2022-11-08: Electrical Power System, Aircraft Fuel System, Hydraulic Power System, Doors, Fuselage Structure, Main Rotor System, Main Rotor Drive System, Tail Rotor System, Tail Rotor Drive System, Rotorcraft Flight Control

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 adding the following new airworthiness directive: 2022-11-08 Airbus Helicopters: Amendment 39-22058; Docket No. FAA-2022-0297; Project Identifier MCAI-2021-01099-R. (a) Effective Date This airworthiness directive (AD) is effective July 8, 2022. (b) Affected ADs This AD affects AD 2011-22-05 R1, Amendment 39-17765 (79 FR 14169, March 13, 2014) (AD 2011-22-05 R1); and AD 2016-25-20, Amendment 39-18746 (81 FR 94954, December 27, 2016) (AD 2016-25-20). (c) Applicability This AD applies to all Airbus Helicopters Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, EC130B4, and EC130T2 helicopters, certificated in any category. (d) Subject Joint Aircraft Service Component (JASC) Codes: 2400, Electrical Power System; 2800, Aircraft Fuel System; 2900, Hydraulic Power System; 5200, Doors; 5300, Fuselage Structure; 6200, Main Rotor System; 6300, Main Rotor Drive System; 6400, Tail Rotor System; 6500, Tail Rotor Drive System; and 6700, Rotorcraft Flight Control. (e) Unsafe Condition This AD was prompted by the identification of certain parts needing maintenance actions, including life limits and maintenance tasks. The FAA is issuing this AD to address the failure of certain parts, which could result in the loss of control of the helicopter. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions Within 30 days after the effective date of this AD, incorporate into maintenance records required by 14 CFR 91.417(a)(2) or 135.439(a)(2), as applicable for your rotorcraft, the requirements (airworthiness limitations) specified in paragraph (1) of European Union Aviation Safety Agency (EASA) AD 2021-0194R1, dated October 8, 2021 (EASA AD 2021-0194R1). (h) Provisions for Alternative Requirements (Airworthiness Limitations) After the action required by paragraph (g) of this AD has been done, no alternative requirements (airworthiness limitations) are allowed unless they are approved as specified in the provisions of the "Ref. Publications" section of EASA AD 2021-0194R1. (i) Terminating Action for ADs 2011-22-05 R1 and 2016-25-20 (1) Accomplishing the actions required by this AD terminates all requirements of AD 2011-22-05 R1 for Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, and AS350D helicopters only. (2) Accomplishing the actions required by this AD terminates all requirements of AD 2016-25-20 for Model AS350B, AS350BA, AS350B1, AS350B2, AS350B3, AS350D, EC130B4, and EC130T2 helicopters only. (j) Special Flight Permit Special flight permits, as described in 14 CFR 21.197 and 21.199, are prohibited. (k) Alternative Methods of Compliance (AMOCs) (1) 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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph (l) of this AD. Information may be emailed to: 9-AVS-AIR-730-AMOC@faa.gov. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (l) Related Information For more information about this AD, contact Andrea Jimenez, Aerospace Engineer, COS Program Management Section, Operational Safety Branch, Compliance & Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-7330; email andrea.jimenez@faa.gov. (m) 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 2021-0194R1, dated October 8, 2021. (ii) [Reserved] (3) For EASA AD 2021-0194R1, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find the EASA material on the EASA website at https://ad.easa.europa.eu. (4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222-5110. This material may be found in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-0297. (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: https://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued on May 17, 2022. Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-11957 Filed 6-2-22; 8:45 am]BILLING CODE 4910-13-P