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2024-14-02 DASSAULT AVIATION: Amendment 39-22783; Docket No. FAA-2024-1008; Project Identifier MCAI-2024-00080-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective September 25, 2024.

(b) AFFECTED ADS

    This  AD  replaces  AD 2023-02-13,  Amendment  39-22320  (88 FR  8740,
    February 10, 2023) (AD 2023-02-13).

(c) APPLICABILITY

    This AD  applies to  Dassault Aviation  Model FALCON  900EX airplanes,
    certificated in any category, as identified in European Union Aviation
    Safety Agency  (EASA) AD  2024-0035, dated  January 31,  2024 (EASA AD
    2024-0035).

(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 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 A NEW TERMINATING ACTION

    This paragraph  restates the requirements of paragraph (j) of AD 2023-
    02-13, 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 2022-0144,  dated July
    11,  2022  (EASA  AD 2022-0144).  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 2022-0144, WITH NO CHANGES

    This paragraph  restates the exceptions  specified in paragraph (k) of
    AD 2023-02-13, with no changes.

(1) The requirements  specified in paragraphs (1) and (2) of EASA AD 2022-
    0144 do not apply to this AD.

(2) Paragraph (3) of EASA AD 2022-0144  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 March 17, 2023 (the effective date of
    AD 2023-02-13).

(3) The initial compliance time for doing the tasks specified in paragraph
    (3) of EASA AD 2022-0144 is at the applicable "associated  thresholds"
    specified in  paragraph (3)  of EASA  AD 2022-0144,  or within 90 days
    after March 17, 2023 (the effective date of AD 2023-02-13),  whichever
    occurs later.

(4) The provisions  specified  in  paragraphs (4) and (5) of EASA AD 2022-
    0144 do not apply to this AD.

(5) The "Remarks" section of EASA AD 2020-0144 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 (l) of AD 2023-
    02-13, 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) and  intervals are  allowed unless  they are  approved as
    specified in the provisions of the "Ref. Publications" section of EASA
    AD 2022-0144.

(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  2024-0035. 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 2024-0035

(1) This AD does not adopt the requirements  specified  in  paragraphs (1)
    and (2) of EASA AD 2024-0035.

(2) Paragraph (3) of EASA AD 2024-0035  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  2024-0035  is at  the  applicable "limitations"  and
    "associated  thresholds"  as  incorporated  by  the  requirements   of
    paragraph  (3) of  EASA AD  2024-0035,  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 2024-0035.

(5) This AD does not adopt the "Remarks" section of EASA AD 2024-0035.

(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 2024-0035.

(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  manager  of  the International
    Validation Branch, mail it to the address 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,  1600 Stewart Avenue,  Suite 410,  Westbury, NY
    11590; telephone 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 material  listed  in  this paragraph  under 5
    U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this material as applicable to do the actions required by
    this AD, unless this AD specifies otherwise.

(3) The following material was approved for IBR on September 25, 2024.

(i) European Union Aviation Safety Agency (EASA) AD 2024-0035, dated Janu-
    ary 31, 2024.

(ii) [Reserved]

(4) The following material was approved  for IBR on March 17, 2023  (88 FR
    8740, February 10, 2023).

(i) European Union Aviation Safety Agency (EASA) AD 2022-0144,  dated July
    11, 2022.

(ii) [Reserved]

(5) For EASA AD 2024-0035  and EASA AD 2022-0144,  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 ad.easa.europa.eu.

(6) You may view this material 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.

(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 July 10, 2024. James D Foltz, Deputy Director, Compliance & Air-
worthiness Division, Aircraft Certification Service.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-1008; Project Identifier MCAI-2024-00080-T;
Amendment 39-22783; AD 2024-14-02]
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) 2023-02-
13, which applied to certain Dassault Aviation Model FALCON 900EX
airplanes. AD 2023-02-13 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. Since the FAA issued AD 2023-02-
13, the FAA has determined that new or more restrictive airworthiness
limitations are necessary. This AD continues to require certain actions
in AD 2023-02-13 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 September 25, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September
25, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of March
17, 2023 (88 FR 8740, February 10, 2023).

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-1008; 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, 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 ad.easa.europa.eu. It is also available at
regulations.gov under Docket No. FAA-2024-1008.
You may view this material 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.

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 2023-02-13, Amendment 39-22320 (88 FR 8740,
February 10, 2023) (AD 2023-02-13). AD 2023-02-13 applied to certain
Dassault Aviation Model FALCON 900EX airplanes. AD 2023-02-13 required
revising the existing maintenance or inspection program, as applicable,
to incorporate new or more restrictive airworthiness limitations. The
FAA issued AD 2023-02-13 to address reduced structural integrity of the
airplane.
The NPRM published in the Federal Register on April 23, 2024 (89 FR
30289). The NPRM was prompted by AD 2024-0035, dated January 31, 2024,
issued by EASA, which is the Technical Agent for the Member States of
the European Union (EASA AD 2024-0035) (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 certain
actions in AD 2023-02-13 and to require revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations, as specified in EASA AD
2024-0035. 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-2024-1008.

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 Material Under 1 CFR part 51

EASA AD 2024-0035 specifies new or more restrictive airworthiness
limitations for airplane structures and safe life limits.
This AD also requires EASA AD 2022-0144, dated July 11, 2022, which
the Director of the Federal Register approved for incorporation by
reference as of March 17, 2023 (88 FR 8740, February 10, 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 88 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 2023-02-13 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 2023-02-13, Amendment 39-22320 (88
FR 8740, February 10, 2023); and
b. Adding the following new airworthiness directive: