Airworthiness Directive · Amendment 39-23256 · Time limits/maintenance checks
Airbus SAS Airplanes
This AD applies to Airbus SAS Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, -343, -841, and -941 airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 1, 2024.
The FAA is superseding Airworthiness Directive (AD) 2024-08- 05, which applied to certain Airbus SAS Model A330-200, A330-200 Freighter, and A330-300 series airplanes; and Model A330-841 and A330- 941 airplanes. AD 2024-08-05 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2024-08- 05, the FAA has determined that additional new and more restrictive airworthiness limitations are necessary. This AD continues to require certain actions in AD 2024-08-05 until the existing maintenance or inspection program, as applicable, is revised to incorporate the new and more restrictive airworthiness limitations. The FAA is issuing this AD to address the unsafe condition on these products.
This paragraph restates the requirements of paragraph (p) of AD 2024-08-05, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before October 2, 2023: 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 2023-0199, dated November 17, 2023 (EASA AD 2023-0199). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph.
This paragraph restates the requirements of paragraph (q) of AD 2024-08-05, with no changes.
(1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2023-0199.
(2) Paragraph (3) of EASA AD 2023-0199 specifies revising “the AMP” within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, within 90 days after July 19, 2024 (the effective date of AD 2024-08-05).
(3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2023-0199 is at the applicable “associated thresholds” as incorporated by the requirements of paragraph (3) of EASA AD 2023-0199, or within 90 days after July 19, 2024 (the effective date of AD 2024-08-05), whichever occurs later.
(4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2023-0199.
(5) This AD does not adopt the “Remarks” section of EASA AD 2023-0199.
(6) Where the service information referenced in EASA AD 2023-0199 specifies the compliance time for tasks 282400-G0001-1-C and 282400-P0001-1-C as “24 Months from the Effective Date of the EASA Airworthiness Directive that is expected to be issued to mandate this change, without exceeding the current 29,000 FH,” this AD requires using within 24 months after July 19, 2024 (the effective date of AD 2024-08-05), without exceeding the current 29,000 flight hour interval.
This paragraph restates the requirements of paragraph (r) of AD 2024-08-05, with a new exception. Except as required by paragraph (j) of this AD, after the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are approved as specified in the provisions of the “Ref. Publications” section of EASA AD 2023-0199.
Except as specified in paragraph (k) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2025-0012, dated January 13, 2025 (EASA AD 2025-0012). Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the requirements of paragraphs (g) of this AD.
(1) This AD does not adopt paragraphs (1), (2), (4), and (5) of EASA AD 2025-0012.
(2) Where paragraph (3) of EASA AD 2025-0012 specifies revising “the AMP” within 12 months after its effective date, this AD requires revising the existing maintenance or inspection program, as applicable, within 90 days after the effective date of this AD.
(3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2025-0012 is at the applicable “associated thresholds” as incorporated by the requirements of paragraph (3) of EASA AD 2025-0012, or within 90 days after the effective date of this AD, whichever occurs later.
(4) This AD does not adopt the “Remarks” section of EASA AD 2025-0012.
(5) Where the Compliance Time column of the table in the service information referenced in EASA AD 2025-0012 refers to “01 December 2025 (Corresponding to the 24 Months from the Effective Date of the EASA Airworthiness Directive No.: 2023-0199), without exceeding the current 29 000 FH,” this AD requires using within 24 months after July 19, 2024 (the effective date of AD 2024-08-05), without exceeding the current 29,000 flight hour interval.
(6) Where the Compliance Time column of the table in the material referenced in EASA AD 2025-0012 refers to “the Effective Date of the EASA Airworthiness Directive that is expected to be issued to mandate these changes,” this AD requires using the effective date of this AD.
After the existing maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections) and intervals are allowed unless they are approved as specified in the “Ref. Publications” section of EASA AD 2025-0012.
For Model A330-330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes: Accomplishing the actions required by paragraph (j) of this AD terminates the provisions in paragraphs (4) through (7) of EASA AD 2021-0281, dated December 17, 2021, that are required by paragraph (g) of AD 2022-17-08.
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 Continued Operational Safety Branch, send it to the attention of the person identified in paragraph (o) 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.
For more information about this AD, contact Frank Carreras, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 312-203-5670; email: Frank.Carreras@faa.gov.
