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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 2022-25-18, Amendment 39-22274 (87 FR 75915, December 12, 2022; corrected December 27, 2022 (87 FR 79236)); and b. Adding the following new airworthiness directive: 2024-06-10 BAE Systems (Operations) Limited: Amendment 39-22715; Docket No. FAA-2023-2400; Project Identifier MCAI-2023-00782-T. (a) Effective Date This airworthiness directive (AD) is effective May 22, 2024. (b) Affected ADs This AD replaces AD 2022-25-18, Amendment 39-22274 (87 FR 75915, December 12, 2022; corrected December 27, 2022 (87 FR 79236)). (c) Applicability This AD applies to all BAE Systems (Operations) Limited Model BAe 146-100A, -200A, and -300A airplanes and Model Avro 146-RJ70A, 146-RJ85A, and 146-RJ100A airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 32, Landing gear. (e) Unsafe Condition This AD was prompted by reports of cracking on the shoulders of a main landing gear (MLG) side stay outer link. The FAA is issuing this AD to address cracking of the MLG side stay outer link. The unsafe condition, if not addressed, could lead to failure of the MLG side stay outer link and MLG collapse, which could result in a runway departure and the engine or wing contacting the ground. The engine or wing contacting the ground could result in damage to the airplane, an increased risk of fire, the airplane flipping, and injury to occupants. (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, United Kingdom (U.K.) Civil Aviation Authority (CAA) (U.K. CAA) AD G-2023-0004R1, dated November 16, 2023 (U.K. CAA AD G-2023-0004R1). (h) Exceptions to U.K. CAA AD G-2023-0004R1 (1) Where U.K. CAA AD G-2023-0004R1 refers to July 7, 2023 (the effective date of U.K. CAA AD G-2023-0004 at original issue), this AD requires using the effective date of this AD. (2) This AD does not adopt the paragraph that begins with "Required as indicated, unless accomplished previously in accordance with ASB.32-A189 . . ." and the Note that begins with "Prior accomplishment of inspection requirements . . ." specified in "Required Actions(s) and Compliance Time(s)" of U.K. CAA AD G-2023-0004R1. (3) Where U.K. CAA AD G-2023-0004R1 refers to "ASB," "the ASB," or "ASB.32-A189 Revision 2," this AD requires using BAE Systems (Operations) Limited Alert Service Bulletin ASB.32-A189, Revision 2, dated August 3, 2023. (4) Where U.K. CAA AD G-2023-0004R1 specifies a detailed visual inspection "every 500 flights or 6 months (whichever occurs first)," for this AD, replace that text with "repeat at intervals not to exceed 500 flight cycles or 6 months, whichever occurs first." (5) Where U.K. CAA AD G-2023-0004R1 specifies a special detailed inspection "every 1200 flights or 12 months (whichever occurs first)," for this AD, replace that text with "repeat at intervals not to exceed 1,200 flight cycles or 12 months, whichever occurs first." (6) Where U.K. CAA AD G-2023-0004R1 specifies "in accordance with the dimensional limits provided in Appendix 2 then Safran Landing Systems must be contacted to provide further instructions," this AD requires "before further flight, repair using a method approved by the Manager, International Validation Branch, FAA; or the U.K. CAA; or BAE Systems (Operations) Limited's U.K. CAA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature." (7) Where U.K. CAA AD G-2023-0004R1 specifies the lubrication of the MLG sidestay outer link pivots "every 500 flights or 6 months (whichever occurs first)," for this AD, replace that text with "at intervals not to exceed 500 flight cycles or 6 months, whichever occurs first." (8) Where paragraph (5) of U.K. CAA AD G-2023-0004R1 specifies "as required by paragraphs (1) and (2) of this AD," for this AD, replace that text with "as required by paragraphs (1), (2), and (3) of this AD." (9) Where the Note in paragraph (5) of U.K. CAA AD G-2023-0004R1 specifies "the part must have been inspected in accordance with paragraph (1) of this AD and a one-off dimensional check, airworthiness assessment and reporting performed in accordance with paragraph (2) of this AD," for this AD, replace that text with "the part must have been inspected in accordance with paragraph (1) or (2) of this AD and a one-off dimensional check and airworthiness assessment performed in accordance with paragraph (3) of this AD." (10) This AD does not adopt the "Remarks" section of U.K. CAA AD G-2023-0004R1. (i) No Reporting Requirement Although U.K. CAA AD G-2023-0004R1 and BAE Systems (Operations) Limited Alert Service Bulletin ASB.32-A189, Revision 2, dated August 3, 2023, specify to submit certain information to the manufacturer, this AD does not include that requirement. (j) Credit for Previous Actions (1) This paragraph provides credit for actions required by paragraph (1) of U.K. CAA AD G-2023-0004R1, if those actions were performed before the effective date of this AD using BAE Systems (Operations) Limited Alert Service Bulletin ASB.32-A189, dated September 16, 2022, which was incorporated by reference in AD 2022-25-18, Amendment 39-22274 (87 FR 75915, December 12, 2022; corrected December 27, 2022 (87 FR 79236)); or BAE Systems (Operations) Limited Alert Service Bulletin ASB.32-A189, Revision 1, dated March 13, 2023, which is not incorporated by reference in this AD. (2) This paragraph provides credit for actions required by paragraph (3) of U.K. CAA AD G-2023-0004R1, if those actions were performed before the effective date of this AD using BAE Systems (Operations) Limited Alert Service Bulletin ASB.32-A189, Revision 1, dated March 13, 2023, which is not incorporated by reference in this AD. (k) 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 manager of the International Validation Branch, mail it to the address identified in paragraph (l)(1) of this AD or email to: 9-AVS-AIR-730-AMOC@faa.gov. If mailing information, also submit information by email. 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, International Validation Branch, FAA; or the U.K. CAA; or BAE Systems (Operations) Limited's U.K. CAA DOA. If approved by the DOA, the approval must include the DOA-authorized signature. (l) Additional Information (1) For more information about this AD, contact Todd Thompson, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206-231-3228; email todd.thompson@faa.gov. (2) Service information identified in this AD that is not incorporated by reference is available at the address specified in paragraph (m)(4) of this AD. (m) 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. (i) BAE Systems (Operations) Limited Alert Service Bulletin ASB.32-A189, Revision 2, dated August 3, 2023. (ii) United Kingdom Civil Aviation Authority (U.K. CAA) AD G-2023-0004R1, dated November 16, 2023. (3) For U.K. CAA AD G-2023-0004R1, contact Civil Aviation Authority, Aviation House, Beehive Ring Road, Crawley, West Sussex RH6 0YR, United Kingdom; telephone +44(0) 330 022 4401; email continued.airworthiness@caa.co.uk; website caa.co.uk. (4) For BAE Systems (Operations) Limited service information, contact BAE Systems (Operations) Limited, Customer Information Department, Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United Kingdom; telephone +44 1292 675207; fax +44 1292 675704; email RApublications@baesystems.com; website regional-services.com. (5) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th Street, Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (6) 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 March 19, 2024. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2024-08108 Filed 4-16-24; 8:45 am]BILLING CODE 4910-13-P