|  DEPARTMENT OF TRANSPORTATION
 Federal Aviation Administration
 
 14 CFR Part 39
 
 [Docket No. FAA-2020-1111; Product Identifier MCAI-2020-01374-T;
 Amendment 39-21442; AD 2021-04-20]
 RIN 2120-AA64
 
 Airworthiness Directives; Dassault Aviation Airplanes
 
 AGENCY: Federal Aviation Administration (FAA), Department of
 Transportation (DOT).
 
 ACTION: Final rule.
 
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 SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2018-24-
 03, which applied to all Dassault Aviation Model Falcon 10 airplanes.
 AD 2018-24-03 required revising the existing maintenance or inspection
 program, as applicable, to incorporate new or more restrictive
 maintenance requirements and airworthiness limitations. This AD
 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 April 9, 2021.
 The Director of the Federal Register approved the incorporation by
 reference of a certain publication listed in this AD as of April 9,
 2021.
 The Director of the Federal Register approved the incorporation by
 reference of a certain other publication listed in this AD as of
 January 4, 2019 (83 FR 61523, November 30, 2018).
 
 ADDRESSES: For EASA material incorporated by reference (IBR) in 
        this
 AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
 telephone +49 221 8999 000; email ADs@easa.europa.eu; internet
 www.easa.europa.eu. You may find this IBR material on the EASA website
 at https://ad.easa.europa.eu. For Dassault Aviation service information
 identified in this final rule, contact Dassault Falcon Jet Corporation,
 Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone
 201-440-6700; internet https://www.dassaultfalcon.com. You may view
 this IBR 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 on the internet at
 https://www.regulations.gov by searching for and locating Docket No.
 FAA-2020-1111.
 
 Examining the AD Docket
 
 You may examine the AD docket on the internet at https://www.regulations.
 gov by searching for and locating Docket No. FAA-2020-
 1111; 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, 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.
 
 FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
 Large Aircraft Section, International Validation Branch, FAA, 2200
 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226;
 email tom.rodriguez@faa.gov.
 
 SUPPLEMENTARY INFORMATION:
 
 Background
 
 The EASA, which is the Technical Agent for the Member States of the
 European Union, has issued EASA AD 2020-0215, dated October 6, 2020
 (EASA AD 2020-0215) (also referred to as the Mandatory Continuing
 Airworthiness Information, or the MCAI), to correct an unsafe condition
 for all Dassault Aviation Model Falcon 10 airplanes.
 The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
 CFR part 39 to supersede AD 2018-24-03, Amendment 39-19507 (83 FR
 61523, November 30, 2018) (AD 2018-24-03). AD 2018-24-03 applied to all
 Dassault Aviation Model Falcon 10 airplanes. The NPRM published in the
 Federal Register on December 7, 2020 (85 FR 78808). The NPRM was
 prompted by a determination that new or more restrictive airworthiness
 limitations are necessary. The NPRM 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 2020-0215.
 The FAA is issuing this AD to address among other things, fatigue
 cracking and damage in principal structural elements; such fatigue
 cracking and damage could result in reduced structural integrity of the
 airplane. See the MCAI for additional background information.
 
 Comments
 
 The FAA gave the public the opportunity to participate in
 developing this final rule. The FAA received no comments on the NPRM or
 on the determination of the cost to the public.
 
 Conclusion
 
 The FAA reviewed the relevant data and determined that air safety
 and the public interest require adopting this final rule as proposed,
 except for minor editorial changes. The FAA has determined that these
 minor changes:
 Are consistent with the intent that was proposed in the
 NPRM for addressing the unsafe condition; and
 Do not add any additional burden upon the public than was
 already proposed in the NPRM.
 
 Related Service Information Under 1 CFR part 51
 
 EASA AD 2020-0215 describes new or more restrictive airworthiness
 limitations for airplane structures and safe life limits.
 This AD also requires Section 5-40-00, Airworthiness Limitations,
 Revision 13, dated July 2017, of the Dassault Falcon 10 Maintenance
 Manual, which the Director of the Federal Register approved for
 incorporation by reference as of January 4, 2019 (83 FR 61523, November
 30, 2018).
 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 60 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 2018-24-03 to be $7,650 (90 work-hours x $85 per work-
 hour).
 The FAA has determined that revising the existing maintenance or
 inspection program takes an average of 90 work-hours per operator,
 although the agency recognizes that this number may vary from operator
 to operator. Since operators incorporate maintenance or inspection
 program changes for their affected fleet(s), the FAA has determined
 that a per-operator estimate is more accurate than a per-airplane
 estimate. The FAA estimates the total cost per operator for the new
 proposed actions to be $7,650 (90 work-hours x $85 per work-hour).
 
 Authority for This Rulemaking
 
 Title 49 of the United States Code specifies the FAA's authority to
 issue rules on aviation safety. Subtitle I, section 106, describes the
 authority of the FAA Administrator. Subtitle VII: Aviation Programs,
 describes in more detail the scope of the Agency's authority.
 The FAA is issuing this rulemaking under the authority described in
 Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
 Under that section, Congress charges the FAA with promoting safe flight
 of civil aircraft in air commerce by prescribing regulations for
 practices, methods, and procedures the Administrator finds necessary
 for safety in air commerce. This regulation is within the scope of that
 authority because it addresses an unsafe condition that is likely to
 exist or develop on products identified in this rulemaking action.
 
 Regulatory Findings
 
 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.
 
 Adoption of 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.
 
 Sec. 39.13 [Amended]
 
 2. The FAA amends Sec. 39.13 by:
 
 a. Removing Airworthiness Directive (AD) 2018-24-03, Amendment 39-19507
 (83 FR 61523, November 30, 2018); and
 
 b. Adding the following new AD:
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