2022-22-10: Time Limits/Maintenance Checks

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) 2020-21-11, Amendment 39-21284 (85 FR 65674, October 16, 2020); and b. Adding the following new AD: 2022-22-10 Airbus SAS: Amendment 39-22225; Docket No. FAA-2022-1066; Project Identifier MCAI-2022-00622-T. (a) Effective Date This airworthiness directive (AD) is effective December 30, 2022. (b) Affected ADs This AD replaces AD 2020-21-11, Amendment 39-21284 (85 FR 65674, October 16, 2020) (AD 2020-21-11). (c) Applicability This AD applies to Airbus SAS Model airplanes specified 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 February 2, 2022. (1) Model A318-111, -112, -121, and -122 airplanes. (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, -153N, and -171N airplanes. (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -252N, -253N, -271N, -272N, and -273N airplanes. (4) Model 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, which 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 (i) of AD 2020-21-11, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before November 13, 2019, except for Model A319-171N airplanes: 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 2020-0080, dated April 1, 2020 (EASA AD 2020-0080). 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 2020-0080, With No Changes (1) The requirements specified in paragraph (1), (3), and (4) of EASA AD 2020-0080 do not apply to this AD. (2) Paragraph (2) of EASA AD 2020-0080 specifies revising "the AMP" within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, to incorporate the "limitations" specified in paragraph (3) of EASA AD 2020-0080 within 90 days after November 20, 2020 (the effective date of AD 2020-21-11). (3) The initial compliance time for doing the tasks specified in paragraph (2) of EASA AD 2020-0080 is at the applicable compliance times specified in paragraph (2) of EASA AD 2020-0080, or within 90 days after November 20, 2020 (the effective date of AD 2020-21-11), whichever occurs later. (4) The "Remarks" section of EASA AD 2020-0080 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 (k) of AD 2020-21-11, with a new exception. Except as required by paragraph (j) of this AD, after the maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions ( e.g., inspections) or intervals are allowed except as specified in the provisions of the "Ref. Publications" section of EASA AD 2020-0080. (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 2022-0082, dated May 10, 2022 (EASA AD 2022-0082). 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 2022-0082 (1) Where EASA AD 2022-0082 refers to its effective date, this AD requires using the effective date of this AD. (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 the effective date of this AD. (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 the effective date of this AD, 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. (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 2022-0082. (m) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Validation 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 International Validation Branch, send it to the attention of the person identified in paragraph (n) of this AD. Information may be emailed 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 2020-21-11 are approved as AMOCs for the corresponding provisions of EASA AD 2022-0082 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, International Validation 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 Dan Rodina, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 206-231-3225; email [email protected]. (o) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (3) The following service information was approved for IBR on December 30, 2022. (i) European Union Aviation Safety Agency (EASA) AD 2022-0082, dated May 10, 2022. (ii) [Reserved] (4) The following service information was approved for IBR on November 20, 2020 (85 FR 65674, October 16, 2020). (i) European Union Aviation Safety Agency (EASA) AD 2020-0080, dated April 1, 2020. (ii) [Reserved] (5) For EASA ADs 2022-0082 and 2020-0080, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email [email protected]; website easa.europa.eu. You may find these EASA ADs 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 that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html. Issued on October 21, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-25510 Filed 11-23-22; 8:45 am]BILLING CODE 4910-13-P