The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-200, -200 Freighter, -300, -800, and -900 series airplanes. This AD was prompted by the ...
[Docket No. FAA-2025-3988; Project Identifier MCAI-2025-00443-T; Amendment 39-23353; AD 2026-10-13]
RIN 2120-AA64
AGENCY:
Federal Aviation Administration (FAA), DOT.
ACTION:
Final rule.
SUMMARY:
The FAA is adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-200, -200 Freighter, -300, -800, and -900 series airplanes. This AD was prompted by the identification of an incorrect shot peening application implemented in production. This AD requires repetitive special detailed inspections (SDIs) of affected central windshield frames and applicable corrective actions. The FAA is issuing this AD to address the unsafe condition on these products.
DATES:
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.
ADDRESSES:
AD Docket:
You may examine the AD docket at
regulations.gov
under Docket No. FAA-2025-3988 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; 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
under Docket No. FAA-2025-3988.
FOR FURTHER INFORMATION CONTACT:
Nicholas Benson, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3647; email:
nicholas.h.benson@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
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 A330-200, -200 Freighter, -300, -800, and -900 series airplanes. The NPRM was published in the
Federal Register
on November 17, 2025 (90 FR 51222). The NPRM was prompted by AD 2025-0071, dated March 31, 2025 (EASA AD 2025-0071) (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 an incorrect shot peening application was implemented in production and the fatigue life of affected central windshield frames could consequently be lower than the certified value. This condition, if not addressed, could adversely affect the structural integrity of the airplane.
In the NPRM, the FAA proposed to require repetitive SDIs of affected central windshield frames and applicable corrective actions, as specified in EASA AD 2025-0071. The FAA is issuing this AD to address the unsafe condition on these products.
( printed page 31878)
You may examine the MCAI in the AD docket at
regulations.gov
under Docket No. FAA-2025-3988.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from Air Line Pilots Association, International (ALPA) who supported the NPRM without change.
The FAA received additional comments from the Citizens Rulemaking Alliance. The following presents the comments received on the NPRM and the FAA's response to each comment.
Request To Justify Forgoing Notice and Comment or Issue an NPRM
The Citizens Rulemaking Alliance requested that the FAA either provide its justification for finding good cause to bypass notice and comment procedures, or convert this action to an NPRM to extend the comment period at least 60 days. The commenter asserted the FAA has not adequately justified use of the good cause exemption.
The FAA notes the comment was submitted in response to an NPRM for which the FAA provided a 45-day comment period. This final rule is effective 35 days after its publication in the
Federal Register
. Therefore, no change to this AD is necessary.
Request To Comply With the Paperwork Reduction Act (PRA)
The Citizens Rulemaking Alliance requested that the FAA revise the AD to comply with the PRA if reporting is required or remove any reporting provisions until PRA requirements are satisfied. If reporting is not required, the commenter requested the FAA clarify that in the AD.
The FAA notes paragraph (i) of this AD specifies that reporting is not required. If an AD were to require reporting, the preamble of the AD would include a paragraph titled “Paperwork Reduction Act” that would provide the applicable OMB control number, required PRA statements, and the estimated time to collect the required information (burden). Any costs associated with the reporting requirement would be included in the Costs of Compliance section in the preamble of the AD. Therefore, the FAA did not change this AD as a result of this comment.
Request To Consider Impact on Small Entities
The Citizens Rulemaking Alliance requested that the FAA either provide the factual basis for its Regulatory Flexibility Act (RFA) certification that the AD will not have a significant economic impact on a substantial number of small entities, or prepare an initial regulatory flexibility analysis.
The FAA provides the following clarification. The RFA of 1980 (5 U.S.C. 601-612), as amended by the Small Business Regulatory Enforcement Fairness Act of 1996 (Pub. L. 104-121) and the Small Business Jobs Act of 2010 (Pub. L. 111-240), requires Federal agencies to consider the effects of the regulatory action on small business and other small entities and to minimize any significant economic impact. The term “small entities” comprises small businesses and not-for-profit organizations that are independently owned and operated and are not dominant in their fields, and governmental jurisdictions with populations of less than 50,000.
This AD will affect 11 domestic entities, of which three are small entities. The table below displays the industries of the small entities, their average annual revenue, and the AD's estimated cost burden relative to average annual revenue.
Number of Small Entities Affected by Industry and Cost Significance 1
NAICS
code
Description
Number of
airplanes
Average
annual
revenue
Cost per AD/
annual revenue
(%)
532411
Commercial Air, Rail, and Water Transportation Equipment Rental and Leasing
5
$1,007,000
0.17
532411
Commercial Air, Rail, and Water Transportation Equipment Rental and Leasing
5
3,960,000
0.00
481111
Scheduled Passenger Air Transportation
1
278,910
0.00
Total
11
1,748,637
0.06
1
Source: SBA (2023). NAICS (North American Industrial Classification System). Dun & Bradstreet. D&B Hoovers. Retrieved April 12, 2024.
https://app.hoovers.dnb.com/.
While the FAA has determined that this AD affects a number of small entities, the compliance cost of the AD relative to each small entity's annual revenue is minimal. The FAA estimates the total cost per affected airplane to be $340 (4 work-hours × $85 per work-hour). The total cost burden is less than 1 percent of average annual revenue for all small entities. Therefore, as provided in section 605(b), the FAA certifies this AD will not result in a significant economic impact on a substantial number of small entities. The FAA did not change this AD as a result of this comment.
Request To Provide Additional Cost Information
The Citizens Rulemaking Alliance requested that the FAA add to the AD docket the methodology and assumptions supporting the estimated cost of the proposed AD and reopen the comment period for public input on the additional cost information. The commenter stated that the FAA should also provide the fleet size, per airplane labor and parts cost, any assumed downtime or out-of-service impacts, aggregate costs, and any assumption that the manufacturer would provide parts free of charge.
In the Costs of Compliance section of the proposed AD, the FAA disclosed the number of airplanes affected on the U.S. registry, estimated number of work hours provided by the manufacturer, and the aggregate costs. The FAA did not disclose an estimated parts cost since this AD does not require any parts. Additionally, the FAA considered the impact that this AD will have on affected operators and determined this AD will not trigger any downtime costs because the requirements of this AD can be performed during regularly scheduled maintenance. Since the FAA has assessed and disclosed the total known costs of the AD requirements in the Costs of Compliance section of the proposed AD, and the commenter did not provide additional cost data for the FAA to consider in its cost analysis, it is not necessary to reopen the comment period or provide additional information in the AD docket. The FAA
( printed page 31879)
did not change this AD as a result of this comment.
Conclusion
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.
Material Incorporated by Reference Under 1 CFR Part 51
EASA AD 2025-0071 specifies procedures for repetitive SDIs (
i.e.,
high frequency eddy current inspections) for cracking of the windshield central lower framing fillet radius on the left-hand and right-hand sides and applicable corrective actions. Corrective actions include repair.
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.
Costs of Compliance
The FAA estimates that this AD affects 85 airplanes of U.S. registry. The FAA estimates the following total costs to comply with this AD:
Estimated Costs for Required Actions
Labor cost
Parts cost
Total cost
per product
Total cost on
U.S. operators
4 work-hours × $85 per hour = $340
$0
$340
$28,900
The FAA has received no definitive data on which to base the cost estimates for the on-condition repairs specified in this AD.
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
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:
(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.
This airworthiness directive (AD) is effective July 6, 2026.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus SAS airplanes identified in paragraphs (c)(1) through (5) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2025-0071, dated March 31, 2025 (EASA AD 2025-0071).
(1) Model A330-201, -202, -203, -223, and -243 airplanes.
(2) Model A330-223F and -243F airplanes.
(3) Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
(4) Model A330-841 airplanes.
(5) Model A330-941 airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
(e) Unsafe Condition
This AD was prompted by the identification of an incorrect shot peening application that was implemented in production. The FAA is issuing this AD to address the fatigue life of affected central windshield frames that might be lower than the certified value. This condition, if not addressed, could adversely affect the structural integrity of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Requirements
Except as specified in paragraphs (h) and (i) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2025-0071.
(h) Exceptions to EASA AD 2025-0071
(1) Where paragraph (2) of EASA AD 2025-0071 specifies if “any crack is found on an affected part, before next flight, contact Airbus for repair instructions and, within the compliance time specified in those instructions, accomplish those instructions accordingly.”, this AD requires replacing that text with “any cracking is found on an affected part, the cracking must be repaired before further flight using a method approved by the Manager, AIR-520, Continued Operational Safety Branch, FAA; or EASA; or Airbus SAS's EASA Design Organization
( printed page 31880)
Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.”
(2) This AD does not adopt the “Remarks” section of EASA AD 2025-0071.
(i) No Reporting Requirement
Although the material referenced in EASA AD 2025-0071 specifies to submit certain information to the manufacturer, this AD does not include that requirement.
(j) 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 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 the Operational Safety Branch, send it to the attention of the person identified in paragraph (k) 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 DOA. If approved by the DOA, the approval must include the DOA-authorized signature.
(3)
Required for Compliance (RC):
Except as required by paragraphs (i) and (j)(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.
(k) Additional Information
For more information about this AD, contact Nicholas Benson, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-3647; email:
nicholas.h.benson@faa.gov.
(l) 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 2025-0071, dated March 31, 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.
Use this for formal legal and research references to the published document.
91 FR 31877
Web Citation
Suggested Web Citation
Use this when citing the archival web version of the document.
“Airworthiness Directives; Airbus SAS Airplanes,” thefederalregister.org (May 29, 2026), https://thefederalregister.org/documents/2026-10802/airworthiness-directives-airbus-sas-airplanes.