Airworthiness Directives; Dassault Aviation Airplanes, 86029-86032 [2023-27117]

Download as PDF 86029 Rules and Regulations Federal Register Vol. 88, No. 237 Tuesday, December 12, 2023 This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. DEPARTMENT OF DEFENSE Office of the Secretary 5 CFR Part 3601 RIN 0790–AL21 Supplemental Standards of Ethical Conduct for Employees of the Department of Defense; Correction Department of Defense (DoD). Final rule; correcting amendment. AGENCY: ACTION: The Department of Defense is correcting a final rule that appeared in the Federal Register on February 28, 2023. The Department of Defense, with the concurrence of the U.S. Office of Government Ethics (OGE), finalized amendments to its Supplemental Standards of Ethical Conduct for Employees of the Department of Defense (DoD Supplemental Regulation). The amendments revised and updated the DoD Supplemental Regulation originally written in 1993, to supplement the OGE Standards of Ethical Conduct for Employees of the Executive Branch (OGE Standards). Amendments included changes in the following areas: designation of separate agency components for the purposes of gifts and teaching, speaking, and writing; additional exceptions for gifts from outside sources; additional limitations on gifts between DoD employees; and authority to waive any of the provisions of the DoD Supplemental Regulation. DATES: This final rule correction is effective December 12, 2023 and is applicable beginning March 30, 2023. FOR FURTHER INFORMATION CONTACT: Karen Dalheim, Standards of Conduct Office, Office of the Secretary of Defense, Office of the General Counsel; telephone: 703–695–3422. SUPPLEMENTARY INFORMATION: Subsequent to the publication of the final rule on February 28, 2023 (88 FR ddrumheller on DSK120RN23PROD with RULES1 VerDate Sep<11>2014 15:47 Dec 11, 2023 Jkt 262001 DEPARTMENT OF TRANSPORTATION List of Subjects in 5 CFR Part 3601 RIN 2120–AA64 Conflict of interests, Executive branch standards of conduct, Government employees. Airworthiness Directives; Dassault Aviation Airplanes Accordingly, the Department of Defense amends 5 CFR part 3601 by making the following correcting amendment: [Docket ID: DoD–2021–OS–0032] SUMMARY: 12541), it was discovered that during the final review and editing of the final rule, a comma was moved in the first sentence of § 3601.106(a) introductory text that changed the meaning of the sentence. The document corrects the CFR to reflect the intended version of this paragraph. PART 3601—SUPPLEMENTAL STANDARDS OF ETHICAL CONDUCT FOR EMPLOYEES OF THE DEPARTMENT OF DEFENSE 1. The authority citation for part 3601 continues to read as follows: ■ Authority: 5 U.S.C. 301, 7301, 7351, 7353; 5 U.S.C. Chapter 131; E.O. 12674, 54 FR 15159, 3 CFR, 1989 Comp., p. 215, as modified by E.O. 12731, 55 FR 42547, 3 CFR, 1990 Comp., p. 306; 5 CFR 2635.105, 2635.203(a), 2635.204(k), 2635.803, 2635.807. 2. In § 3601.106, revise the first sentence of paragraph (a) introductory text to read as follows: ■ § 3601.106 Prior approval for outside employment and business activities. (a) A DoD employee, other than a special Government employee, who is required to file a financial disclosure report (OGE Forms 450 or 278e) shall obtain approval from the agency designee before engaging in a business activity or compensated outside employment with a prohibited source, unless general approval has been given in accordance with paragraph (b) of this section. * * * * * * * * Dated: December 6, 2023. Patricia L. Toppings, OSD Federal Register Liaison Officer, Department of Defense. [FR Doc. 2023–27172 Filed 12–11–23; 8:45 am] BILLING CODE 6001–FR–P PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2023–1721; Project Identifier MCAI–2023–00676–T; Amendment 39–22608; AD 2023–23–06] Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is superseding Airworthiness Directive (AD) 2023–04– 13, which applied to certain Dassault Aviation Model FALCON 2000EX airplanes. AD 2023–04–13 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2023–04–13 and requires 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 incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 16, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 16, 2024. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of May 12, 2023 (88 FR 20741, April 7, 2023). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–1721; 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 final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The address for Docket Operations is U.S. Department of SUMMARY: E:\FR\FM\12DER1.SGM 12DER1 86030 Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Rules and Regulations Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For material incorporated by reference in this AD, 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 in the AD docket at regulations.gov under Docket No. FAA– 2023–1721. 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. SUPPLEMENTARY INFORMATION: ddrumheller on DSK120RN23PROD with RULES1 Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2023–04–13, Amendment 39–22360 (88 FR 20741, April 7, 2023) (AD 2023–04–13). AD 2023–04–13 applied to certain Dassault Aviation Model FALCON 2000EX airplanes. AD 2023–04–13 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2023–04–13 to address reduced structural integrity of the airplane. AD 2023–04–13 specifies that accomplishing the revision required by paragraph (g) or (j) of that AD terminates the requirements of paragraph (g)(1) of AD 2010–26–05, Amendment 39–16544 (75 FR 79952, December 21, 2010), for Dassault Aviation Model FALCON 2000EX airplanes. This AD therefore continues to allow that terminating action. The NPRM published in the Federal Register on August 29, 2023 (88 FR 59476). The NPRM was prompted by AD 2023–0100, dated May 11, 2023, issued by EASA, which is the Technical Agent for the Member States of the European Union (EASA AD 2023–0100) (also referred to as the MCAI). The MCAI states that new or more restrictive airworthiness limitations have been developed. In the NPRM, the FAA proposed to continue to require the actions in AD VerDate Sep<11>2014 15:47 Dec 11, 2023 Jkt 262001 2023–04–13. The NPRM also proposed to require revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations, as specified in EASA AD 2023–0100. The FAA is issuing this AD to address reduced structural integrity of the airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2023–1721. Discussion of Final Airworthiness Directive Comments The FAA received no comments on the NPRM or on the determination of the cost to the public. 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, 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 2023–0100 specifies new or more restrictive airworthiness limitations for airplane structures and safe life limits. This AD also requires EASA AD 2022–0136, dated July 6, 2022, which the Director of the Federal Register approved for incorporation by reference as of May 12, 2023 (88 FR 20741, April 7, 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 the ADDRESSES section. Costs of Compliance The FAA estimates that this AD affects 245 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: The FAA estimates the total cost per operator for the retained actions from AD 2023–04–13 to be $7,650 (90 workhours × $85 per work-hour). The FAA has determined that revising the existing maintenance or inspection PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 program takes an average of 90 workhours per operator, although the agency recognizes that this number may vary from operator to operator. In the past, the agency has estimated that this action takes 1 work-hour per airplane. 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 actions to be $7,650 (90 work-hours × $85 per workhour). 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. E:\FR\FM\12DER1.SGM 12DER1 Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Rules and Regulations (EASA AD 2022–0136). Accomplishing the revision of the existing maintenance or inspection program required by paragraph (j) of this AD terminates the requirements of this paragraph. 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: a. Removing Airworthiness Directive (AD) 2023–04–13, Amendment 39– 22360 (88 FR 20741, April 7, 2023); and ■ b. Adding the following new AD: ■ ■ 2023–23–06 Dassault Aviation: Amendment 39–22608; Docket No. FAA–2023–1721; Project Identifier MCAI–2023–00676–T. (a) Effective Date This airworthiness directive (AD) is effective January 16, 2024. (b) Affected ADs (1) This AD replaces AD 2023–04–13, Amendment 39–22360 (88 FR 20741, April 7, 2023) (AD 2023–04–13). (2) This AD affects AD 2010–26–05, Amendment 39–16544 (75 FR 79952, December 21, 2010) (AD 2010–26–05). (c) Applicability This AD applies to Dassault Aviation Model FALCON 2000EX airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before January 15, 2023. (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 of the airplane. ddrumheller on DSK120RN23PROD with RULES1 (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Maintenance or Inspection Program Revision, With No Changes This paragraph restates the requirements of paragraph (j) of AD 2023–04–13, with no changes. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before January 15, 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 2022–0136, dated July 6, 2022 VerDate Sep<11>2014 15:47 Dec 11, 2023 Jkt 262001 (h) Retained Exceptions to EASA AD 2022– 0136, With No Changes This paragraph restates the exceptions specified in paragraph (k) of AD 2023–04–13, with no changes. (1) The requirements specified in paragraphs (1) and (2) of EASA AD 2022– 0136 do not apply to this AD. (2) Paragraph (3) of EASA AD 2022–0136 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 May 12, 2023 (the effective date of AD 2023–04–13). (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2022–0136 is at the applicable ‘‘limitation’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2022–0136, or within 90 days after the May 12, 2023 (the effective date of AD 2023–04–13), whichever occurs later. (4) The provisions specified in paragraphs (4) and (5) of EASA AD 2022–0136 do not apply to this AD. (5) The ‘‘Remarks’’ section of EASA AD 2022–0136 does not apply to this AD. (i) Retained Provisions for Alternative Actions or Intervals, With a New Exception This paragraph restates the requirements of paragraph (l) of AD 2023–04–13, with a new exception. Except as required by paragraph (j) of this AD, after the existing maintenance or inspection program has been revised as required by paragraph (g) of this AD, no alternative actions (e.g., inspections) or intervals may be used unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2022–0136. (j) New Maintenance or Inspection Program Revision 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 2023–0100, dated May 11, 2023 (EASA AD 2023–0100). 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 2023–0100 (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2023–0100. (2) Paragraph (3) of EASA AD 2023–0100 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 2023–0100 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 86031 incorporated by the requirements of paragraph (3) of EASA AD 2023–0100, 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 2023–0100. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2023–0100. (l) New Provisions for Alternative Actions and Intervals After the maintenance or inspection program has been revised as required by paragraph (j) of this AD, no alternative actions (e.g., inspections), and intervals are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2023– 0100. (m) Terminating Action for Certain Actions in AD 2010–26–05 Accomplishing the actions required by paragraph (g) or (j) of this AD terminates the requirements of paragraph (g)(1) of AD 2010– 26–05, for Dassault Aviation Model FALCON 2000EX airplanes only. (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 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. E:\FR\FM\12DER1.SGM 12DER1 86032 Federal Register / Vol. 88, No. 237 / Tuesday, December 12, 2023 / Rules and Regulations (3) The following service information was approved for IBR on January 16, 2024. (i) European Union Aviation Safety Agency (EASA) AD 2023–0100, dated May 11, 2023. (ii) [Reserved] (4) The following service information was approved for IBR on May 12, 2023 (88 FR 20741, April 7, 2023). (i) European Union Aviation Safety Agency (EASA) AD 2022–0136, dated July 6, 2022. (ii) [Reserved] (5) For EASA ADs 2022–0136 and 2023– 0100, 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: ad.easa.europa.eu. (6) You may view this service information 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. (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-locations or email fr.inspection@nara.gov. Issued on November 9, 2023. Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2023–27117 Filed 12–11–23; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2023–1815; Project Identifier MCAI–2023–00581–T; Amendment 39–22606; AD 2023–23–04] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A321–111, –112, –131, –211, –212, –213, –231, and –232 airplanes. This AD was prompted by stress analysis results indicating that cracks may appear in the center wing box at frame 42 and slanted junction areas. This AD requires a one-time inspection of the center wing box at frame 42 and slanted junction areas, and applicable corrective actions, if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. ddrumheller on DSK120RN23PROD with RULES1 SUMMARY: VerDate Sep<11>2014 15:47 Dec 11, 2023 Jkt 262001 The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 16, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 16, 2024. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–1815; 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 final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. Material Incorporated by Reference: • For material incorporated by reference in this AD, 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 in the AD docket at regulations.gov under Docket No. FAA– 2023–1815. FOR FURTHER INFORMATION CONTACT: Tim Dowling, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206– 231–3667; email: timothy.p.dowling@ faa.gov. SUPPLEMENTARY INFORMATION: that cracks may appear in the center wing box at frame 42 and slanted junction areas of the affected airplanes. Cracks may appear due to the high fatigue stress in affected areas. In the NPRM, the FAA proposed to require a one-time inspection of the center wing box at frame 42 and slanted junction areas, and applicable corrective actions, if necessary, as specified in EASA AD 2023–0074. The FAA is issuing this AD to detect potential cracks in the center wing box at frame 42 and slanted junction areas. The unsafe condition, if not addressed, could affect the structural integrity of the fuselage. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2023–1815. Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Airbus SAS Model A321– 111, –112, –131, –211, –212, –213, –231, and –232 airplanes. The NPRM published in the Federal Register on September 6, 2023 (88 FR 60908). The NPRM was prompted by AD 2023–0074, dated April 5, 2023, issued by EASA, which is the Technical Agent for the Member States of the European Union (EASA AD 2023–0074) (also referred to as the MCAI). The MCAI states that stress analysis results from A321 XLR certification and fatigue and damage tolerance harmonization have revealed EASA AD 2023–0074 specifies procedures for one-time rototest and high frequency eddy current inspections for cracks of the center wing box rear lower spar junction area at frame 42; a rototest inspection for cracks of the frame 42 slanted beam connection; a detailed visual inspection of certain fasteners for damage; and applicable corrective actions. Corrective actions include obtaining and following instructions for crack repair and replacing damaged fasteners. 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. PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 Discussion of Final Airworthiness Directive Comments The FAA received no comments on the NPRM or on the determination of the cost to the public. 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, 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 E:\FR\FM\12DER1.SGM 12DER1

Agencies

[Federal Register Volume 88, Number 237 (Tuesday, December 12, 2023)]
[Rules and Regulations]
[Pages 86029-86032]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-27117]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1721; Project Identifier MCAI-2023-00676-T; 
Amendment 39-22608; AD 2023-23-06]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-04-
13, which applied to certain Dassault Aviation Model FALCON 2000EX 
airplanes. AD 2023-04-13 required revising the existing maintenance or 
inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations. This AD was prompted by a 
determination that new or more restrictive airworthiness limitations 
are necessary. This AD continues to require the actions in AD 2023-04-
13 and requires 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 incorporated by reference. The FAA is 
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective January 16, 2024.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of January 16, 
2024.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of May 
12, 2023 (88 FR 20741, April 7, 2023).

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-1721; 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 final rule, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
address for Docket Operations is U.S. Department of

[[Page 86030]]

Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
    Material Incorporated by Reference:
     For material incorporated by reference in this AD, 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 in the AD docket at 
regulations.gov under Docket No. FAA-2023-1721.

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: 

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 to supersede AD 2023-04-13, Amendment 39-22360 (88 FR 
20741, April 7, 2023) (AD 2023-04-13). AD 2023-04-13 applied to certain 
Dassault Aviation Model FALCON 2000EX airplanes. AD 2023-04-13 required 
revising the existing maintenance or inspection program, as applicable, 
to incorporate new or more restrictive airworthiness limitations. The 
FAA issued AD 2023-04-13 to address reduced structural integrity of the 
airplane. AD 2023-04-13 specifies that accomplishing the revision 
required by paragraph (g) or (j) of that AD terminates the requirements 
of paragraph (g)(1) of AD 2010-26-05, Amendment 39-16544 (75 FR 79952, 
December 21, 2010), for Dassault Aviation Model FALCON 2000EX 
airplanes. This AD therefore continues to allow that terminating 
action.
    The NPRM published in the Federal Register on August 29, 2023 (88 
FR 59476). The NPRM was prompted by AD 2023-0100, dated May 11, 2023, 
issued by EASA, which is the Technical Agent for the Member States of 
the European Union (EASA AD 2023-0100) (also referred to as the MCAI). 
The MCAI states that new or more restrictive airworthiness limitations 
have been developed.
    In the NPRM, the FAA proposed to continue to require the actions in 
AD 2023-04-13. The NPRM also proposed to require revising the existing 
maintenance or inspection program, as applicable, to incorporate new or 
more restrictive airworthiness limitations, as specified in EASA AD 
2023-0100. The FAA is issuing this AD to address reduced structural 
integrity of the airplane.
    You may examine the MCAI in the AD docket at regulations.gov under 
Docket No. FAA-2023-1721.

Discussion of Final Airworthiness Directive

Comments

    The FAA received no comments on the NPRM or on the determination of 
the cost to the public.

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, 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 2023-0100 specifies new or more restrictive airworthiness 
limitations for airplane structures and safe life limits.
    This AD also requires EASA AD 2022-0136, dated July 6, 2022, which 
the Director of the Federal Register approved for incorporation by 
reference as of May 12, 2023 (88 FR 20741, April 7, 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 the ADDRESSES section.

Costs of Compliance

    The FAA estimates that this AD affects 245 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:
    The FAA estimates the total cost per operator for the retained 
actions from AD 2023-04-13 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. In the past, the agency has estimated that this action 
takes 1 work-hour per airplane. 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 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

    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.

[[Page 86031]]

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

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) 2023-04-13, Amendment 39-22360 
(88 FR 20741, April 7, 2023); and
0
b. Adding the following new AD:

2023-23-06 Dassault Aviation: Amendment 39-22608; Docket No. FAA-
2023-1721; Project Identifier MCAI-2023-00676-T.

(a) Effective Date

    This airworthiness directive (AD) is effective January 16, 2024.

(b) Affected ADs

    (1) This AD replaces AD 2023-04-13, Amendment 39-22360 (88 FR 
20741, April 7, 2023) (AD 2023-04-13).
    (2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 
79952, December 21, 2010) (AD 2010-26-05).

(c) Applicability

    This AD applies to Dassault Aviation Model FALCON 2000EX 
airplanes, certificated in any category, with an original 
airworthiness certificate or original export certificate of 
airworthiness issued on or before January 15, 2023.

(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 of the 
airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Retained Maintenance or Inspection Program Revision, With No 
Changes

    This paragraph restates the requirements of paragraph (j) of AD 
2023-04-13, with no changes. For airplanes with an original 
airworthiness certificate or original export certificate of 
airworthiness issued on or before January 15, 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 2022-0136, dated 
July 6, 2022 (EASA AD 2022-0136). 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 2022-0136, With No Changes

    This paragraph restates the exceptions specified in paragraph 
(k) of AD 2023-04-13, with no changes.
    (1) The requirements specified in paragraphs (1) and (2) of EASA 
AD 2022-0136 do not apply to this AD.
    (2) Paragraph (3) of EASA AD 2022-0136 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 May 12, 2023 (the effective date 
of AD 2023-04-13).
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2022-0136 is at the applicable 
``limitation'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0136, or within 90 
days after the May 12, 2023 (the effective date of AD 2023-04-13), 
whichever occurs later.
    (4) The provisions specified in paragraphs (4) and (5) of EASA 
AD 2022-0136 do not apply to this AD.
    (5) The ``Remarks'' section of EASA AD 2022-0136 does not apply 
to this AD.

(i) Retained Provisions for Alternative Actions or Intervals, With a 
New Exception

    This paragraph restates the requirements of paragraph (l) of AD 
2023-04-13, with a new exception. Except as required by paragraph 
(j) of this AD, after the existing maintenance or inspection program 
has been revised as required by paragraph (g) of this AD, no 
alternative actions (e.g., inspections) or intervals may be used 
unless they are approved as specified in the provisions of the 
``Ref. Publications'' section of EASA AD 2022-0136.

(j) New Maintenance or Inspection Program Revision

    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 2023-0100, dated May 11, 2023 (EASA AD 
2023-0100). 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 2023-0100

    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2023-0100.
    (2) Paragraph (3) of EASA AD 2023-0100 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 2023-0100 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2023-0100, 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 2023-0100.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0100.

(l) New Provisions for Alternative Actions and Intervals

    After the maintenance or inspection program has been revised as 
required by paragraph (j) of this AD, no alternative actions (e.g., 
inspections), and intervals are allowed unless they are approved as 
specified in the provisions of the ``Ref. Publications'' section of 
EASA AD 2023-0100.

(m) Terminating Action for Certain Actions in AD 2010-26-05

    Accomplishing the actions required by paragraph (g) or (j) of 
this AD terminates the requirements of paragraph (g)(1) of AD 2010-
26-05, for Dassault Aviation Model FALCON 2000EX airplanes only.

(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 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.

[[Page 86032]]

    (3) The following service information was approved for IBR on 
January 16, 2024.
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0100, 
dated May 11, 2023.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
May 12, 2023 (88 FR 20741, April 7, 2023).
    (i) European Union Aviation Safety Agency (EASA) AD 2022-0136, 
dated July 6, 2022.
    (ii) [Reserved]
    (5) For EASA ADs 2022-0136 and 2023-0100, 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: ad.easa.europa.eu.
    (6) You may view this service information 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.
    (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-locations or email [email protected].

    Issued on November 9, 2023.
Ross Landes,
Deputy Director for Regulatory Operations, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2023-27117 Filed 12-11-23; 8:45 am]
BILLING CODE 4910-13-P

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