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2023-22-05 DASSAULT AVIATION: Amendment 39-22589; Docket No. FAA-2023-1651; Project Identifier MCAI-2023-00481-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective December 26, 2023.

(b) AFFECTED ADS

    This AD replaces AD 2020-23-10,  Amendment 39-21326  (85 FR 73404, No-
    vember 18, 2020) (AD 2020-23-10).

(c) APPLICABILITY

    This AD applies to Dassault Aviation airplanes specified in paragraphs
    (c)(1) and (2) of this AD, certificated in any category, as identified
    in European Union Aviation Safety Agency  (EASA)  AD 2023-0060,  dated
    March 16, 2023 (EASA AD 2023-0060).

(1) Model FAN JET FALCON airplanes.

(2) Model FAN JET FALCON SERIES C, D, E, F, and G airplanes.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 05,  Time Limits/Main-
    tenance 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, among other things, fatigue cracking and damage in  principle
    structural elements; such fatigue cracking and damage could result  in
    reduced structural integrity of the airplane.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) RETAINED REVISION OF THE EXISTING MAINTENANCE  OR  INSPECTION PROGRAM,
    WITH A NEW TERMINATING ACTION

    This paragraph restates the requirements of paragraph (i)  of AD 2020-
    23-10, with a new terminating action. Except as specified in paragraph
    (h) of this AD: Comply with all required actions and compliance  times
    specified in, and  in accordance with,  EASA AD 2019-0141,  dated June
    17,  2019  (EASA  AD 2019-0141).  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 2019-0141, WITH NO CHANGES

    This paragraph restates  the exceptions  specified in paragraph (j) of
    AD 2020-23-10, with no changes.

(1) The requirements specified in paragraphs (1), (2), (4) and (5) of EASA
    AD 2019-0141 do not apply to this AD.

(2) Paragraph (3) of EASA AD 2019-0141  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 AD  2019
    -0141 within 90 days after December 23, 2020 (the effective date of AD
    2020-23-10).

(3) The initial compliance time for doing the tasks specified in paragraph
    (3) of EASA AD 2019-0141 is at the applicable  "associated thresholds"
    specified in paragraph (3) of EASA AD 2019-0141, or within 90 days af-
    ter December 23, 2020 (the effective date of AD 2020-23-10), whichever
    occurs later.

(4) The "Remarks" section of EASA AD 2019-0141 does not apply to this AD.

(i) RETAINED RESTRICTIONS ON ALTERNATIVE ACTIONS AND INTERVALS, WITH A NEW
    EXCEPTION

    This paragraph restates the requirements of paragraph (k)  of AD 2020-
    23-10, 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  except as  specified  in the
    provisions of the "Ref. Publications" section of EASA AD 2019-0141.

(j) NEW REVISION OF THE EXISTING MAINTENANCE OR INSPECTION PROGRAM

    Except as specified in paragraph (k)  of this AD:  Comply with all re-
    quired actions and  compliance times specified  in, and in  accordance
    with, EASA AD  2023-0060. 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 2023-0060

(1) This AD does not adopt the requirements  specified  in  paragraphs (1)
    and (2) of EASA AD 2023-0060.

(2) Paragraph (3) of EASA AD 2023-0060  specifies  revising  "the approved
    AMP" within 12 months  after its effective date,  but this AD requires
    revising the existing maintenance or  inspection program,  as applica-
    ble, 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 2023-0060 is at the applicable "limitations" and "asso-
    ciated thresholds" as incorporated  by  the  requirements of paragraph
    (3) of EASA AD 2023-0060,  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 2023-0060.

(5) This AD does not adopt the "Remarks" section of EASA AD 2023-0060.

(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 2023-0060.

(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: 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 DOA-authorized signature.

(n) ADDITIONAL INFORMATION

    For more information about this AD,  contact  Tom Rodriguez,  Aviation
    Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; tel-
    ephone: 206-231-3226; email: tom.rodriguez@faa.gov.

(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 December 26,
    2023.

(i) European Union Aviation Safety Agency (EASA) AD 2023-0060, dated March
    16, 2023.

(ii) [Reserved]

(4) The following service information was approved for IBR on December 23,
    2020 (85 FR 73404, November 18, 2020).

(i) European Union Aviation Safety Agency (EASA) AD 2019-0141,  dated June
    17, 2019.

(ii) [Reserved]

(5) For EASA ADs 2023-0060 and 2019-0141,  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 service information at the FAA,  Airworthiness Prod-
    ucts 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 Admin-
    istration (NARA). For information on the availability of this material
    at NARA,  visit www.archives.gov/federal-register/cfr/ibr-locations or
    email fr.inspection@nara.gov.

Issued on October 27, 2023. Caitlin Locke, Director, Compliance & Airworth
-iness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Tom Rodriguez, Aviation Safety Engineer,
FAA, 2200 South 216th St., Des Moines, WA 98198;  telephone: 206-231-3226;
email: tom.rodriguez@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39


[Docket No. FAA-2023-1651; Project Identifier MCAI-2023-00481-T;
Amendment 39-22589; AD 2023-22-05]
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) 2020-23-
10, which applied to certain Dassault Aviation Model FAN JET FALCON and
FAN JET FALCON SERIES C, D, E, F, and G airplanes. AD 2020-23-10
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 2020-23-10 and requires revising the
existing maintenance or inspection program, as applicable, to
incorporate additional 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 December 26, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 26,
2023.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of
December 23, 2020 (85 FR 73404, November 18, 2020).

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1651; 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-2023-1651.

FOR FURTHER INFORMATION CONTACT
: Tom Rodriguez, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; 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 2020-23-10, Amendment 39-21326 (85 FR
73404, November 18, 2020) (AD 2020-23-10). AD 2020-23-10 applied to
certain Dassault Aviation Model FAN JET FALCON and FAN JET FALCON
SERIES C, D, E, F, and G airplanes. AD 2020-23-10 required revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations. The FAA
issued AD 2020-23-10 to address, among other things, fatigue cracking
and damage in principle structural elements; such fatigue cracking and
damage could result in reduced structural integrity of the airplane.
The NPRM published in the Federal Register on August 14, 2023 (88
FR 54935). The NPRM was prompted by AD 2023-0060, dated March 16, 2023,
issued by EASA, which is the Technical Agent for the Member States of
the European Union (EASA AD 2023-0060) (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 2020-23-10 and to require revising the existing maintenance or
inspection program, as applicable, to incorporate additional new or
more restrictive airworthiness limitations, as specified in EASA AD
2023-0060. The FAA is issuing this AD to address the unsafe condition
on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1651.

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 2023-0060 specifies new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires EASA AD 2019-0141, dated June 17, 2019, which
the Director of the Federal Register approved for incorporation by
reference as of December 23, 2020 (85 FR 73404, November 18, 2020).
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 168 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 2020-23-10 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

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) 2020-23-10, Amendment 39-21326
(85 FR 73404, November 18, 2020); and

b. Adding the following new AD: