Proposed Rule2023-14367

Airworthiness Directives; Dassault Aviation Airplanes

Primary source

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Published
July 10, 2023

Issuing agencies

Transportation DepartmentFederal Aviation Administration

Abstract

The FAA proposes to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model MYSTERE-FALCON 900, FALCON 900EX, FALCON 2000, and FALCON 2000EX airplanes. This proposed AD was prompted by reports of the wing anti-icing (WAI) system leaking in the wing leading edge. This proposed AD would require a one-time inspection of the WAI system, and corrective actions if necessary, 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.

Full Text

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<title>Federal Register, Volume 88 Issue 130 (Monday, July 10, 2023)</title>
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[Federal Register Volume 88, Number 130 (Monday, July 10, 2023)]
[Proposed Rules]
[Pages 43477-43479]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2023-14367]


========================================================================
Proposed Rules
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains notices to the public of 
the proposed issuance of rules and regulations. The purpose of these 
notices is to give interested persons an opportunity to participate in 
the rule making prior to the adoption of the final rules.

========================================================================


Federal Register / Vol. 88, No. 130 / Monday, July 10, 2023 / 
Proposed Rules

[[Page 43477]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1402; Project Identifier MCAI-2023-00324-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 adopt a new airworthiness directive (AD) 
for certain Dassault Aviation Model MYSTERE-FALCON 900, FALCON 900EX, 
FALCON 2000, and FALCON 2000EX airplanes. This proposed AD was prompted 
by reports of the wing anti-icing (WAI) system leaking in the wing 
leading edge. This proposed AD would require a one-time inspection of 
the WAI system, and corrective actions if necessary, 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 August 24, 
2023.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow 
the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> 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.
    <bullet> 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 <a href="http://regulations.gov">regulations.gov</a> under 
Docket No. FAA-2023-1402; 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:
    <bullet> For material that is proposed for IBR in this NPRM, 
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone 
+49 221 8999 000; email: <a href="/cdn-cgi/l/email-protection#6d2c291e2d080c1e0c4308181f021d0c430818"><span class="__cf_email__" data-cfemail="a4e5e0d7e4c1c5d7c58ac1d1d6cbd4c58ac1d1">[email&#160;protected]</span></a>; website: easa.europa.eu. 
You may find this material on the EASA website: ad.easa.europa.eu. It 
is also available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2023-1402.
    <bullet> You may view this service information 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 <a href="/cdn-cgi/l/email-protection#fa8e9597d488959e88939d8f9f80ba9c9b9bd49d958c"><span class="__cf_email__" data-cfemail="95e1faf8bbe7faf1e7fcf2e0f0efd5f3f4f4bbf2fae3">[email&#160;protected]</span></a>.

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-2023-1402; Project Identifier 
MCAI-2023-00324-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 
<a href="http://regulations.gov">regulations.gov</a>, 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 
<a href="/cdn-cgi/l/email-protection#a3d7ccce8dd1ccc7d1cac4d6c6d9e3c5c2c28dc4ccd5"><span class="__cf_email__" data-cfemail="93e7fcfebde1fcf7e1faf4e6f6e9d3f5f2f2bdf4fce5">[email&#160;protected]</span></a>. Any commentary that the FAA receives which is 
not specifically designated as CBI will be placed in the public docket 
for this rulemaking.

Background

    EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2023-0041, dated February 21, 2023 
(EASA AD 2023-0041) (also referred to as the MCAI), to correct an 
unsafe condition for certain Dassault Aviation Model MYSTERE-FALCON 
900, FALCON 900EX, FALCON 2000, and FALCON 2000EX airplanes. The MCAI 
states the WAI system was reported leaking in the wing leading edge. 
The leaks were either from an incorrect installation of the Wiggins 
coupling on the WAI system, or detachment of the pressure switch line 
from the WAI pipe (only found on the Falcon 2000 and Falcon 2000EX 
airplanes). This condition, if not detected and corrected, could lead 
to a loss of performance of WAI protection system, possibly resulting 
in reduced control of the airplane.
    The FAA is proposing this AD to address the unsafe condition on 
these products. You may examine the MCAI in the AD docket at 
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2023-1402.

[[Page 43478]]

Related Service Information Under 1 CFR Part 51

    EASA AD 2023-0041 specifies procedures for a one-time general 
visual inspection of the WAI system for discrepancies, including 
incorrect installation, deformation, leakage or signs of overheating, 
and lack of free rotation of the clamp around the two ferrules, and, 
depending on findings, corrective actions. Corrective actions include 
replacement or re-installation of the affected WAI Wiggins coupling 
with new seals and couplings. For the Falcon 2000 and Falcon 2000EX 
airplanes, there is an additional one-time general visual inspection of 
the WAI pipes for traces of abnormal leakage, overheating, or 
degradation of the thermal lagging, and depending on findings, 
corrective actions. Corrective actions are for replacement of the 
affected WAI pipes. 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 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 require accomplishing the actions specified 
in EASA AD 2023-0041 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 2023-0041 by reference in the FAA 
final rule. This proposed AD would, therefore, require compliance with 
EASA AD 2023-0041 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 2023-0041 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-
0041. Service information required by EASA AD 2023-0041 for compliance 
will be available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2023-1402 
after the FAA final rule is published.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 820 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
7 work-hours x $85 per hour = $595...........................              $0             $595         $487,900
----------------------------------------------------------------------------------------------------------------

    The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of any 
required actions. The FAA has no way of determining the number of 
aircraft that might need these on-condition actions:

                 Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
           Labor cost               Parts cost       Cost per product
------------------------------------------------------------------------
Up to 2 work-hours x $85 per                $517  Up to $687.
 hour = $170.
------------------------------------------------------------------------

    The FAA has included all known costs in its cost estimate. 
According to the manufacturer, however, some or all of the costs of 
this proposed AD may be covered under warranty, thereby reducing the 
cost impact on affected operators.

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:

[[Page 43479]]

    (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

0
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]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive:

Dassault Aviation: Docket No. FAA-2023-1402; Project Identifier 
MCAI-2023-00324-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by August 24, 2023.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Dassault Aviation Model MYSTERE-FALCON 900, 
FALCON 900EX, FALCON 2000, and FALCON 2000EX airplanes, certificated 
in any category, as identified in European Union Aviation Safety 
Agency (EASA) AD 2023-0041, dated February 21, 2023 (EASA AD 2023-
0041).

(d) Subject

    Air Transport Association (ATA) of America Code: 30, Ice and 
Rain Protection.

(e) Unsafe Condition

    This AD was prompted by reports of the wing anti-icing (WAI) 
system leaking in the wing leading edge. The FAA is issuing this AD 
to address leaks in the WAI system. The unsafe condition, if not 
addressed, could lead to a loss of performance of the WAI protection 
system, possibly resulting in reduced control of the airplane.

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Requirements

    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 2023-0041.

(h) Exceptions to EASA AD 2023-0041

    (1) Where EASA AD 2023-0041 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) Where paragraph (2) of EASA AD 2023-0041 specifies actions 
if ``any discrepancy [as defined in the applicable inspection SB] is 
found,'' for this AD, discrepancies are defined as incorrect 
installation, deformation, leakage, signs of overheating, and lack 
of free rotation of the clamp around the two ferrules.
    (3) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0041.

(i) 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 (j) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#89b0a4c8dfdaa4c8c0dba4bebab9a4c8c4c6cac9efe8e8a7eee6ff"><span class="__cf_email__" data-cfemail="a29b8fe3f4f18fe3ebf08f9591928fe3efede1e2c4c3c38cc5cdd4">[email&#160;protected]</span></a>. 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.

(j) 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 
<a href="/cdn-cgi/l/email-protection#9febf0f2b1edf0fbedf6f8eafae5dff9fefeb1f8f0e9"><span class="__cf_email__" data-cfemail="81f5eeecaff3eee5f3e8e6f4e4fbc1e7e0e0afe6eef7">[email&#160;protected]</span></a>.

(k) 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 2023-0041, 
dated February 21, 2023.
    (ii) [Reserved]
    (3) For EASA AD 2023-0041, contact EASA, Konrad-Adenauer-Ufer 3, 
50668 Cologne, Germany; telephone +49 221 8999 000; email: 
<a href="/cdn-cgi/l/email-protection#6a2b2e192a0f0b190b440f1f18051a0b440f1f"><span class="__cf_email__" data-cfemail="5415102714313527357a3121263b24357a3121">[email&#160;protected]</span></a>; website: easa.europa.eu. You may find this EASA 
AD on the EASA website: ad.easa.europa.eu.
    (4) You may view this service information 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.
    (5) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, email <a href="/cdn-cgi/l/email-protection#b8deca96d1d6cbc8dddbccd1d7d6f8d6d9cad996dfd7ce"><span class="__cf_email__" data-cfemail="5a3c28743334292a3f392e3335341a343b283b743d352c">[email&#160;protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued on July 3, 2023.
Michael Linegang,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-14367 Filed 7-7-23; 8:45 am]
BILLING CODE 4910-13-P


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