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2023-22-10 DASSAULT AVIATION: Amendment 39-22594; Docket No. FAA-2023-1705; Project Identifier MCAI-2023-00480-T.
(a) EFFECTIVE DATE

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

(b) AFFECTED ADS

(1) This AD replaces AD 2020-02-13, Amendment 39-19827 (85 FR 6744, Febru-
    ary 6, 2020) (AD 2020-02-13).

(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 Dassault Aviation Model FAN JET FALCON,  FAN JET
    FALCON SERIES C, D, E, F,  and G airplanes,  certificated in any cate-
    gory, as identified in European Union Aviation Safety Agency (EASA) AD
    2023-0059, dated March 16, 2023 (EASA AD 2023-0059).

(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  principal
    structural elements.  The unsafe  condition,  if not addressed,  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-
    02-13,  with no  changes. Within  90 days  after March  12, 2020  (the
    effective date of AD  2020-02-13), revise the existing  maintenance or
    inspection  program,  as applicable,  to  incorporate the  information
    specified in Chapter 5-40-01, Airworthiness Limitations,  Revision 10,
    effective  January  1,  2019,  of  the  Dassault  Aviation  Falcon  20
    Maintenance Manual. The initial compliance time for doing the tasks is
    at the time specified  in Chapter 5-40-01, Airworthiness  Limitations,
    Revision  10,  effective January  1,  2019, of  the  Dassault Aviation
    Falcon 20 Maintenance Manual, or  within 90 days after March  12, 2020
    (the effective date of  AD 2020-02-13), whichever occurs  later. Where
    the  threshold  column  in   the  table  in  paragraph   B,  Mandatory
    Maintenance Operations, of Chapter 5-40-01, Airworthiness Limitations,
    Revision  10,  effective January 1, 2019,  of  the  Dassault  Aviation
    Falcon 20  Maintenance Manual  specifies a  compliance time  in years,
    those compliance times start from the date of issuance of the original
    airworthiness certificate or date  of issuance of the  original export
    certificate of airworthiness.

(h) RETAINED RESTRICTIONS  ON ALTERNATIVE ACTIONS  AND  INTERVALS  WITH NO
    CHANGE

    This paragraph restates the requirements of paragraph (j)  of AD 2020-
    02-13, with no  changes. 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 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, EASA AD  2023-0059. Accomplishing the  revision of the  existing
    maintenance  or   inspection  program   required  by   this  paragraph
    terminates the requirements of paragraph (g) of this AD.

(j) EXCEPTIONS TO EASA AD 2023-0059

(1) This  AD  does not adopt the requirements  specified in paragraphs (1)
    and (2) of EASA AD 2023-0059.

(2) Paragraph (3) of EASA AD 2023-0059  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  2023-0059  is at  the  applicable "limitations"  and
    "associated  thresholds"  as  incorporated  by  the  requirements   of
    paragraph  (3) of  EASA AD  2023-0059,  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 2023-0059.

(5) This AD does not adopt the "Remarks" section of EASA AD 2023-0059.

(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 2023-0059.

(l) TERMINATING ACTIONS FOR CERTAIN ACTIONS IN 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 FAN JET FALCON, FAN JET FALCON SERIES C, D, E,
    F and G airplanes on which the supplemental structural inspection pro-
    gram (SSIP) has been incorporated into the airplane's maintenance pro-
    gram 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
    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,  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 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 2023-0059, dated March
    16, 2023.

(ii) [Reserved]

(4) The following service information was approved  for  IBR  on March 12,
    2020 (85 FR 6744, February 6, 2020).

(i) Chapter 5-40-01, Airworthiness Limitations Revision 10, effective Jan-
    uary 1, 2019, of the Dassault Aviation Falcon 20 Maintenance Manual.

(ii) [Reserved]

(5) For EASA AD 2023-0059,  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 website
    at ad.easa.europa.eu.

(6) For Dassault  service  information  identified  in  this  AD,  contact
    Dassault Falcon Jet Corporation, Teterboro Airport, PO Box 2000, South
    Hackensack, NJ 07606;  telephone 201-440-6700; website dassaultfalcon.
    com.

(7) 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.

(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-locations or
    email fr.inspection@nara.gov.

Issued on November 13, 2023.  Ross Landes,  Deputy Director for Regulatory
Operations,  Compliance & Airworthiness 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-2023-1705; Project Identifier MCAI-2023-00480-T;
Amendment 39-22594; AD 2023-22-10]
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) 2020-02-
13, which applied to certain Dassault Aviation Model FAN JET FALCON,
FAN JET FALCON SERIES C, D, E, F, and G airplanes. AD 2020-02-13
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 certain actions in AD 2020-02-13 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 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 March
12, 2020 (85 FR 6744, February 6, 2020).

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1705; 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 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 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 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-2023-1705.

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 2020-02-13, Amendment 39-19827 (85 FR 6744,
February 6, 2020) (AD 2020-02-13). AD 2020-02-13 applied to certain
Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D, E,
F, and G. AD 2020-02-13 required revising the existing maintenance or
inspection program, as applicable, to incorporate new maintenance
requirements and airworthiness limitations. The FAA issued AD 2020-02-
13 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.
The NPRM published in the Federal Register on August 11, 2023 (88
FR 54500). The NPRM was prompted by AD 2023-0059, dated March 16, 2023
(EASA AD 2023-0059) (also referred to as the MCAI), issued by EASA,
which is the Technical Agent for the Member States of the European
Union. 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 2020-02-13 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
2023-0059. 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-2023-1705.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of
the cost to the public.

Additional Changes Made to This AD

The FAA has added paragraph (l) of this AD to clarify that this AD
terminates the requirements of paragraph (g)(1) of AD 2010-26-05,
Amendment 39-16544 (75 FR 79952, December 21, 2010) (AD 2010-26-05),
for Dassault Aviation Model FAN JET FALCON, FAN JET FALCON SERIES C, D,
E, F, and G airplanes on which the supplemental structural inspection
program (SSIP) has been incorporated into the airplane's maintenance
program only. The FAA has also redesignated subsequent paragraphs
accordingly. The FAA also added paragraph (b)(2) of this AD to specify
that AD 2010-26-05 is affected by this AD. AD 2020-02-13 included this
terminating action, but the FAA inadvertently omitted it from the
proposed AD.

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, and any other changes described
previously, 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 2023-0059. This service information
specifies new or more restrictive airworthiness limitations for
airplane structures and safe life limits.
This AD also requires Chapter 5-40-01, Airworthiness Limitations,
Revision 10, effective January 1, 2019, of the Dassault Aviation Falcon
20 Maintenance Manual, which the Director of the Federal Register
approved for incorporation by reference as of March 12, 2020 (85 FR
6744, February 6, 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 61 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 2020-02-13 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 (AD) 2020-02-13, Amendment 39-19827
(85 FR 6744, February 6, 2020); and

b. Adding the following new AD: