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 A350-941 and -1041 airplanes. The NPRM published in the Federal Register on September 20, 2022 (87 FR 57427). The NPRM was prompted by AD 2022-0065, dated April 7, 2022, issued by EASA (EASA AD 2022-0065), which is the Technical Agent for the Member States of the European Union (referred to after this as the MCAI). The MCAI states the possibility that protective caps are present on engine fire extinguishing pipes. This condition, if not addressed, could prevent the extinguishment of an engine fire. In the NPRM, the FAA proposed to require a one-time inspection of the engine fire extinguishing pipes for the presence of protective caps and removal of any protective caps found, as specified in EASA AD 2022-0065. The FAA is issuing this AD to address the possibility that protective caps are present on engine fire extinguishing pipes. This condition, if not addressed, could prevent the extinguishment of an engine fire. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA-2022-1167. 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 an additional comment from Delta Air Lines (DAL). The following presents the comment received on the NPRM and the FAA's response. Request To Remove Paragraph (h)(3) or Allow Later Approved Revisions of Service Information DAL requested that paragraph (h)(3) of the proposed AD be removed or that the FAA allow use of any later approved revisions of Rolls-Royce Alert Non-Modification Service Bulletin TRENT XWB 26-AK834, dated March 9, 2022; or Rolls-Royce Alert Non-Modification Service Bulletin TRENT XWB 26-AK835, dated March 10, 2022. DAL stated that a revision to either of these documents could change the applicability of the EASA AD and that the MCAI allows for later approved revisions of the service information. The FAA does not agree with the requested change. Although later approved documents are allowed for certain requirements in EASA AD 2022-0065, the FAA requires AD applicability to be fixed, and therefore requires specific revision levels to identify affected engines, as stated in paragraph (h)(3) of this AD. The FAA has made no changes to this AD in this regard. Conclusion This product has been approved by the aviation authority of another country and is approved for operation in the United States. Pursuant to the FAA's bilateral agreement with this State of Design Authority, it has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on this product. Except for minor editorial changes, and any other changes described previously, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator. Related Service Information Under 1 CFR Part 51 EASA AD 2022-0065 specifies procedures for a one-time special detailed (borescope) inspection of the engine fire extinguishing pipes in Zone 2 and removal of any protective caps found. If any protective cap is found, the lower gas generator fairing is removed and reinstalled, which includes the application of OMat 872 (a cold cure silicone compound). 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 30 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: Estimated Costs for Required Actions Labor cost Parts cost Cost per product Cost on U.S. operators 1 work-hour × $85 per hour = $85 $0 $85 $2,550 The FAA estimates the following costs to do any necessary on-condition actions that would be required based on the results of any required actions. The FAA has no way of determining the number of aircraft that might need these on-condition actions: Estimated Costs of On-Condition Actions Labor cost Parts cost Cost per product 3 work-hours × $85 per hour = $255 $0 * $255 * Up to an additional 48 hours to cure the OMat 872 (cold cure silicone compound) may be required. 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: (1) Is not a "significant regulatory action" under Executive Order 12866, (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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39-AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2022-25-22 Airbus SAS: Amendment 39-22278; Docket No. FAA-2022-1167; Project Identifier MCAI-2022-00461-T (a) Effective Date This airworthiness directive (AD) is effective January 23, 2023. (b) Affected ADs None. (c) Applicability This AD applies to Airbus SAS Model A350-941 and -1041 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2022-0065, dated April 7, 2022 (EASA AD 2022-0065). (d) Subject Air Transport Association (ATA) of America Code 26, Fire protection. (e) Unsafe Condition This AD was prompted by reports indicating that protective caps were found on engine fire extinguishing pipes in the engine core zone (Zone 2) after airplane delivery. The FAA is issuing this AD to address the possibility that protective caps are present on engine fire extinguishing pipes. This condition, if not addressed, could prevent the extinguishment of an engine fire. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2022-0065. (h) Exceptions to EASA AD 2022-0065 (1) Where EASA AD 2022-0065 refers to its effective date, this AD requires using the effective date of this AD. (2) The "Remarks" section of EASA AD 2022-0065 does not apply to this AD. (3) Where EASA AD 2022-0065 defines an affected engine, replace the text "as listed in Appendix 1 of the Rolls-Royce NMSB, as applicable" with "as listed in Appendix 1 of Rolls-Royce Alert Non-Modification Service Bulletin TRENT XWB 26-AK834, dated March 9, 2022; or Rolls-Royce Alert Non-Modification Service Bulletin TRENT XWB 26-AK835, dated March 10, 2022; as applicable." (i) No Reporting Requirement Although the service information referenced in EASA AD 2022-0065 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, Large Aircraft Section, 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 Large Aircraft Section, International Validation Branch, send it to the attention of the person identified in paragraph (k) of this AD. Information may be emailed to: 9-AVS-AIR-730-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, Large Aircraft Section, 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. (3) Required for Compliance (RC): Except as required by paragraph (j)(2) of this AD, if any service information referenced in EASA AD 2022-0065 contains paragraphs that are labeled as RC, the instructions in RC paragraphs, including subparagraphs under an RC paragraph, must be done to comply with this AD; any paragraphs, including subparagraphs under those paragraphs, that are not identified as RC are recommended. The instructions in paragraphs, including subparagraphs under those paragraphs, 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 instructions identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to instructions identified as RC require approval of an AMOC. (k) Additional Information For more information about this AD, contact Dat Le, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 516-228-7317; email Dat.V.Le@faa.gov . (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference 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) European Union Aviation Safety Agency (EASA) AD 2022-0065, dated April 7, 2022. (ii) [Reserved] (3) For EASA AD 2022-0065, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu ; website easa.europa.eu . You may find this EASA AD 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. (5) 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 fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibr-locations.html . Issued on December 5, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service.