Airworthiness Directives; Dassault Aviation Airplanes, 41361-41365 [2024-09511]

Download as PDF Federal Register / Vol. 89, No. 93 / Monday, May 13, 2024 / Proposed Rules § 208.31 Reasonable fear of persecution or torture determinations involving aliens ordered removed under section 238(b) of the Act and aliens whose removal is reinstated under section 241(a)(5) of the Act. lotter on DSK11XQN23PROD with PROPOSALS1 * * * * * (c) Interview and procedure. The asylum officer shall conduct the interview in a non-adversarial manner, separate and apart from the general public. At the time of the interview, the asylum officer shall determine that the alien has an understanding of the reasonable fear determination process. The alien may be represented by counsel or an accredited representative at the interview, at no expense to the Government, and may present evidence, if available, relevant to the possibility of persecution or torture. The alien’s representative may present a statement at the end of the interview. The asylum officer, in his or her discretion, may place reasonable limits on the number of persons who may be present at the interview and the length of the statement. If the alien is unable to proceed effectively in English, and if the asylum officer is unable to proceed competently in a language chosen by the alien, the asylum officer shall arrange for the assistance of an interpreter in conducting the interview. The interpreter may not be a representative or employee of the applicant’s country or nationality, or if the applicant is stateless, the applicant’s country of last habitual residence. The asylum officer shall create a summary of the material facts as stated by the applicant. At the conclusion of the interview, the officer shall review the summary with the alien and provide the alien with an opportunity to correct errors therein. The asylum officer shall create a written record of his or her determination, including a summary of the material facts as stated by the applicant, any additional facts relied on by the officers, and the officer’s determination of whether, in light of such facts, the alien has established a reasonable fear of persecution or torture. The alien shall be determined to have a reasonable fear of persecution if the alien establishes a reasonable possibility that he or she would be persecuted on account of his or her race, religion, nationality, membership in a particular social group or political opinion, unless the alien appears to be subject to one or more of the mandatory bars to being granted withholding of removal under the Act contained in section 241(b)(3)(B) of the Act and the alien fails to show that there is a reasonable possibility that no mandatory bar applies, if the asylum officer considers such bars. The alien VerDate Sep<11>2014 21:32 May 10, 2024 Jkt 262001 shall be determined to have a reasonable fear of persecution or torture if the alien establishes a reasonable possibility that he or she would be tortured in the country of removal. * * * * * (g) Review by immigration judge. The asylum officer’s negative decision regarding reasonable fear shall be subject to review by an immigration judge upon the alien’s request. If the alien requests such review, the asylum officer shall serve him or her with a Notice of Referral to Immigration Judge. The record of determination, including copies of the Notice of Referral to Immigration Judge, the asylum officer’s notes, the summary of the material facts, and other materials upon which the determination was based shall be provided to the immigration judge with the negative determination. The immigration judge’s review shall proceed under the procedures set forth in 8 CFR 1208.31(g). 4. Amend § 208.33 by revising paragraphs (b)(2)(i) through (iii) to read as follows: ■ 41361 country or countries of removal, the Department will issue a Form I–862, Notice to Appear. (iii) In cases described in paragraph (b)(2)(i) of this section, if an alien fails to establish a reasonable possibility of persecution with respect to the identified country or countries of removal or, to the extent bars are considered, fails to establish that there is a reasonable possibility that no mandatory bar applies, and fails to establish a reasonable possibility of torture with respect to the identified country or countries of removal, the asylum officer will provide the alien with a written notice of decision and inquire whether the alien wishes to have an immigration judge review the negative credible fear determinations. * * * * * Alejandro N. Mayorkas, Secretary, U.S. Department of Homeland Security. [FR Doc. 2024–10390 Filed 5–9–24; 4:15 pm] BILLING CODE 9111–97–P § 208.33 Lawful pathways condition on asylum eligibility. DEPARTMENT OF TRANSPORTATION * Federal Aviation Administration * * * * (b) * * * (2) * * * (i) In cases in which the asylum officer enters a negative credible fear determination under paragraph (b)(1)(i) of this section, the asylum officer will assess whether the alien has established a reasonable possibility of persecution (meaning a reasonable possibility of being persecuted because of their race, religion, nationality, membership in a particular social group, or political opinion) or torture, with respect to the identified country or countries of removal identified pursuant to section 241(b) of the Act. As part of this reasonable possibility determination, if there is evidence that the alien is subject to one or more of the mandatory bars to being granted withholding of removal under the Act contained in section 241(b)(3)(B) of the Act, the asylum officer may consider the applicability of such bar(s). (ii) In cases described in paragraph (b)(2)(i) of this section, if the alien establishes a reasonable possibility of persecution with respect to the identified country or countries of removal and, to the extent bars are considered, that there is a reasonable possibility that no mandatory bar applies, the Department will issue a Form I–862, Notice to Appear. If the alien establishes a reasonable possibility of torture with respect to the identified PO 00000 Frm 00015 Fmt 4702 Sfmt 4702 14 CFR Part 39 [Docket No. FAA–2024–1290; Project Identifier MCAI–2024–00078–T] RIN 2120–AA64 Airworthiness Directives; Dassault Aviation Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to supersede Airworthiness Directive (AD) 2023–22–13, which applies to certain Dassault Aviation Model FALCON 7X airplanes. AD 2023–22–13 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2023–22–13, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require certain actions in AD 2023–22–13 and would require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The SUMMARY: E:\FR\FM\13MYP1.SGM 13MYP1 41362 Federal Register / Vol. 89, No. 93 / Monday, May 13, 2024 / Proposed Rules FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this proposed AD by June 27, 2024. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: 202–493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2024–1290; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this NPRM, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For material that is proposed for IBR in this NPRM, 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 material on the EASA website at ad.easa.europa.eu. • 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. It is also available at regulations.gov under Docket No. FAA–2024–1290. FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 206– 231–3226; email: tom.rodriguez@ faa.gov. lotter on DSK11XQN23PROD with PROPOSALS1 SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2024–1290; Project Identifier MCAI–2024–00078–T’’ at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, explain the reason for any VerDate Sep<11>2014 21:32 May 10, 2024 Jkt 262001 recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this proposal because of those comments. Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this NPRM. Confidential Business Information CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this NPRM contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this NPRM, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as ‘‘PROPIN.’’ The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this NPRM. Submissions containing CBI should be sent to Tom Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone: 206–231–3226; email: tom.rodriguez@faa.gov. Any commentary that the FAA receives that is not specifically designated as CBI will be placed in the public docket for this rulemaking. Background The FAA issued AD 2023–22–13, Amendment 39–22597 (88 FR 82246, November 24, 2023) (AD 2023–22–13), for certain Dassault Aviation Model FALCON 7X airplanes. AD 2023–22–13 was prompted by an MCAI originated by EASA, which is the Technical Agent for the Member States of the European Union. EASA issued AD 2023–0063, dated March 20, 2023 (EASA AD 2023– 0063) (which corresponds to FAA AD 2023–22–13), to correct an unsafe condition. AD 2023–22–13 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2023– 22–13 to address reduced structural integrity and reduced control of the PO 00000 Frm 00016 Fmt 4702 Sfmt 4702 airplane due to the failure of system components. AD 2023–22–13 specifies that accomplishing the revision required by that AD terminates certain requirements of AD AD 2014–16–23, Amendment 39–17947 (79 FR 52545, September 4, 2014) (AD 2014–16–23). This proposed AD would therefore continue to allow that terminating action. Actions Since AD 2023–22–13 Was Issued Since the FAA issued AD 2023–22– 13, EASA superseded AD 2023–0063 and issued EASA AD 2024–0033, dated January 31, 2024 (EASA AD 2024–0033) (referred to after this as the MCAI), for all Dassault Aviation Model FALCON 7X airplanes. The MCAI states that new or more restrictive airworthiness limitations have been developed. Airplanes with an original airworthiness certificate or original export certificate of airworthiness issued after September 7, 2022, must comply with the airworthiness limitations specified as part of the approved type design and referenced on the type certificate data sheet; this proposed AD therefore does not include those airplanes in the applicability. The FAA is proposing this AD to address reduced structural integrity and reduced control of the airplane due to the failure of system components. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2024–1290. Related Service Information Under 1 CFR Part 51 The FAA reviewed EASA AD 2024– 0033. This service information specifies new or more restrictive airworthiness limitations for airplane structures and safe life limits. This proposed AD would also require EASA AD 2023–0063, which the Director of the Federal Register approved for incorporation by reference as of December 29, 2023 (88 FR 82246, November 24, 2023). 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 ADDRESSES. FAA’s Determination 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 is issuing this NPRM after determining E:\FR\FM\13MYP1.SGM 13MYP1 Federal Register / Vol. 89, No. 93 / Monday, May 13, 2024 / Proposed Rules that the unsafe condition described previously is likely to exist or develop in other products of the same type design. lotter on DSK11XQN23PROD with PROPOSALS1 Proposed AD Requirements in This NPRM This proposed AD would retain certain requirements of AD 2023–22–13. This proposed AD would also require revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive airworthiness limitations, which are specified in EASA AD 2024– 0033 already described, as proposed for incorporation by reference. Any differences with EASA AD 2024–0033 are identified as exceptions in the regulatory text of this AD. This proposed AD would require revisions to certain operator maintenance documents to include new actions (e.g., inspections) and Critical Design Configuration Control Limitations (CDCCLs). Compliance with these actions and CDCCLs is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by this proposed AD, the operator may not be able to accomplish the actions described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance (AMOC) according to paragraph (n)(1) of this proposed AD. Explanation of Required Compliance Information In the FAA’s ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, the FAA proposes to retain the IBR of EASA AD 2023–0063 and incorporate EASA AD 2024–0033 by reference in the FAA final rule. This proposed AD would, therefore, require compliance with EASA AD 2024–0033 and EASA AD 2023–0063 through that incorporation, except for any differences identified as exceptions in the regulatory text of this proposed AD. Using common terms that are the same as the heading of a particular section in EASA AD 2024–0033 or EASA AD 2023–0063 does not mean that operators need comply only with that section. For example, where the AD requirement refers to ‘‘all required actions and compliance times,’’ compliance with this AD requirement is not limited to VerDate Sep<11>2014 21:32 May 10, 2024 Jkt 262001 the section titled ‘‘Required Action(s) and Compliance Time(s)’’ in EASA AD 2024–0033 or EASA AD 2023–0063. Service information required by EASA AD 2024–0033 and EASA AD 2023– 0063 for compliance will be available at regulations.gov by searching for and locating Docket No. FAA–2024–1290 after the FAA final rule is published. Airworthiness Limitation ADs Using the New Process The FAA’s process of incorporating by reference MCAI ADs as the primary source of information for compliance with corresponding FAA ADs has been limited to certain MCAI ADs (primarily those with service bulletins as the primary source of information for accomplishing the actions required by the FAA AD). However, the FAA is now expanding the process to include MCAI ADs that require a change to airworthiness limitation documents, such as airworthiness limitation sections. For these ADs that incorporate by reference an MCAI AD that changes airworthiness limitations, the FAA requirements are unchanged. Operators must revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in the new airworthiness limitation document. The airworthiness limitations must be followed according to 14 CFR 91.403(c) and 91.409(e). The previous format of the airworthiness limitation ADs included a paragraph that specified that no alternative actions (e.g., inspections), intervals, or CDCCLs may be used unless the actions, intervals, and CDCCLs are approved as an AMOC in accordance with the procedures specified in the AMOCs paragraph under ‘‘Additional AD Provisions.’’ This new format includes a ‘‘New Provisions for Alternative Actions, Intervals, and CDCCLs’’ paragraph that does not specifically refer to AMOCs, but operators may still request an AMOC to use an alternative action, interval, or CDCCL. Costs of Compliance The FAA estimates that this AD, if adopted as proposed, would affect 134 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD: The FAA estimates the total cost per operator for the retained actions from AD 2023–22–13 to be $7,650 (90 workhours × $85 per work-hour). The FAA has determined that revising the existing maintenance or inspection program takes an average of 90 workhours per operator, although the agency PO 00000 Frm 00017 Fmt 4702 Sfmt 4702 41363 recognizes that this number may vary from operator to operator. Since operators incorporate maintenance or inspection program changes for their affected fleet(s), the FAA has determined that a per-operator estimate is more accurate than a per-airplane estimate. The FAA estimates the total cost per operator for the new proposed actions to be $7,650 (90 work-hours × $85 per work-hour). 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 The FAA determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would 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 this proposed regulation: (1) Is not a ‘‘significant regulatory action’’ under Executive Order 12866, (2) Would not affect intrastate aviation in Alaska, and (3) Would 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 Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, E:\FR\FM\13MYP1.SGM 13MYP1 41364 Federal Register / Vol. 89, No. 93 / Monday, May 13, 2024 / Proposed Rules the FAA proposes to amend 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: a. Removing Airworthiness Directive (AD) 2023–22–13, Amendment 39– 22597 (88 FR 82246, November 24, 2023); and ■ b. Adding the following new AD: ■ ■ Dassault Aviation: Docket No. FAA–2024– 1290; Project Identifier MCAI–2024– 00078–T. (a) Comments Due Date The FAA must receive comments on this airworthiness directive (AD) by June 27, 2024. (b) Affected ADs (1) This AD replaces AD 2023–22–13, Amendment 39–22597 (88 FR 82246, November 24, 2023) (AD 2023–22–13). (2) This AD affects AD 2014–16–23, Amendment 39–17947 (79 FR 52545, September 4, 2014) (AD 2014–16–23) (c) Applicability This AD applies to Dassault Aviation Model FALCON 7X airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before September 7, 2023. Note 1 to paragraph (c): Model FALCON 7X airplanes with modification M1000 incorporated are commonly referred to as ‘‘Model FALCON 8X’’ airplanes as a marketing designation. (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 reduced structural integrity and reduced control of the airplane due to the failure of system components. lotter on DSK11XQN23PROD with PROPOSALS1 (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 (j) of AD 2023–22–13, with a new terminating action. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before September 7, 2022, except as specified in paragraph (h) of this AD: Comply VerDate Sep<11>2014 21:32 May 10, 2024 Jkt 262001 with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2023–0063, dated March 20, 2023 (EASA AD 2023–0063). 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 2023– 0063, With No Changes This paragraph restates the exceptions specified in paragraph (k) of AD 2023–22–13, with no changes. (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2023–0063. (2) Paragraph (3) of EASA AD 2023–0063 specifies revising ‘‘the approved AMP [aircraft maintenance program]’’ within 12 months after its effective date, but this AD requires revising the existing maintenance or inspection program, as applicable, within 90 days after December 29, 2023 (the effective date of AD 2023–22–13). (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2023–0063 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2023–0063, or within 90 days after December 29, 2023 (the effective date of AD 2023–22–13), whichever occurs later. (4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2023–0063. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2023–0063. (i) Retained Restrictions on Alternative Actions, Intervals, and Critical Design Configuration Control Limitations (CDCCLs), With a New Exception This paragraph restates the requirements of paragraph (l) of AD 2023–22–13, 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), intervals, or CDCCLs are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2023–0063. (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 2024–0033, dated January 31, 2024 (EASA AD 2024– 0033). 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 2024–0033 (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2024–0033. (2) Paragraph (3) of EASA AD 2024–0033 specifies revising ‘‘the approved AMP’’ within 12 months after its effective date, but this AD requires revising the existing PO 00000 Frm 00018 Fmt 4702 Sfmt 4702 maintenance or inspection program, as applicable, within 90 days after the effective date of this AD. (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2024–0033 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2024–0033, or within 90 days after the effective date of this AD, whichever occurs later. (4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2024–0033. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2024–0033. (l) New Provisions for Alternative Actions, Intervals, and CDCCLs After the existing maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections), intervals, and CDCCLs are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2024–0033. (m) Terminating Action for Certain Requirements in AD 2014–16–23 Accomplishing the actions required by paragraphs (g) or (j) of this AD terminates the requirements of paragraph (q) of AD 2014– 16–23. (n) 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 (o) 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, 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 DOAauthorized signature. (o) Additional Information For more information about this AD, contact Tom Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206– 231–3226; email: tom.rodriguez@faa.gov. (p) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this E:\FR\FM\13MYP1.SGM 13MYP1 Federal Register / Vol. 89, No. 93 / Monday, May 13, 2024 / Proposed Rules 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 [DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE]. (i) European Union Aviation Safety Agency (EASA) AD 2024–0033, dated January 31, 2024. (ii) [Reserved] (4) The following service information was approved for IBR on December 29, 2023 (88 FR 82246, November 24, 2023). (i) European Union Aviation Safety Agency (EASA) AD 2023–0063, dated March 20, 2023. (ii) [Reserved] (5) For EASA ADs 2024–0033 and 2023– 0063, 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 these EASA ADs on the EASA website at ad.easa.europa.eu. (6) You may view this service information 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 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-locationsoremailfr.inspection@nara.gov. Issued on April 26, 2024. James D. Foltz, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2024–09511 Filed 5–10–24; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2024–1294; Project Identifier MCAI–2024–00042–T] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: The FAA proposes to supersede Airworthiness Directive (AD) 2022–16–06, which applies to certain Airbus SAS Model A330–200, A330– 200 Freighter, A330–300, and A330–900 series airplanes; and all Model A340– 200 and A340–300 series airplanes. AD 2022–16–06 requires modifying the Trimmable Horizontal Stabilizer lotter on DSK11XQN23PROD with PROPOSALS1 SUMMARY: VerDate Sep<11>2014 21:32 May 10, 2024 Jkt 262001 Actuator (THSA) installation, implementing the electrical load sensing device (ELSD) wiring provisions, and installing and activating the ELSD. Since the FAA issued AD 2022–16–06, it has been determined that the required actions cannot be accomplished on certain airplanes, and additional instructions and corrections have been developed. This proposed AD would continue to require the actions in AD 2022–16–06 with certain revised procedures and would require additional work for certain airplanes, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products. The FAA must receive comments on this proposed AD by June 27, 2024. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: 202–493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2024–1294; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this NPRM, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For the EASA AD identified in this NPRM, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; website easa.europa.eu. You may find this material on the EASA website at ad.easa.europa.eu. It is also available at regulations.gov under Docket No. FAA– 2024–1294. • 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. DATES: PO 00000 Frm 00019 Fmt 4702 Sfmt 4702 41365 FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206–231–3229; email Vladimir.Ulyanov@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under ADDRESSES. Include ‘‘Docket No. FAA–2024–1294; Project Identifier MCAI–2024–00042–T’’ at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this proposal because of those comments. Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this NPRM. Confidential Business Information CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this NPRM contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this NPRM, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as ‘‘PROPIN.’’ The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this NPRM. Submissions containing CBI should be sent to Vladimir Ulyanov, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206–231–3229; email Vladimir.Ulyanov@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking. E:\FR\FM\13MYP1.SGM 13MYP1

Agencies

[Federal Register Volume 89, Number 93 (Monday, May 13, 2024)]
[Proposed Rules]
[Pages 41361-41365]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-09511]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-1290; Project Identifier MCAI-2024-00078-T]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 
2023-22-13, which applies to certain Dassault Aviation Model FALCON 7X 
airplanes. AD 2023-22-13 requires revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations. Since the FAA issued AD 2023-22-
13, the FAA has determined that new or more restrictive airworthiness 
limitations are necessary. This proposed AD would continue to require 
certain actions in AD 2023-22-13 and would require revising the 
existing maintenance or inspection program, as applicable, to 
incorporate new or more restrictive airworthiness limitations, as 
specified in a European Union Aviation Safety Agency (EASA) AD, which 
is proposed for incorporation by reference (IBR). The

[[Page 41362]]

FAA is proposing this AD to address the unsafe condition on these 
products.

DATES: The FAA must receive comments on this proposed AD by June 27, 
2024.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to regulations.gov. Follow 
the instructions for submitting comments.
     Fax: 202-493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2024-1290; or in person at Docket Operations between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD 
docket contains this NPRM, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For material that is proposed for IBR in this NPRM, 
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone 
+49 221 8999 000; email [email protected]; website easa.europa.eu. You 
may find this material on the EASA website at ad.easa.europa.eu.
     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. It is also available at regulations.gov under 
Docket No. FAA-2024-1290.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aviation Safety 
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
telephone: 206-231-3226; email: [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2024-1290; Project Identifier 
MCAI-2024-00078-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, explain the 
reason for any recommended change, and include supporting data. The FAA 
will consider all comments received by the closing date and may amend 
this proposal because of those comments.
    Except for Confidential Business Information (CBI) as described in 
the following paragraph, and other information as described in 14 CFR 
11.35, the FAA will post all comments received, without change, to 
regulations.gov, including any personal information you provide. The 
agency will also post a report summarizing each substantive verbal 
contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily 
and actually treated as private by its owner. Under the Freedom of 
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public 
disclosure. If your comments responsive to this NPRM contain commercial 
or financial information that is customarily treated as private, that 
you actually treat as private, and that is relevant or responsive to 
this NPRM, it is important that you clearly designate the submitted 
comments as CBI. Please mark each page of your submission containing 
CBI as ``PROPIN.'' The FAA will treat such marked submissions as 
confidential under the FOIA, and they will not be placed in the public 
docket of this NPRM. Submissions containing CBI should be sent to Tom 
Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 
410, Westbury, NY 11590; telephone: 206-231-3226; email: 
[email protected]. Any commentary that the FAA receives that is not 
specifically designated as CBI will be placed in the public docket for 
this rulemaking.

Background

    The FAA issued AD 2023-22-13, Amendment 39-22597 (88 FR 82246, 
November 24, 2023) (AD 2023-22-13), for certain Dassault Aviation Model 
FALCON 7X airplanes. AD 2023-22-13 was prompted by an MCAI originated 
by EASA, which is the Technical Agent for the Member States of the 
European Union. EASA issued AD 2023-0063, dated March 20, 2023 (EASA AD 
2023-0063) (which corresponds to FAA AD 2023-22-13), to correct an 
unsafe condition.
    AD 2023-22-13 requires revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations. The FAA issued AD 2023-22-13 to 
address reduced structural integrity and reduced control of the 
airplane due to the failure of system components. AD 2023-22-13 
specifies that accomplishing the revision required by that AD 
terminates certain requirements of AD AD 2014-16-23, Amendment 39-17947 
(79 FR 52545, September 4, 2014) (AD 2014-16-23). This proposed AD 
would therefore continue to allow that terminating action.

Actions Since AD 2023-22-13 Was Issued

    Since the FAA issued AD 2023-22-13, EASA superseded AD 2023-0063 
and issued EASA AD 2024-0033, dated January 31, 2024 (EASA AD 2024-
0033) (referred to after this as the MCAI), for all Dassault Aviation 
Model FALCON 7X airplanes. The MCAI states that new or more restrictive 
airworthiness limitations have been developed.
    Airplanes with an original airworthiness certificate or original 
export certificate of airworthiness issued after September 7, 2022, 
must comply with the airworthiness limitations specified as part of the 
approved type design and referenced on the type certificate data sheet; 
this proposed AD therefore does not include those airplanes in the 
applicability.
    The FAA is proposing this AD to address reduced structural 
integrity and reduced control of the airplane due to the failure of 
system components. You may examine the MCAI in the AD docket at 
regulations.gov under Docket No. FAA-2024-1290.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2024-0033. This service information 
specifies new or more restrictive airworthiness limitations for 
airplane structures and safe life limits.
    This proposed AD would also require EASA AD 2023-0063, which the 
Director of the Federal Register approved for incorporation by 
reference as of December 29, 2023 (88 FR 82246, November 24, 2023).
    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 ADDRESSES.

FAA's Determination

    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 is issuing this NPRM after determining

[[Page 41363]]

that the unsafe condition described previously is likely to exist or 
develop in other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would retain certain requirements of AD 2023-22-
13. This proposed AD would also require revising the existing 
maintenance or inspection program, as applicable, to incorporate 
additional new or more restrictive airworthiness limitations, which are 
specified in EASA AD 2024-0033 already described, as proposed for 
incorporation by reference. Any differences with EASA AD 2024-0033 are 
identified as exceptions in the regulatory text of this AD.
    This proposed AD would require revisions to certain operator 
maintenance documents to include new actions (e.g., inspections) and 
Critical Design Configuration Control Limitations (CDCCLs). Compliance 
with these actions and CDCCLs is required by 14 CFR 91.403(c). For 
airplanes that have been previously modified, altered, or repaired in 
the areas addressed by this proposed AD, the operator may not be able 
to accomplish the actions described in the revisions. In this 
situation, to comply with 14 CFR 91.403(c), the operator must request 
approval for an alternative method of compliance (AMOC) according to 
paragraph (n)(1) of this proposed AD.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD 
process, the FAA developed a process to use some civil aviation 
authority (CAA) ADs as the primary source of information for compliance 
with requirements for corresponding FAA ADs. The FAA has been 
coordinating this process with manufacturers and CAAs. As a result, the 
FAA proposes to retain the IBR of EASA AD 2023-0063 and incorporate 
EASA AD 2024-0033 by reference in the FAA final rule. This proposed AD 
would, therefore, require compliance with EASA AD 2024-0033 and EASA AD 
2023-0063 through that incorporation, except for any differences 
identified as exceptions in the regulatory text of this proposed AD. 
Using common terms that are the same as the heading of a particular 
section in EASA AD 2024-0033 or EASA AD 2023-0063 does not mean that 
operators need comply only with that section. For example, where the AD 
requirement refers to ``all required actions and compliance times,'' 
compliance with this AD requirement is not limited to the section 
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2024-
0033 or EASA AD 2023-0063. Service information required by EASA AD 
2024-0033 and EASA AD 2023-0063 for compliance will be available at 
regulations.gov by searching for and locating Docket No. FAA-2024-1290 
after the FAA final rule is published.

Airworthiness Limitation ADs Using the New Process

    The FAA's process of incorporating by reference MCAI ADs as the 
primary source of information for compliance with corresponding FAA ADs 
has been limited to certain MCAI ADs (primarily those with service 
bulletins as the primary source of information for accomplishing the 
actions required by the FAA AD). However, the FAA is now expanding the 
process to include MCAI ADs that require a change to airworthiness 
limitation documents, such as airworthiness limitation sections.
    For these ADs that incorporate by reference an MCAI AD that changes 
airworthiness limitations, the FAA requirements are unchanged. 
Operators must revise the existing maintenance or inspection program, 
as applicable, to incorporate the information specified in the new 
airworthiness limitation document. The airworthiness limitations must 
be followed according to 14 CFR 91.403(c) and 91.409(e).
    The previous format of the airworthiness limitation ADs included a 
paragraph that specified that no alternative actions (e.g., 
inspections), intervals, or CDCCLs may be used unless the actions, 
intervals, and CDCCLs are approved as an AMOC in accordance with the 
procedures specified in the AMOCs paragraph under ``Additional AD 
Provisions.'' This new format includes a ``New Provisions for 
Alternative Actions, Intervals, and CDCCLs'' paragraph that does not 
specifically refer to AMOCs, but operators may still request an AMOC to 
use an alternative action, interval, or CDCCL.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 134 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed AD:
    The FAA estimates the total cost per operator for the retained 
actions from AD 2023-22-13 to be $7,650 (90 work-hours x $85 per work-
hour).
    The FAA has determined that revising the existing maintenance or 
inspection program takes an average of 90 work-hours per operator, 
although the agency recognizes that this number may vary from operator 
to operator. Since operators incorporate maintenance or inspection 
program changes for their affected fleet(s), the FAA has determined 
that a per-operator estimate is more accurate than a per-airplane 
estimate.
    The FAA estimates the total cost per operator for the new proposed 
actions to be $7,650 (90 work-hours x $85 per work-hour).

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

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would 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 Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator,

[[Page 41364]]

the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by:
0
a. Removing Airworthiness Directive (AD) 2023-22-13, Amendment 39-22597 
(88 FR 82246, November 24, 2023); and
0
b. Adding the following new AD:

Dassault Aviation: Docket No. FAA-2024-1290; Project Identifier 
MCAI-2024-00078-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by June 27, 2024.

(b) Affected ADs

    (1) This AD replaces AD 2023-22-13, Amendment 39-22597 (88 FR 
82246, November 24, 2023) (AD 2023-22-13).
    (2) This AD affects AD 2014-16-23, Amendment 39-17947 (79 FR 
52545, September 4, 2014) (AD 2014-16-23)

(c) Applicability

    This AD applies to Dassault Aviation Model FALCON 7X airplanes, 
certificated in any category, with an original airworthiness 
certificate or original export certificate of airworthiness issued 
on or before September 7, 2023.
    Note 1 to paragraph (c): Model FALCON 7X airplanes with 
modification M1000 incorporated are commonly referred to as ``Model 
FALCON 8X'' airplanes as a marketing designation.

(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 reduced structural integrity and reduced 
control of the airplane due to the failure of system components.

(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 (j) of AD 
2023-22-13, with a new terminating action. For airplanes with an 
original airworthiness certificate or original export certificate of 
airworthiness issued on or before September 7, 2022, 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 2023-0063, dated 
March 20, 2023 (EASA AD 2023-0063). 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 2023-0063, With No Changes

    This paragraph restates the exceptions specified in paragraph 
(k) of AD 2023-22-13, with no changes.
    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2023-0063.
    (2) Paragraph (3) of EASA AD 2023-0063 specifies revising ``the 
approved AMP [aircraft maintenance program]'' within 12 months after 
its effective date, but this AD requires revising the existing 
maintenance or inspection program, as applicable, within 90 days 
after December 29, 2023 (the effective date of AD 2023-22-13).
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2023-0063 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2023-0063, or within 90 
days after December 29, 2023 (the effective date of AD 2023-22-13), 
whichever occurs later.
    (4) This AD does not adopt the provisions specified in 
paragraphs (4) and (5) of EASA AD 2023-0063.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0063.

(i) Retained Restrictions on Alternative Actions, Intervals, and 
Critical Design Configuration Control Limitations (CDCCLs), With a New 
Exception

    This paragraph restates the requirements of paragraph (l) of AD 
2023-22-13, 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), intervals, or CDCCLs are allowed unless 
they are approved as specified in the provisions of the ``Ref. 
Publications'' section of EASA AD 2023-0063.

(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 2024-0033, dated January 31, 2024 (EASA AD 
2024-0033). 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 2024-0033

    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2024-0033.
    (2) Paragraph (3) of EASA AD 2024-0033 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.
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2024-0033 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2024-0033, or within 90 
days after the effective date of this AD, whichever occurs later.
    (4) This AD does not adopt the provisions specified in 
paragraphs (4) and (5) of EASA AD 2024-0033.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2024-0033.

(l) New Provisions for Alternative Actions, Intervals, and CDCCLs

    After the existing maintenance or inspection program has been 
revised as required by paragraph (j) of this AD, no alternative 
actions (e.g., inspections), intervals, and CDCCLs are allowed 
unless they are approved as specified in the provisions of the 
``Ref. Publications'' section of EASA AD 2024-0033.

(m) Terminating Action for Certain Requirements in AD 2014-16-23

    Accomplishing the actions required by paragraphs (g) or (j) of 
this AD terminates the requirements of paragraph (q) of AD 2014-16-
23.

(n) 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 (o) of this AD. Information may be emailed to: [email protected]. 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 EASA; or Dassault Aviation's EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.

(o) Additional Information

    For more information about this AD, contact Tom Rodriguez, 
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, 
Westbury, NY 11590; telephone 206-231-3226; email: 
[email protected].

(p) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this

[[Page 41365]]

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 
[DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE].
    (i) European Union Aviation Safety Agency (EASA) AD 2024-0033, 
dated January 31, 2024.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
December 29, 2023 (88 FR 82246, November 24, 2023).
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0063, 
dated March 20, 2023.
    (ii) [Reserved]
    (5) For EASA ADs 2024-0033 and 2023-0063, 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 service information 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 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/[email protected]">www.archives.gov/federal-register/cfr/[email protected].

    Issued on April 26, 2024.
James D. Foltz,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2024-09511 Filed 5-10-24; 8:45 am]
BILLING CODE 4910-13-P
This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.