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2023-21-01 DASSAULT AVIATION: Amendment 39-22573; Docket No. FAA-2023-1494; Project Identifier MCAI-2023-00382-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective December 11, 2023.

(b) AFFECTED ADS

(1) This AD replaces AD 2020-01-13,  Amendment 39-19819 (85 FR 5313, Janu-
    ary 30, 2020) (AD 2020-01-13).

(2) This AD affects AD 2010-26-05, Amendment 39-16544 (75 FR 79952, Decem-
    ber 21, 2010) (AD 2010-26-05).

(c) APPLICABILITY

    This AD applies to all Dassault Aviation Model MYSTERE-FALCON 200 air-
    planes, certificated in any category.

(d) SUBJECT

    Air Transport Association (ATA) of America Code: 05, Time Limits/Main-
    tenance 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  fatigue   cracking,  damage,   and  corrosion   in  principal
    structural  elements;  such fatigue  cracking,  damage, and  corrosion
    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 NO CHANGES

    This paragraph restates the requirements of paragraph (i)  of AD 2020-
    01-13, with no changes. Within 90 days after March 5, 2020 (the effec-
    tive date of AD 2020-01-13),  revise the existing maintenance  or  in-
    spection program, as applicable, to incorporate the information speci-
    fied in Chapter 5-40-00, Airworthiness Limitations, Revision 18, dated
    January 15, 2019,  of the Dassault Falcon 200 Maintenance Manual.  The
    initial compliance time  for doing the tasks is at the applicable time
    specified in Chapter 5-40-00,  Airworthiness Limitations, Revision 18,
    dated January 15, 2019, of the Dassault Falcon 200 Maintenance Manual;
    or within 90 days after March 5, 2020;  whichever occurs later. Accom-
    plishing the revision of the existing maintenance  or  inspection pro-
    gram required by paragraph (i) of this AD terminates  the requirements
    of this paragraph.

(h) RETAINED RESTRICTIONS ON ALTERNATIVE ACTIONS OR INTERVALS,  WITH A NEW
    EXCEPTION

    This paragraph restates the requirements  of paragraph (j) of AD 2020-
    01-13, with a  new exception. Except  as required by  paragraph (i) of
    this AD, after the existing maintenance or inspection program has been
    revised  as  required by  paragraph  (g) of  this  AD, no  alternative
    actions  (e.g.,  inspections)  or intervals  may  be  used unless  the
    actions  or  intervals  are  approved  as  an  alternative  method  of
    compliance  (AMOC)  in  accordance with  the  procedures  specified in
    paragraph (m)(1) of this AD.

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

    Except as specified in paragraph (j)  of this AD:  Comply with all re-
    quired actions  and  compliance times specified in,  and in accordance
    with, European Union Aviation Safety Agency (EASA) AD 2023-0045, dated
    March 2, 2023;  corrected  March 3, 2023  (EASA AD 2023-0045).  Accom-
    plishing the revision of the existing maintenance  or  inspection pro-
    gram required by this paragraph terminates  the requirements  of para-
    graph (g) of this AD.

(j) EXCEPTIONS TO EASA AD 2023-0045

(1) This AD does not adopt the requirements  specified  in  paragraphs (1)
    and (2) of EASA AD 2023-0045.

(2) Paragraph (3) of EASA AD 2023-0045  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 2023-0045 is at the applicable "limitations"  as incor-
    porated by the requirements of paragraph (3) of EASA AD 2023-0045,  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 2023-0045.

(5) This AD does not adopt the "Remarks" section of EASA AD 2023-0045.

(k) NEW PROVISIONS FOR ALTERNATIVE ACTIONS AND INTERVALS

    After the existing maintenance or inspection program has been  revised
    as required by paragraph (i) 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 2023-0045.

(l) TERMINATING ACTION FOR AD 2010-26-05

    Accomplishing the actions required by paragraph (g) or (i)  of this AD
    terminates the requirements of paragraph (g)(1) of AD 2010-26-05,  for
    Dassault Aviation Model MYSTERE-FALCON 200 airplanes only.

(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 in-
    spector  or  responsible Flight Standards Office,  as appropriate.  If
    sending information directly to the manager of the International Vali-
    dation 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 in-
    spector, or lacking a principal inspector,  the manager of the respon-
    sible 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; phone 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 11,
    2023.

(i) European Union Aviation Safety Agency (EASA) AD 2023-0045, dated March
    2, 2023; corrected March 3, 2023.

(ii) [Reserved].

(4) The following service information  was  approved  for  IBR on March 5,
    2020 (85 FR 5313, January 30, 2020).

(i) Chapter 5-40-00, Airworthiness Limitations, Revision 18, dated January
    15, 2019, of the Dassault Falcon 200 Maintenance Manual.

(ii) [Reserved]

(5) For EASA AD 2023-0045,  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 EASA AD on the EASA web
    site: ad.easa.europa.eu.

(6) For Dassault Aviation service information incorporated by reference in
    this AD,  contact Dassault Falcon Jet Corporation,  Teterboro Airport,
    P.O. Box 2000, South Hackensack, NJ 07606; telephone 201-440-6700; web
    site dassaultfalcon.com.

(7) You may view this service information at the FAA,  Airworthiness Prod-
    ucts 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.

(8) 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-locationsore
    mailfr.inspection@nara.gov.

Issued on October 30, 2023. Victor Wicklund, Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Tom Rodriguez, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue,  Suite 410,  Westbury, NY 11590;  phone 206-231-
3226; email: tom.rodriguez@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1494; Project Identifier MCAI-2023-00382-T;
Amendment 39-22573; AD 2023-21-01]
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) 2020-01-
13, which applied to all Dassault Aviation Model MYSTERE-FALCON 200
airplanes. AD 2020-01-13 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 2020-01-
13 and require 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 December 11, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 11,
2023.
The Director of the Federal Register approved the incorporation by
reference of a certain other publication listed in this AD as of March
5, 2020 (85 FR 5313, January 30, 2020).

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1494; 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 ADs 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.
For Dassault Aviation service information incorporated by
reference in this AD, contact Dassault Falcon Jet Corporation,
Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone
201-440-6700; website dassaultfalcon.com.
You may view this service information 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 at
regulations.gov under Docket No. FAA-2023-1494.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone 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 2020-01-13, Amendment 39-19819 (85 FR 5313,
January 30, 2020) (AD 2020-01-13). AD 2020-01-13 applied to all
Dassault Aviation Model MYSTERE-FALCON 200 airplanes. AD 2020-01-13
required revising the existing maintenance or inspection program, as
applicable, to incorporate new or more restrictive airworthiness
limitations. The FAA issued AD 2020-01-13 to address fatigue cracking,
damage, and corrosion in principal structural elements; such fatigue
cracking, damage, and corrosion could result in reduced structural
integrity of the airplane.
The NPRM published in the Federal Register on July 19, 2023 (88 FR
46112). The NPRM was prompted by EASA AD 2023-0045, dated March 2,
2023; corrected March 3, 2023, issued by EASA, which is the Technical
Agent for the Member States of the European Union (EASA AD 2023-0045)
(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 2020-01-13 and require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. 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-2023-1494.

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

The FAA reviewed EASA AD 2023-0045. This service information
specifies new or more restrictive airworthiness limitations for airplane
structures and safe life limits.
This AD also requires Chapter 5-40-00, Airworthiness Limitations,
Revision 18, dated January 15, 2019, of the Dassault Falcon 200
Maintenance Manual, which the Director of the Federal Register approved
for incorporation by reference as of March 5, 2020 (85 FR 5313, January
30, 2020).
This service information 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 9 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 2020-01-13 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 agency estimates the average 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

The FAA determined that 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) 2020-01-13, Amendment 39-19819
(85 FR 5313, January 30, 2020); and

b. Adding the following new AD: