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PROPOSED AD DASSAULT AVIATION: Docket No. FAA-2024-0457; Project Identifier MCAI-2023-01207-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    April 22, 2024.

(b) AFFECTED ADS

    This AD replaces AD 2022-02-10, Amendment 39-21907 (87 FR 7025, Febru-
    ary 8, 2022) (AD 2022-02-10).

(c) APPLICABILITY

    This AD applies to Dassault Aviation  airplanes  identified  in  para-
    graphs (c)(1) through (3) of this AD, certificated in any category, as
    identified  in European Union Aviation Safety Agency  (EASA)  AD 2023-
    0207, dated November 21, 2023 (EASA AD 2023-0207).

(1) Model FALCON 7X airplanes.

(2) Model FALCON 900EX airplanes.

(3) Model FALCON 2000EX airplanes.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 51, Standard Practices
    /Structures.

(e) UNSAFE CONDITION

    This AD was prompted by a report of an improper heat treatment process
    applied during the manufacturing of certain Decomatic titanium screws,
    and by the  determination that affected  parts in additional  areas on
    certain airplanes, as well as additional airplanes, are subject to the
    unsafe condition. The FAA is issuing this AD to address failure of  an
    affected screw installed in a critical location, possibly resulting in
    reduced structural integrity of the airplane.

(f) COMPLIANCE

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

(g) REQUIREMENTS

    Except as specified in paragraph (h)  of this AD:  Comply with all re-
    quired actions and compliance times specified in,  and  in  accordance
    with, EASA AD 2023-0207.

(h) EXCEPTIONS TO EASA AD 2023-0207

(1) Where EASA AD 2023-0207 refers to its effective date, this AD requires
    using the effective date of this AD.

(2) This AD does not adopt the "Remarks" section of EASA AD 2023-0207.

(3) Where  Ref Publications  specifies  "Dassault SB 7X-467 original issue
    dated 16 November 2020, Rev. 1 dated 12 December 2022  or Rev. 2 dated
    20 March 2023,"  this AD requires replacing those words with "Dassault
    Service Bulletin 7X-467, Revision 2, dated March 20, 2023."

(i) CREDIT FOR PREVIOUS ACTIONS

    For Model FALCON 7X airplanes:  This paragraph provides credit for the
    actions specified in paragraph (g) of this AD,  if  those actions were
    performed before the effective date of this AD  using Dassault Service
    Bulletin 7X-467, dated November 16, 2020, provided the additional work
    specified in Dassault Service Bulletin 7X-467, Revision 2, dated March
    20, 2023, is accomplished within the applicable compliance time speci-
    fied in EASA AD 2023-0207.

(j) 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 accord
    -ance with 14 CFR 39.19, send your request to your principal inspector
    or responsible Flight Standards Office, as appropriate. If sending in-
    formation  directly  to  the manager  of the  International Validation
    Branch, mail it to the address identified in paragraph (k) 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  accom-
    plished using a method approved by the Manager,  International Valida-
    tion Branch, FAA; or EASA;  or Dassault Aviation's EASA Design Organi-
    zation Approval (DOA).  If approved by the DOA,  the approval must in-
    clude the DOA-authorized signature.

(k) 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.

(l) 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.

(i) European Union Aviation Safety Agency (EASA) AD 2023-0207 dated Novem-
    ber 21, 2023.

(ii) Dassault Service Bulletin 7X-467, Revision 2, dated March 20, 2023.

(3) For EASA AD 2023-0207,  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.

(4) 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.

(5) 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 February 28, 2024.  Victor Wicklund, Deputy Director, Compliance
& Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this  proposed  AD  by  April 22,
2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-0457; Project Identifier MCAI-2023-01207-T]
RIN 2120-AA64

Airworthiness Directives; Dassault Aviation Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2022-02-10, which applies to certain Dassault Aviation Model FALCON 7X,
FALCON 900EX, and FALCON 2000EX airplanes. AD 2022-02-10 requires
replacement of certain titanium screws. Since the FAA issued AD 2022-
02-10, affected parts have been found in other areas of certain Falcon
7X airplanes as well as in additional Falcon 7X airplanes. This
proposed AD would continue to require the actions in AD 2022-02-10, add
other locations for screw replacement, and revise the applicability, as
specified in a European Union Aviation Safety Agency (EASA) AD, which
is proposed for incorporation by reference (IBR). The FAA is proposing
this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by April 22,
2024.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-0457; 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 NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For the EASA AD identified in this NPRM, 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. It is also
available at regulations.gov under Docket No. FAA-2024-0457.
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.

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:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2024-0457; Project Identifier
MCAI-2023-01207-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.

Confidential Business Information

CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Tom
Rodriguez, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone: 206-231-3226; email:
tom.rodriguez@faa.gov. Any commentary that the FAA receives which is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.

Background

The FAA issued AD 2022-02-10, Amendment 39-21907 (87 FR 7025,
February 8, 2022) (AD 2022-02-10), for certain Dassault Aviation Model
FALCON 7X, FALCON 900EX, and FALCON 2000EX airplanes. AD 2022-02-10 was
prompted by MCAI originated by EASA, which is the Technical Agent for
the Member States of the European Union. EASA issued AD 2021-0047,
dated February 16, 2021, to correct an unsafe condition.
AD 2022-02-10 requires replacement of certain titanium screws. The
FAA issued AD 2022-02-10 to address failure of an affected screw
installed in a critical location, possibly resulting in reduced
structural integrity of the airplane. See the MCAI for additional
background information.

Actions Since AD 2022-02-10 Was Issued

Since the FAA issued AD 2022-02-10, EASA superseded EASA AD 2021-
0047, dated February 16, 2021, and issued EASA AD 2023-0207, dated
November 21, 2023 (also referred to as the MCAI), to correct an unsafe
condition for certain Dassault Aviation Model FALCON 7X, FALCON 900EX,
and FALCON 2000EX airplanes. The MCAI states that since EASA issued AD
2021-0047, it was determined that affected parts have been installed in
production in additional areas of certain Model FALCON 7X airplanes
already included in the applicability of EASA AD 2021-0047.
Additionally, it was determined that additional Model FALCON 7X
airplanes were not included in the applicability of EASA AD 2021-0047.
The FAA is proposing 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-2024-0457.

Explanation of Retained Requirements

Although this proposed AD does not explicitly restate the
requirements of AD 2022-02-10, this proposed AD would retain all of the
requirements of AD 2022-02-10. Those requirements are referenced in
EASA AD 2023-0207, which, in turn, is referenced in paragraph (g) of
this proposed AD.

Related Service Information Under 1 CFR Part 51

EASA AD 2023-0207 specifies procedures for replacing titanium screws.
Dassault Service Bulletin 7X-467, Revision 2, dated March 20, 2023,
specifies procedures for additional work.
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.

FAA's Determination

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 is issuing this NPRM after determining that
the unsafe condition described previously is likely to exist or develop
in other products of the same type design.

Proposed AD Requirements in This NPRM

This proposed AD would retain certain requirements of AD 2022-02-
10. This proposed AD would require accomplishing the actions specified
in EASA AD 2023-0207 described previously, except for any differences
identified as exceptions in the regulatory text of this proposed AD.

Explanation of Required Compliance Information

In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate EASA AD 2023-0207 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2023-0207 in its entirety through that incorporation, except
for any differences identified as exceptions in the regulatory text of
this proposed AD. Using common terms that are the same as the heading
of a particular section in EASA AD 2023-0207 does not mean that
operators need comply only with that section. For example, where the AD
requirement refers to ``all required actions and compliance times,''
compliance with this AD requirement is not limited to the section
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2023-
0207. Service information required by EASA AD 2023-0207 for compliance
will be available at regulations.gov under Docket No. FAA-2024-0457
after the FAA final rule is published.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 44 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:

Estimated Costs for Required Actions

Action
Labor cost
Parts cost
Cost per product Cost on U.S. operators
Retained actions from AD 2022-02-10 Up to 90 work-hours x $85 per hour = $7,650
$0
Up to $7,650 Up to $336,600
New proposed requirements Up to 110 work-hours x $85 per hour = $9,350
0
Up to $9,350 Up to $411,400

According to the manufacturer, some or all of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected individuals. The FAA does not control warranty
coverage for affected individuals. As a result, the FAA has included
all known costs in the cost estimate.

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 proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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) 2022-02-10, Amendment 39-21907
(87 FR 7025, February 8, 2022); and

b. Adding the following new AD: