIRWORTHINESS DIRECTIVES

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

Authority: 49 U.S.C. 106(g), 40113, 44701.

§ 39.13 [Amended] 2. The FAA amends § 39.13 by:

a. Removing Airworthiness Directive (AD) 2025-10-12, Amendment 39-23046 (90 FR 22457, May 28, 2025); and

b. Adding the following new AD:

Airbus SAS: Docket No. FAA-2026-3480; Project Identifier MCAI-025-01031-T.

(a) Comments Due Date

The FAA must receive comments on this airworthiness directive (AD) by May 26, 2026.

(b) Affected ADs

This AD replaces AD 2025-10-12, Amendment 39-23046 (90 FR 22457, May 28, 2025) (AD 2025-10-12).

(c) Applicability

This AD applies to all Airbus SAS airplanes specified in paragraphs (c)(1) through (6) of this AD, certificated in any category.

(1) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.

(2) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes.

(3) Model A321-211, -212, -213, -231, -232, -251N, -251NX, -252N, -252NX, -253N, -253NX, -253NY, -271N, -271NX, -271NY, -272N, and -272NX airplanes.

(4) Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, -343, -841, and -941 airplanes.

(5) Model A350-941 and -1041 airplanes.

(6) Model A380-841, -842, and -861 airplanes.

(d) Subject

Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Unsafe Condition

This AD was prompted by a report that found corrosion and cracks on the broadband antenna adapter plate during an inspection. The FAA is issuing this AD to address the corrosion and cracks on the broadband antenna adapter plate and skirt assembly-adapter. The unsafe condition, if not addressed, could lead to in-flight detachment of the radome, antenna, and affected parts, which could impact the tail section of the airplane, possibly resulting in damage and reduced control of the airplane.

(f) Compliance

Comply with this AD within the compliance times specified, unless already done.

(g) Requirements

Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2025-0120, dated May 26, 2025 (EASA AD 2025-0120).

(h) Exceptions to EASA AD 2025-0120

(1) Where Appendix A in “the applicable SB” identified in EASA AD 2025-0120 specifies a compliance time “from SB publication date” or “from 14 June 2024 [the effective date of the EASA AD 2024-0106],” this AD requires using July 2, 2025 (the effective date of AD 2025-10-12), except for Model A321-271NY airplanes this AD requires using the effective date of this AD.

(2) Where EASA AD 2025-0120 specifies “14 June 2024 [the effective date of EASA AD 2024-0106],” this AD requires using July 2, 2025 (the effective date of AD 2025-10-12), except for Model A321-271NY airplanes this AD requires using the effective date of this AD.

(3) This AD does not adopt the “Remarks” section of EASA AD 2025-0120.

(4) Where paragraph (2) of EASA AD 2025-0120 specifies “any crack and/or corrosion are detected on an affected part”, this AD requires replacing that text with “any crack or corrosion is detected on an affected part”.

(5) Paragraph (4) of EASA AD 2025-0120 specifies to report inspection results to Airbus within a certain compliance time. For this AD, report inspection results at the applicable time specified in paragraph (h)(5)(i) or (ii) of this AD.

(i) If the inspection was done on or after the effective date of this AD: Submit the report within 30 days after the inspection.

(ii) If the inspection was done before the effective date of this AD: Submit the report within 30 days after the effective date of this AD.

(i) Additional AD Provisions

The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, AIR-520, Continued Operational Safety Branch, FAA, has the authority to approve AMOCs for this AD, if ( printed page 18337) requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the manager of AIR-520, Continued Operational Safety Branch, send it to the attention of the person identified in paragraph (j) of this AD and email to: AMOC@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.

(2) Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, AIR-520, Continued Operational Safety Branch, FAA; or EASA; or Airbus SAS's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.

(3) Required for Compliance (RC): Except as required by paragraph (i)(2) of this AD, if any material contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC.

(j) Additional Information

For more information about this AD, contact Bill Ashforth, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3520; email: Bill.Ashforth@faa.gov.

(k) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this material as applicable to do the actions required by this AD, unless this AD specifies otherwise.

(i) European Union Aviation Safety Agency (EASA) AD 2025-0120, dated May 26, 2025.

(ii) [Reserved]

(3) For 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.

(4) 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.

(5) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/​federal-register/​cfr/​ibr-locations or email fr.inspection@nara.gov.

Issued on April 8, 2026.

Brian Knaup,

Acting Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service.

[FR Doc. 2026-06980 Filed 4-9-26; 8:45 am]

BILLING CODE 4910-13-P

Published Document: 2026-06980 (91 FR 18333)