Airworthiness Directives; Dassault Aviation Airplanes, 68454-68456 [2023-22068]

Download as PDF 68454 Federal Register / Vol. 88, No. 191 / Wednesday, October 4, 2023 / Rules and Regulations DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2023–1495; Project Identifier MCAI–2023–00492–T; Amendment 39–22564; AD 2023–20–05] RIN 2120–AA64 Airworthiness Directives; Dassault Aviation Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is superseding Airworthiness Directive (AD) 2020–03– 24, which applied to certain Dassault Aviation Model MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes. AD 2020–03–24 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 2020–03–24 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 November 8, 2023. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 8, 2023. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of April 2, 2020 (85 FR 11289, February 27, 2020). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–1495; 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: lotter on DSK11XQN23PROD with RULES1 SUMMARY: VerDate Sep<11>2014 17:03 Oct 03, 2023 Jkt 262001 • For EASA 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. • For Dassault Aviation service information incorporated by reference in this AD, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201–440–6700; website: dassaultfalcon.com. • 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– 2023–1495. FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 206–231– 3226; email: tom.rodriguez@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2020–03–24, Amendment 39–19848 (85 FR 11289, February 27, 2020) (AD 2020–03–24). AD 2020–03–24 applied to certain Dassault Aviation Model MYSTERE– FALCON 20–C5, 20–D5, 20–E5, and 20– F5 airplanes. AD 2020–03–24 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2020–03–24 to address fatigue cracking, damage, and corrosion in principal structural elements, which could result in reduced structural integrity of the airplane. AD 2020–03– 24 specifies that accomplishing the revision required by that AD terminates the requirements of paragraph (g)(1) of AD 2010–26–05, Amendment 39–16544 (75 FR 79952, December 21, 2010), for Model MYSTERE–FALCON 20–C5, 20– D5, 20–E5, and 20–F5 airplanes on which the SSIP [Supplemental Structural Inspection Program (Dassault Service Bulletin 730)] has been embodied into the airplane’s existing maintenance or inspection program only. This AD therefore continues to allow that terminating action. The NPRM published in the Federal Register on July 19, 2023 (88 FR 46115). The NPRM was prompted by AD 2023– 0062, dated March 20, 2023, issued by PO 00000 Frm 00004 Fmt 4700 Sfmt 4700 EASA, (EASA AD 2023–0062) (also referred to as the MCAI), which is the Technical Agent for the Member States of the European Union. 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 2020–03–24 and 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 2023–0062. The FAA is issuing this AD to address fatigue cracking, damage, and corrosion in principal structural elements, which could result in reduced structural integrity of the airplane. You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2023–1495. 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 2023–0062 specifies new or more restrictive airworthiness limitations for airplane structures and safe life limits. This AD also requires Chapter 5–40– 01, Airworthiness Limitations, of the Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, dated January 1, 2019, which the Director of the Federal Register approved for incorporation by reference as of April 2, 2020 (85 FR 11289, February 27, 2020). This material is reasonably available because the interested parties have access to it through their normal course E:\FR\FM\04OCR1.SGM 04OCR1 Federal Register / Vol. 88, No. 191 / Wednesday, October 4, 2023 / Rules and Regulations of business or by the means identified in the ADDRESSES section. Costs of Compliance The FAA estimates that this AD affects 57 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 2020–03–24 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 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 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. lotter on DSK11XQN23PROD with RULES1 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, VerDate Sep<11>2014 17:03 Oct 03, 2023 Jkt 262001 (2) Will not affect intrastate aviation in Alaska, and (3) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by: a. Removing Airworthiness Directive (AD) 2020–03–24, Amendment 39– 19848 (85 FR 11289, February 27, 2020); and ■ b. Adding the following new AD: ■ ■ 2023–20–05 Dassault Aviation: Amendment 39–22564; Docket No. FAA–2023–1495; Project Identifier MCAI–2023–00492–T. (a) Effective Date This airworthiness directive (AD) is effective November 8, 2023. (b) Affected ADs (1) This AD replaces AD 2020–03–24, Amendment 39–19848 (85 FR 11289, February 27, 2020) (AD 2020–03–24). (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 MYSTERE–FALCON 20–C5, 20–D5, 20–E5, and 20–F5 airplanes, certificated in any category, on which the Supplemental Structural Inspection Program (SSIP) (Dassault Service Bulletin 730) has been embodied into the airplane’s existing maintenance or inspection program. (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 fatigue cracking, damage, and corrosion in principal structural elements, which could result in reduced structural integrity of the airplane. PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 68455 (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 No Changes This paragraph restates the requirements of paragraph (g) of AD 2020–03–24, with no changes. Within 90 days after April 2, 2020 (the effective date of AD 2020–03–24), revise the existing maintenance or inspection program, as applicable, to incorporate the information specified in Chapter 5–40–01, Airworthiness Limitations, of the Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, dated January 1, 2019. The initial compliance time for doing the tasks is at the applicable time specified in Chapter 5– 40–01, Airworthiness Limitations, of the Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, dated January 1, 2019; or within 90 days after April 2, 2020; whichever occurs later. Accomplishing the revision of the existing maintenance or inspection program required by paragraph (i) of this AD terminates the requirements of this paragraph. (h) Retained No Alternative Actions or Intervals, With a New Exception This paragraph restates the requirements of paragraph (h) of AD 2020–03–24, with a new exception. Except as required by paragraph (i) 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 the actions or intervals are approved as an alternative method of compliance (AMOC) in accordance with the procedures specified in paragraph (m)(1) of this AD. (i) New Revision of the Existing Maintenance or Inspection Program Except as specified in paragraph (j) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2023–0062, dated March 20, 2023 (EASA AD 2023–0062). Accomplishing the revision of the existing maintenance or inspection program required by this paragraph terminates the requirements of paragraph (g) of this AD. (j) Exceptions to EASA AD 2023–0062 (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2023–0062. (2) Paragraph (3) of EASA AD 2023–0062 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 2023–0062 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2023–0062 or within 90 days after the effective date of this AD, whichever occurs later. E:\FR\FM\04OCR1.SGM 04OCR1 68456 Federal Register / Vol. 88, No. 191 / Wednesday, October 4, 2023 / Rules and Regulations (4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2023–0062. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2023–0062. (k) New Provisions for Alternative Actions and Intervals After the existing maintenance or inspection program has been revised as required by paragraph (i) 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 2023–0062. (l) Terminating Action for AD 2010–26–05 Accomplishing the actions required by paragraph (g) or (i) of this AD terminates the requirements of paragraph (g)(1) of AD 2010– 26–05, for Model MYSTERE–FALCON 20– C5, 20–D5, 20–E5, and 20–F5 airplanes on which the SSIP has been embodied into the airplane’s existing maintenance or inspection program only. (m) Additional AD Provisions lotter on DSK11XQN23PROD with RULES1 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 (n) 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. (i) European Union Aviation Safety Agency (EASA) AD 2023–0062, dated March 20, 2023. (ii) [Reserved] (4) The following service information was approved for IBR on April 2, 2020 (85 FR 11289, February 27, 2020). (i) Chapter 5–40–01, Airworthiness Limitations, of the Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, dated January 1, 2019. (ii) [Reserved] (5) For EASA AD 2023–0062, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email: ADs@easa.europa.eu; website: easa.europa.eu. You may find this EASA AD on the EASA website: ad.easa.europa.eu. (6) For Dassault Aviation service information identified in this AD, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201–440–6700; website dassaultfalcon.com. (7) 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. (8) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to: www.archives.gov/federal-register/cfr/ibrlocations.html. Issued on September 28, 2023. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2023–22068 Filed 10–3–23; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF THE TREASURY Internal Revenue Service 26 CFR Part 300 [TD 9980] RIN 1545–BQ78 (n) Additional Information For more information about this AD, contact Tom Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 206–231– 3226; email: tom.rodriguez@faa.gov. Preparer Tax Identification Number (PTIN) User Fee Update (o) 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. (3) The following service information was approved for IBR on November 8, 2023. SUMMARY: VerDate Sep<11>2014 17:03 Oct 03, 2023 Jkt 262001 Internal Revenue Service (IRS), Treasury. ACTION: Interim final rule. AGENCY: This document contains interim final regulations relating to the imposition of certain user fees on tax return preparers. These regulations reduce the amount of the user fee to apply for or renew a preparer tax identification number (PTIN) and affect individuals who apply for or renew a PTIN. The Independent Offices Appropriation Act of 1952 authorizes PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 the charging of user fees. The text of the interim final regulations also serves as the text of the proposed regulations set forth in the notice of proposed rulemaking on this subject in this issue in the Proposed Rules section of this edition of the Federal Register. DATES: Effective date: These regulations are effective on October 19, 2023. Applicability date: For date of applicability, see paragraph (d) of these interim final regulations. FOR FURTHER INFORMATION CONTACT: Concerning the interim final regulations, Jamie Song at (202) 317– 6845; concerning cost methodology, Michael A. Weber at (202) 803–9738 (not toll-free numbers). SUPPLEMENTARY INFORMATION: Background This document contains interim final amendments to 26 CFR part 300 regarding user fees. A. User Fee Authority The Independent Offices Appropriation Act of 1952 (IOAA), which is codified at 31 U.S.C. 9701, authorizes agencies to prescribe regulations that establish user fees for services provided by the agency. The IOAA provides that regulations implementing user fees are subject to policies prescribed by the President; these policies are set forth in the Office of Management and Budget Circular A– 25, 58 FR 38142 (July 15, 1993) (OMB Circular A–25). Under OMB Circular A–25, Federal agencies that provide services that confer benefits on identifiable recipients are to establish user fees that recover the full cost of providing the service. An agency that seeks to impose a user fee for government-provided services must calculate the full cost of providing those services. In general, a user fee should be set at an amount that allows the agency to recover the direct and indirect costs of providing the service, unless the Office of Management and Budget (OMB) grants an exception. OMB Circular A–25 provides that agencies are to review user fees biennially and update them as necessary. B. PTIN Requirement Section 6109(a)(4) of the Internal Revenue Code (Code) authorizes the Secretary of the Treasury or her delegate to prescribe regulations for the inclusion of a tax return preparer’s identifying number on a return, statement, or other document required to be filed with the IRS. On September 30, 2010, the Treasury Department and the IRS E:\FR\FM\04OCR1.SGM 04OCR1

Agencies

[Federal Register Volume 88, Number 191 (Wednesday, October 4, 2023)]
[Rules and Regulations]
[Pages 68454-68456]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-22068]



[[Page 68454]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1495; Project Identifier MCAI-2023-00492-T; 
Amendment 39-22564; AD 2023-20-05]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-03-
24, which applied to certain Dassault Aviation Model MYSTERE-FALCON 20-
C5, 20-D5, 20-E5, and 20-F5 airplanes. AD 2020-03-24 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 2020-03-24 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 November 8, 2023.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of November 8, 
2023.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of April 
2, 2020 (85 FR 11289, February 27, 2020).

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-1495; 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 EASA 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.
     For Dassault Aviation service information incorporated by 
reference in this AD, contact Dassault Falcon Jet Corporation, 
Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 
201-440-6700; website: dassaultfalcon.com.
     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-2023-1495.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aviation Safety 
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; 
phone: 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 2020-03-24, Amendment 39-19848 (85 FR 
11289, February 27, 2020) (AD 2020-03-24). AD 2020-03-24 applied to 
certain Dassault Aviation Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 
20-F5 airplanes. AD 2020-03-24 required revising the existing 
maintenance or inspection program, as applicable, to incorporate new or 
more restrictive airworthiness limitations. The FAA issued AD 2020-03-
24 to address fatigue cracking, damage, and corrosion in principal 
structural elements, which could result in reduced structural integrity 
of the airplane. AD 2020-03-24 specifies that accomplishing the 
revision required by that AD terminates the requirements of paragraph 
(g)(1) of AD 2010-26-05, Amendment 39-16544 (75 FR 79952, December 21, 
2010), for Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 
airplanes on which the SSIP [Supplemental Structural Inspection Program 
(Dassault Service Bulletin 730)] has been embodied into the airplane's 
existing maintenance or inspection program only. This AD therefore 
continues to allow that terminating action.
    The NPRM published in the Federal Register on July 19, 2023 (88 FR 
46115). The NPRM was prompted by AD 2023-0062, dated March 20, 2023, 
issued by EASA, (EASA AD 2023-0062) (also referred to as the MCAI), 
which is the Technical Agent for the Member States of the European 
Union. 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 2020-03-24 and 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-
0062. The FAA is issuing this AD to address fatigue cracking, damage, 
and corrosion in principal structural elements, which could result in 
reduced structural integrity of the airplane.
    You may examine the MCAI in the AD docket at regulations.gov under 
Docket No. FAA-2023-1495.

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 2023-0062 specifies new or more restrictive airworthiness 
limitations for airplane structures and safe life limits.
    This AD also requires Chapter 5-40-01, Airworthiness Limitations, 
of the Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, 
dated January 1, 2019, which the Director of the Federal Register 
approved for incorporation by reference as of April 2, 2020 (85 FR 
11289, February 27, 2020).
    This material is reasonably available because the interested 
parties have access to it through their normal course

[[Page 68455]]

of business or by the means identified in the ADDRESSES section.

Costs of Compliance

    The FAA estimates that this AD affects 57 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 2020-03-24 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 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.

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) 2020-03-24, Amendment 39-19848 
(85 FR 11289, February 27, 2020); and
0
b. Adding the following new AD:

2023-20-05 Dassault Aviation: Amendment 39-22564; Docket No. FAA-
2023-1495; Project Identifier MCAI-2023-00492-T.

(a) Effective Date

    This airworthiness directive (AD) is effective November 8, 2023.

(b) Affected ADs

    (1) This AD replaces AD 2020-03-24, Amendment 39-19848 (85 FR 
11289, February 27, 2020) (AD 2020-03-24).
    (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 MYSTERE-FALCON 20-C5, 
20-D5, 20-E5, and 20-F5 airplanes, certificated in any category, on 
which the Supplemental Structural Inspection Program (SSIP) 
(Dassault Service Bulletin 730) has been embodied into the 
airplane's existing maintenance or inspection program.

(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 fatigue cracking, damage, and corrosion 
in principal structural elements, which could result in reduced 
structural integrity of the airplane.

(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 No Changes

    This paragraph restates the requirements of paragraph (g) of AD 
2020-03-24, with no changes. Within 90 days after April 2, 2020 (the 
effective date of AD 2020-03-24), revise the existing maintenance or 
inspection program, as applicable, to incorporate the information 
specified in Chapter 5-40-01, Airworthiness Limitations, of the 
Dassault Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, 
dated January 1, 2019. The initial compliance time for doing the 
tasks is at the applicable time specified in Chapter 5-40-01, 
Airworthiness Limitations, of the Dassault Falcon 20 Retrofit 731 
Maintenance Manual, Revision 10, dated January 1, 2019; or within 90 
days after April 2, 2020; whichever occurs later. Accomplishing the 
revision of the existing maintenance or inspection program required 
by paragraph (i) of this AD terminates the requirements of this 
paragraph.

(h) Retained No Alternative Actions or Intervals, With a New Exception

    This paragraph restates the requirements of paragraph (h) of AD 
2020-03-24, with a new exception. Except as required by paragraph 
(i) 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 the actions or intervals are approved as an alternative 
method of compliance (AMOC) in accordance with the procedures 
specified in paragraph (m)(1) of this AD.

(i) New Revision of the Existing Maintenance or Inspection Program

    Except as specified in paragraph (j) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, European Union Aviation Safety Agency (EASA) AD 
2023-0062, dated March 20, 2023 (EASA AD 2023-0062). Accomplishing 
the revision of the existing maintenance or inspection program 
required by this paragraph terminates the requirements of paragraph 
(g) of this AD.

(j) Exceptions to EASA AD 2023-0062

    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2023-0062.
    (2) Paragraph (3) of EASA AD 2023-0062 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 2023-0062 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2023-0062 or within 90 days 
after the effective date of this AD, whichever occurs later.

[[Page 68456]]

    (4) This AD does not adopt the provisions specified in 
paragraphs (4) and (5) of EASA AD 2023-0062.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0062.

(k) New Provisions for Alternative Actions and Intervals

    After the existing maintenance or inspection program has been 
revised as required by paragraph (i) 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 2023-0062.

(l) Terminating Action for AD 2010-26-05

    Accomplishing the actions required by paragraph (g) or (i) of 
this AD terminates the requirements of paragraph (g)(1) of AD 2010-
26-05, for Model MYSTERE-FALCON 20-C5, 20-D5, 20-E5, and 20-F5 
airplanes on which the SSIP has been embodied into the airplane's 
existing maintenance or inspection program only.

(m) 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 (n) 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.

(n) Additional Information

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

(o) 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.
    (3) The following service information was approved for IBR on 
November 8, 2023.
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0062, 
dated March 20, 2023.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
April 2, 2020 (85 FR 11289, February 27, 2020).
    (i) Chapter 5-40-01, Airworthiness Limitations, of the Dassault 
Falcon 20 Retrofit 731 Maintenance Manual, Revision 10, dated 
January 1, 2019.
    (ii) [Reserved]
    (5) For EASA AD 2023-0062, 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 EASA 
AD on the EASA website: ad.easa.europa.eu.
    (6) For Dassault Aviation service information identified in this 
AD, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. 
Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; 
website dassaultfalcon.com.
    (7) 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.
    (8) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on September 28, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-22068 Filed 10-3-23; 8:45 am]
BILLING CODE 4910-13-P

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