2022-02-10: Standard Practices/Structures

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: 2022-02-10 Dassault Aviation: Amendment 39-21907; Docket No. FAA-2021-0684; Project Identifier MCAI-2021-00194-T. (a) Effective Date This airworthiness directive (AD) is effective March 15, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Dassault Aviation airplanes identified in paragraphs (c)(1) through (3) of this AD, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2021-0047, dated February 16, 2021 (EASA AD 2021-0047). (1) Model FALCON 7X airplanes. (2) Model FALCON 900EX airplanes. (3) Model FALCON 2000EX airplanes. (d) Subject Air Transport Association (ATA) of America Code 51, Standard Practices/Structures. (e) Reason This AD was prompted by a report of an improper heat treatment process applied during the manufacturing of certain Decomatic titanium screws. The FAA is issuing this AD to address failure of an affected screw installed in a critical location, possibly resulting in reduced structural integrity of the airplane. (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 2021-0047. (h) Exceptions to EASA AD 2021-0047 (1) Where EASA AD 2021-0047 refers to its effective date, this AD requires using the effective date of this AD. (2) The "Remarks" section of EASA AD 2021-0047 does not apply to this AD. (3) Where EASA AD 2021-0047 specifies to "replace each serviceable part," for this AD that replacement includes an inspection of the bore dimension and corrective actions (oversizing or repair), as specified in the service information referenced in EASA AD 2021-0047. (i) No Reporting Requirement Although the service information referenced in EASA AD 2021-0047 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 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 Dassault Aviation's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (k) Related Information For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226; email tom.rodriguez@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 2021-0047, dated February 16, 2021. (ii) [Reserved] (3) For EASA AD 2021-0047, 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 this EASA AD on the EASA website at https://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: https://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued on January 10, 2022. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-02555 Filed 2-7-22; 8:45 am]BILLING CODE 4910-13-P