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Federal Register / Vol. 86, No. 84 / Tuesday, May 4, 2021 / Rules and Regulations
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 work-hour.
Authority for This Rulemaking Title 49 of the United States Code specifies the FAAs 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 Agencys 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.

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Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:

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Authority: 49 U.S.C. 106g, 40113, 44701.
39.13

Amended
2. The FAA amends 39.13 by:
a. Removing airworthiness directive 20200716, Amendment 3919895 85
FR 20405, April 13, 2020; and b. Adding the following new airworthiness directive:

20210912 Dassault Aviation:
Amendment 3921526; Docket No.
FAA20201169; Project Identifier MCAI202001373T.
a Effective Date This airworthiness directive AD is effective June 8, 2021.
b Affected ADs 1 This AD replaces AD 20200716, Amendment 3919895 85 FR 20405, April 13, 2020 AD 20200716.
2 This AD affects AD 20141623, Amendment 3917947 79 FR 52545, September 4, 2014 AD 20141623.
c Applicability This AD applies to Dassault Aviation Model FALCON 7X airplanes, certificated in any category, with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 1, 2020.
Note 1 to paragraph c: Model FALCON
7X airplanes with modification M1000
incorporated are commonly referred to as Model FALCON 8X airplanes as a marketing designation.
d Subject Air Transport Association ATA of America Code 05, Time Limits/Maintenance Checks.
e Reason This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. The FAA is issuing this AD to address reduced structural integrity and reduced control of airplanes due to the failure of system components.
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 i of AD 20200716, with no changes. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 1, 2019, 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 20190257, dated October 17, 2019 EASA AD 20190257.
h Retained Exceptions to EASA AD 2019
0257, With No Changes This paragraph restates the requirements of paragraph j of AD 20200716 with no
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changes. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 1, 2019:
1 The requirements specified in paragraphs 1 and 2 of EASA AD 2019
0257 do not apply to this AD.
2 Where paragraph 3 of EASA AD 2019
0257 specifies a compliance time of Within 12 months after its effective date to revise the approved AMP Aircraft Maintenance Program, this AD requires revising the existing maintenance or inspection program, as applicable to incorporate the limitations, tasks and associated thresholds and intervals specified in paragraph 3 of EASA AD 20190257 within 90 days after May 18, 2020 the effective date of AD 2020
0716.
3 The initial compliance time for doing the tasks specified in paragraph 3 of EASA
AD 20190257 is at the applicable associated thresholds specified in paragraph 3 of EASA AD 20190257, or within 90 days after May 18, 2020 the effective date of AD 20200716, whichever occurs later.
4 The provisions specified in paragraphs 4 and 5 of EASA AD 20190257 do not apply to this AD.
5 The Remarks section of EASA AD
20190257 does not apply to this AD.
i Retained Provisions for Alternative Actions, Intervals, and Critical Design Configuration Control Limitations CDCCLs With a New Exception This paragraph restates the requirements of paragraph k of AD 20200716, with a new exception. For airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or before June 1, 2019, except as required by paragraph j of this AD, after the maintenance or inspection program has been revised as required by paragraph g of this AD, no alternative actions e.g., inspections, intervals, or CDCCLs are allowed unless they are approved as specified in the provisions of the Ref. Publications section of EASA
AD 20190257.
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 20200214, dated October 6, 2020 EASA AD 2020
0214. Accomplishing the maintenance or inspection program revision required by this paragraph terminates the requirements of paragraph g of this AD.
k Exceptions to EASA AD 20200214
1 The requirements specified in paragraphs 1 and 2 of EASA AD 2020
0214 do not apply to this AD.
2 Paragraph 3 of EASA AD 20200214
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, to incorporate the limitations, tasks and associated thresholds and intervals specified in paragraph 3 of EASA

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