Airworthiness Directives; Dassault Aviation Airplanes, 3342-3344 [R1-2023-28853]

Download as PDF 3342 Federal Register / Vol. 89, No. 12 / Thursday, January 18, 2024 / Rules and Regulations (i) Bombardier Service Bulletin 604–35– 008, Revision 02, dated January 13, 2023. (ii) [Reserved] (3) For service information identified in this AD, contact Bombardier, Inc., Business Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que´bec H4S 1Y9, Canada; telephone 514–855–2999; email: ac.yul@aero.bombardier.com; website: bombardier.com. (4) 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. (5) 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 December 14, 2023. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. R1–2023–28849 Filed 1–17–24; 8:45 am] BILLING CODE 0099–10–D DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2023–1502; Project Identifier MCAI–2023–00380–T; Amendment 39–22634; AD 2023–25–07] RIN 2120–AA64 Airworthiness Directives; Dassault Aviation Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: Editorial Note: Rule document 2023–28853 originally published on pages 244–246 in the issue of Wednesday, January 3, 2024. In that publication, on page 244, in the second column, in the DATES section, on the first, second, and sixth lines, on page 245, in the third column, in paragraph ‘‘(a) Effective Date,’’ on the second line, and on page 246, in the second column, in paragraph ‘‘(p) Material Incorporated by Reference,’’ in sub paragraph ‘‘(3),’’ ‘‘February 7, 2023’’ should read ‘‘February 7, 2024’’. The rule is republished here corrected and in its entirety. The FAA is superseding Airworthiness Directive (AD) 2023–04– 10, which applied to all Dassault Aviation Model MYSTERE–FALCON 900 airplanes. AD 2023–04–10 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 khammond on DSKJM1Z7X2PROD with RULES SUMMARY: VerDate Sep<11>2014 16:09 Jan 17, 2024 Jkt 262001 or more restrictive airworthiness limitations are necessary. This AD continues to require the actions in AD 2023–04–10, 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 February 7, 2024. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of February 7, 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 20743, April 7, 2023). ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–1502; 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– 2023–1502. 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: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2023–04–10, PO 00000 Frm 00044 Fmt 4700 Sfmt 4700 Amendment 39–22357 (88 FR 20743, April 7, 2023) (AD 2023–04–10). AD 2023–04–10 applied to all Dassault Aviation Model MYSTERE-FALCON 900 airplanes. AD 2023–04–10 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. The FAA issued AD 2023–04–10 to address reduced structural integrity of the airplane. AD 2023–04–10 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) (AD 2010–26–05) for Dassault Aviation Model MYSTEREFALCON 900 airplanes only. This AD therefore continues to allow that terminating action. The NPRM published in the Federal Register on July 21, 2023 (88 FR 47086); corrected August 14, 2023 (88 FR 54933). The NPRM was prompted by AD 2023–0046, dated March 2, 2023, issued by EASA, which is the Technical Agent for the Member States of the European Union (EASA AD 2023–0046) (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 2023–04–10 and to require revising the existing maintenance or inspection program, as specified in EASA AD 2023–0046. 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–2023–1502. 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 E:\FR\FM\18JAR1.SGM 18JAR1 Federal Register / Vol. 89, No. 12 / Thursday, January 18, 2024 / Rules and Regulations in the NPRM. None of the changes will increase the economic burden on any operator. Related Service Information Under 1 CFR Part 51 The FAA reviewed EASA AD 2023– 0046. This service information specifies new or more restrictive airworthiness limitations for airplane structures and safe life limits. This AD also requires EASA AD 2022–0137, dated July 6, 2022, which the Director of the Federal Register approved for incorporation by reference as of May 12, 2023 (88 FR 20743, 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. khammond on DSKJM1Z7X2PROD with RULES Costs of Compliance The FAA estimates that this AD affects 151 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 2023–04–10 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 VerDate Sep<11>2014 16:09 Jan 17, 2024 Jkt 262001 3343 that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. (d) Subject Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks. 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. (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. 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) 2023–04–10, Amendment 39– 22357 (88 FR 20743, April 7, 2023); and ■ b. Adding the following new AD: ■ ■ 2023–25–07 Dassault Aviation: Amendment 39–22634; Docket No. FAA– 2023–1502; Project Identifier MCAI–2023– 00380–T. (a) Effective Date This airworthiness directive (AD) is effective February 16, 2024. (b) Affected ADs (1) This AD replaces AD 2023–04–10, Amendment 39–22357 (88 FR 20743, April 7, 2023) (AD 2023–04–10). (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 all Dassault Aviation Model MYSTERE–FALCON 900 airplanes, certificated in any category. PO 00000 Frm 00045 Fmt 4700 Sfmt 4700 (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 (j) of AD 2023–04–10, with no changes. 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 2022–0137, dated July 6, 2022 (EASA AD 2022- 0137). 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– 0137, With No Changes This paragraph restates the exceptions specified in paragraph (k) of AD 2023–04- 10, with no changes. (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2022–0137. (2) Paragraph (3) of EASA AD 2022–0137 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 2023–04–10). (3) The initial compliance time for doing the tasks specified in paragraph (3) of EASA AD 2022–0137 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2022–0137, or within 90 days after May 12, 2023 (the effective date of AD 2023–04–10), whichever occurs later. (4) This AD does not adopt the provisions specified in paragraphs (4) and (5) of EASA AD 2022–0137. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2022–0137 (i) Retained Restrictions on Alternative Actions or Intervals, With a New Exception This paragraph restates the requirements of paragraph (l) of AD 2023–04–10, 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) or intervals are allowed unless they are approved as specified in the provisions of the ‘‘Ref. Publications’’ section of EASA AD 2022–0137. E:\FR\FM\18JAR1.SGM 18JAR1 3344 Federal Register / Vol. 89, No. 12 / Thursday, January 18, 2024 / Rules and Regulations (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 2023–0046, dated March 2, 2023 (EASA AD 2023–0046). 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 2023–0046 (1) This AD does not adopt the requirements specified in paragraphs (1) and (2) of EASA AD 2023–0046. (2) Paragraph (3) of EASA AD 2023–0046 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 2023–0046 is at the applicable ‘‘limitations’’ and ‘‘associated thresholds’’ as incorporated by the requirements of paragraph (3) of EASA AD 2023–0046, 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 2023–0046. (5) This AD does not adopt the ‘‘Remarks’’ section of EASA AD 2023–0046. (l) New Provisions for Alternative Actions and Intervals After the existing 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 2023–0046. khammond on DSKJM1Z7X2PROD with RULES (m) Terminating Action for 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 MYSTERE–FALCON 900 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 VerDate Sep<11>2014 16:09 Jan 17, 2024 Jkt 262001 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. (3) The following service information was approved for IBR on February 7, 2024. (i) European Union Aviation Safety Agency (EASA) AD 2023–0046, dated March 2, 2023. (ii) [Reserved] (4) The following service information was approved for IBR on May 12, 2023 (88 FR 20743, April 7, 2023). (i) European Union Aviation Safety Agency (EASA) AD 2022–0137, dated July 6, 2022. (ii) [Reserved] (5) For EASA ADs 2023–0046 and 2022– 0137, 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 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. (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 December 14, 2023. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. R1–2023–28853 Filed 1–17–24; 8:45 am] BILLING CODE 0099–10–D CONSUMER PRODUCT SAFETY COMMISSION 16 CFR Parts 1112 and 1250 [Docket No. CPSC–2017–0010] Safety Standard Mandating ASTM F963 for Toys Consumer Product Safety Commission. AGENCY: PO 00000 Frm 00046 Fmt 4700 Sfmt 4700 ACTION: Direct final rule. Section 106 of the Consumer Product Safety Improvement Act (CPSIA) made ASTM F963–07e1, Standard Consumer Safety Specification for Toy Safety, a mandatory consumer product safety standard. Section 106 also provides procedures for revisions to the ASTM F963 standard. In accordance with those procedures, the Consumer Product Safety Commission (CPSC or Commission) has allowed the revised standard, ASTM F963–23, to become the mandatory toy standard. This direct final rule incorporates by reference ASTM F963–23 and updates the existing notice of requirements (NOR) that provide the criteria and processes for Commission acceptance of accreditation of third-party conformity assessment bodies for testing to ASTM F963. DATES: The rule is effective on April 20, 2024, unless CPSC receives a significant adverse comment by February 20, 2024. If CPSC receives such a significant adverse comment, it will publish a document in the Federal Register withdrawing this direct final rule before its effective date. The incorporation by reference of the publication listed in this rule is approved by the Director of the Federal Register as of April 20, 2024. ADDRESSES: You can submit comments, identified by Docket No. CPSC–2017– 0010, by any of the following methods: Electronic Submissions: Submit electronic comments to the Federal eRulemaking Portal at: www.regulations.gov. Follow the instructions for submitting comments. Do not submit through this website: confidential business information, trade secret information, or other sensitive or protected information that you do not want to be available to the public. CPSC typically does not accept comments submitted by email except as described below. Mail/Hand Delivery/Courier/ Confidential Written Submissions: CPSC encourages you to submit electronic comments by using the Federal eRulemaking Portal. You may, however, submit comments by mail, hand delivery, or courier to: Office of the Secretary, Consumer Product Safety Commission, 4330 East West Highway, Bethesda, MD 20814; telephone: (301) 504–7479. Instructions: All submissions must include the agency name and docket number. CPSC may post all comments without change, including any personal identifiers, contact information, or other personal information provided, to: www.regulations.gov. If you wish to SUMMARY: E:\FR\FM\18JAR1.SGM 18JAR1

Agencies

[Federal Register Volume 89, Number 12 (Thursday, January 18, 2024)]
[Rules and Regulations]
[Pages 3342-3344]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: R1-2023-28853]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1502; Project Identifier MCAI-2023-00380-T; 
Amendment 39-22634; AD 2023-25-07]
RIN 2120-AA64


Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

    Editorial Note: Rule document 2023-28853 originally published on 
pages 244-246 in the issue of Wednesday, January 3, 2024. In that 
publication, on page 244, in the second column, in the DATES 
section, on the first, second, and sixth lines, on page 245, in the 
third column, in paragraph ``(a) Effective Date,'' on the second 
line, and on page 246, in the second column, in paragraph ``(p) 
Material Incorporated by Reference,'' in sub paragraph ``(3),'' 
``February 7, 2023'' should read ``February 7, 2024''. The rule is 
republished here corrected and in its entirety.

SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-04-
10, which applied to all Dassault Aviation Model MYSTERE-FALCON 900 
airplanes. AD 2023-04-10 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-
10, 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 February 7, 2024.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of February 7, 
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 20743, April 7, 2023).

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2023-1502; 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 [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-2023-1502.

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 2023-04-10, Amendment 39-22357 (88 FR 
20743, April 7, 2023) (AD 2023-04-10). AD 2023-04-10 applied to all 
Dassault Aviation Model MYSTERE-FALCON 900 airplanes. AD 2023-04-10 
required revising the existing maintenance or inspection program, as 
applicable, to incorporate new or more restrictive airworthiness 
limitations. The FAA issued AD 2023-04-10 to address reduced structural 
integrity of the airplane. AD 2023-04-10 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) (AD 2010-26-05) for Dassault Aviation Model MYSTERE-
FALCON 900 airplanes only. This AD therefore continues to allow that 
terminating action.
    The NPRM published in the Federal Register on July 21, 2023 (88 FR 
47086); corrected August 14, 2023 (88 FR 54933). The NPRM was prompted 
by AD 2023-0046, dated March 2, 2023, issued by EASA, which is the 
Technical Agent for the Member States of the European Union (EASA AD 
2023-0046) (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 2023-04-10 and to require revising the existing maintenance or 
inspection program, as specified in EASA AD 2023-0046. 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-2023-1502.

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

[[Page 3343]]

in the NPRM. None of the changes will increase the economic burden on 
any operator.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed EASA AD 2023-0046. This service information 
specifies new or more restrictive airworthiness limitations for 
airplane structures and safe life limits.
    This AD also requires EASA AD 2022-0137, dated July 6, 2022, which 
the Director of the Federal Register approved for incorporation by 
reference as of May 12, 2023 (88 FR 20743, 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 151 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 2023-04-10 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) 2023-04-10, Amendment 39-22357 
(88 FR 20743, April 7, 2023); and
0
b. Adding the following new AD:

2023-25-07 Dassault Aviation: Amendment 39-22634; Docket No. FAA-
2023-1502; Project Identifier MCAI-2023-00380-T.

(a) Effective Date

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

(b) Affected ADs

    (1) This AD replaces AD 2023-04-10, Amendment 39-22357 (88 FR 
20743, April 7, 2023) (AD 2023-04-10).
    (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 all Dassault Aviation Model MYSTERE-FALCON 
900 airplanes, certificated in any category.

(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 Revision of the Existing Maintenance or Inspection 
Program, With No Changes

    This paragraph restates the requirements of paragraph (j) of AD 
2023-04-10, with no changes. 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 2022-0137, dated July 6, 2022 (EASA AD 2022- 0137). 
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 2022-0137, With No Changes

    This paragraph restates the exceptions specified in paragraph 
(k) of AD 2023-04- 10, with no changes.
    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2022-0137.
    (2) Paragraph (3) of EASA AD 2022-0137 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 2023-04-10).
    (3) The initial compliance time for doing the tasks specified in 
paragraph (3) of EASA AD 2022-0137 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2022-0137, or within 90 
days after May 12, 2023 (the effective date of AD 2023-04-10), 
whichever occurs later.
    (4) This AD does not adopt the provisions specified in 
paragraphs (4) and (5) of EASA AD 2022-0137.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2022-0137

(i) Retained Restrictions on Alternative Actions or Intervals, With a 
New Exception

    This paragraph restates the requirements of paragraph (l) of AD 
2023-04-10, 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) or intervals are allowed unless they are 
approved as specified in the provisions of the ``Ref. Publications'' 
section of EASA AD 2022-0137.

[[Page 3344]]

(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 2023-0046, dated March 2, 2023 (EASA AD 
2023-0046). 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 2023-0046

    (1) This AD does not adopt the requirements specified in 
paragraphs (1) and (2) of EASA AD 2023-0046.
    (2) Paragraph (3) of EASA AD 2023-0046 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 2023-0046 is at the applicable 
``limitations'' and ``associated thresholds'' as incorporated by the 
requirements of paragraph (3) of EASA AD 2023-0046, 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 2023-0046.
    (5) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0046.

(l) New Provisions for Alternative Actions and Intervals

    After the existing 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 2023-0046.

(m) Terminating Action for 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 MYSTERE-FALCON 900 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.
    (3) The following service information was approved for IBR on 
February 7, 2024.
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0046, 
dated March 2, 2023.
    (ii) [Reserved]
    (4) The following service information was approved for IBR on 
May 12, 2023 (88 FR 20743, April 7, 2023).
    (i) European Union Aviation Safety Agency (EASA) AD 2022-0137, 
dated July 6, 2022.
    (ii) [Reserved]
    (5) For EASA ADs 2023-0046 and 2022-0137, 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 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.
    (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 December 14, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. R1-2023-28853 Filed 1-17-24; 8:45 am]
BILLING CODE 0099-10-D

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