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2025-02-04: Time Limits/Maintenance Checks

FAA order 2025-02-04 is an airworthiness directive in force since March 17, 2025. The FAA's subject line: Time Limits/Maintenance Checks. It names Airbus A319, Airbus A320, Airbus A321: about 2,057 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Airbus SAS
Models
A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A319-151N, A319-153N, A319-171N, A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, A320-233, A320-251N, A320-252N, A320-253N, A320-271N, A320-272N, A320-273N, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231, A321-232, A321-251N, A321-252N, A321-253N, A321-271N, A321-272N, A321-251NX, A321-252NX, A321-253NX, A321-271NX, A321-272NX
On this site
Airbus A319 329 registered
Airbus A320 792 registered
Airbus A321 936 registered

Dates and paperwork

In force since
March 17, 2025
Published
February 10, 2025 (signed January 15, 2025)
Docket
FAA-2024-2323
Replaces
2022-22-10
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is superseding Airworthiness Directive (AD) 2022-22- 10, which applied to certain Airbus SAS Model A318, A319, A320, and A321 series airplanes. AD 2022-22-10 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require certain actions in AD 2022- 22-10 and requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (9,181 characters)
1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by: a. Removing Airworthiness Directive (AD) 2022-22-10, Amendment 39-22225 (87 FR 72374, November 25, 2022); and b. Adding the following new AD: 2025-02-04 Airbus SAS: Amendment 39-22937; Docket No. FAA-2024-2323; Project Identifier MCAI-2024-00171-T. (a) Effective Date This airworthiness directive (AD) is effective March 17, 2025. (b) Affected ADs This AD replaces AD 2022-22-10, Amendment 39-22225 (87 FR 72374, November 25, 2022) (AD 2022-22-10). (c) Applicability This AD applies to Airbus SAS Model airplanes identified in paragraphs (c)(1) through (4) of this AD, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 6, 2023. (1) A318-111, -112, -121, and -122 airplanes. (2) A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, and -171N airplanes. (3) A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, and -272NX airplanes. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. (e) Unsafe Condition This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address failure of certain life-limited parts. The unsafe condition, if not addressed, could result in reduced structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Revision of the Existing Maintenance or Inspection Program, With a New Terminating Action This paragraph restates the requirements of paragraph (j) of AD 2022-22-10, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before February 2, 2022, 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 2022-0082, dated May 10, 2022 (EASA AD 2022-0082). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph. (h) Retained Exceptions to EASA AD 2022-0082, With No Changes This paragraph restates the exceptions specified in paragraph (k) of AD 2022-22-10, with no changes. (1) Where EASA AD 2022-0082 refers to its effective date, this AD requires using December 30, 2022 (the effective date of AD 2022-22-10). (2) The requirements specified in paragraph (1) of EASA AD 2022-0082 do not apply to this AD. (3) Paragraph (2) of EASA AD 2022-0082 specifies revising "the approved 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 December 30, 2022 (the effective date of AD 2022-22-10). (4) The initial compliance time for doing the tasks specified in paragraph (2) of EASA AD 2022-0082 is at the applicable "limitations" as incorporated by the requirements of paragraph (2) of EASA AD 2022-0082, or within 90 days after December 30, 2022 (the effective date of AD 2022-22-10), whichever occurs later. (5) The provisions specified in paragraphs (3) and (4) of EASA AD 2022-0082 do not apply to this AD. (6) The "Remarks" section of EASA AD 2022-0082 does not apply to this AD. (i) Retained Restrictions on Alternative Actions and Intervals, With a New Exception This paragraph restates the requirements of paragraph (l) of AD 2022-22-10, 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 2022-0082. (j) New Revision of the Existing Maintenance or Inspection Program 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 2024-0066, dated March 8, 2024 (EASA AD 2024-0066). Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the requirements of paragraph (g) of this AD. (k) Exceptions to EASA AD 2024-0066 (1) This AD does not adopt the requirements specified in paragraph (1) of EASA AD 2024-0066. (2) Paragraph (2) of EASA AD 2024-0066 specifies revising "the approved 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 the effective date of this AD. (3) The initial compliance time for doing the tasks specified in paragraph (2) of EASA AD 2024-0066 is at the applicable "limitations" as incorporated by the requirements of paragraph (2) of EASA AD 2024-0066, or within 90 days after the effective date of this AD, whichever occurs later. (4) This AD does not adopt the provisions specified in paragraphs (3) and (4) of EASA AD 2024-0066. (5) This AD does not adopt the "Remarks" section of EASA AD 2024-0066. (l) New Provisions for Alternative Actions and Intervals 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 provisions of the "Ref. Publications" section of EASA AD 2024-0066. (m) 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 Continued Operational Safety Branch, send it to the attention of the person identified in paragraph (n) of this AD and email to: [email protected]. (i) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (ii) AMOCs approved previously for AD 2022-22-10 are approved as AMOCs for the corresponding provisions of EASA AD 2022-0082 that are required by paragraph (g) of this AD. (iii) AMOCs approved previously for AD 2022-22-10 are approved as AMOCs for the corresponding provisions of EASA AD 2024-0066 that are required by paragraph (j) of this AD. (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. (n) Additional Information For more information about this AD, contact Timothy Dowling, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 206-231-3367; email: [email protected]. (o) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) 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. (3) The following material was approved for IBR on March 17, 2025. (i) European Union Aviation Safety Agency (EASA) AD 2024-0066, dated March 8, 2024. (ii) [Reserved] (4) The following material was approved for IBR on December 30, 2022 (87 FR 72374, November 25, 2022). (i) EASA AD 2022-0082, dated May 10, 2022. (ii) [Reserved] (5) For EASA material identified in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email [email protected]; website easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. (6) 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. (7) 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 [email protected]. Issued on January 15, 2025. Suzanne Masterson, Deputy Director, Integrated Certificate Management Division, Aircraft Certification Service. [FR Doc. 2025-02375 Filed 2-7-25; 8:45 am]BILLING CODE 4910-13-P

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Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/2025-02-04.json · aircraft systems.