Rule2024-15305
Airworthiness Directives; Dassault Aviation Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
July 12, 2024
Effective
August 16, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 7X airplanes. This AD was prompted by a determination that non-conforming washers may have been installed in production on engine 1 and 3 forward yokes. This AD requires a one-time inspection for non-conforming washers and, depending on findings, related investigative and corrective actions, 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.
Full Text
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<title>Federal Register, Volume 89 Issue 134 (Friday, July 12, 2024)</title>
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[Federal Register Volume 89, Number 134 (Friday, July 12, 2024)]
[Rules and Regulations]
[Pages 57075-57077]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-15305]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-0998; Project Identifier MCAI-2023-01212-T;
Amendment 39-22778; AD 2024-13-04]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Dassault Aviation Model FALCON 7X airplanes. This AD was
prompted by a determination that non-conforming washers may have been
installed in production on engine 1 and 3 forward yokes. This AD
requires a one-time inspection for non-conforming washers and,
depending on findings, related investigative and corrective actions, 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 August 16, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 16,
2024.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-0998; or in person at Docket Operations between 9
a.m. and
[[Page 57076]]
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:
<bullet> For EASA material, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#d29396a192b7b3a1b3fcb7a7a0bda2b3fcb7a7"><span class="__cf_email__" data-cfemail="68292c1b280d091b09460d1d1a071809460d1d">[email protected]</span></a>; website easa.europa.eu. You may find this material
on the EASA website at ad.easa.europa.eu. It is also available at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2024-0998.
<bullet> 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 <a href="/cdn-cgi/l/email-protection#14607b793a667b70667d7361716e547275753a737b62"><span class="__cf_email__" data-cfemail="d4a0bbb9faa6bbb0a6bdb3a1b1ae94b2b5b5fab3bba2">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Dassault
Aviation Model FALCON 7X airplanes. The NPRM published in the Federal
Register on April 9, 2024 (89 FR 24748). The NPRM was prompted by AD
2023-0208, dated November 22, 2023 (EASA AD 2023-0208) (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 a quality
review revealed that nonconforming washers may have been installed in
production on engine 1 and 3 forward yokes. This condition, if not
addressed, could lead to cracks in the bolts and the engine forward
yokes, possibly resulting in loss of a lateral engine.
In the NPRM, the FAA proposed to require a one-time inspection for
non-conforming washers and, depending on findings, related
investigative and corrective actions, as specified in EASA AD 2023-
0208. The FAA is issuing 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-2024-0998.
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 2023-0208 specifies procedures for a one-time inspection
for non-conforming (non-compliant) double countersink washers on the
engine 1 and 3 forward yokes, installing the engine 1 and 3 forward
yokes with new attachments, and, depending on findings, related
investigative and corrective actions. Related investigative and
corrective actions include a special detailed fatigue inspection for
cracking of the engine forward yokes and replacement if any cracking is
found. 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 8 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
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Cost on U.S.
Labor cost Parts cost Cost per product operators
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8 work-hours x $85 per hour = $680....................... $16,280 $16,960 $135,680
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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
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Labor cost Parts cost Cost per product
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8 work-hours x $85 per hour = $680 $33,170 $33,850
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The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this 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
[[Page 57077]]
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
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:
2024-13-04 Dassault Aviation: Amendment 39-22778; Docket No. FAA-
2024-0998; Project Identifier MCAI-2023-01212-T.
(a) Effective Date
This airworthiness directive (AD) is effective August 16, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Dassault Aviation Model FALCON 7X airplanes,
certificated in any category, as identified in European Union
Aviation Safety Agency (EASA) AD 2023-0208, dated November 22, 2023
(EASA AD 2023-0208).
(d) Subject
Air Transport Association (ATA) of America Code 71, Powerplant.
(e) Unsafe Condition
This AD was prompted by a determination that non-conforming
washers may have been installed in production on engine 1 and 3
forward yokes. The FAA is issuing this AD to address a condition
that could lead to cracks in the bolts and the engine forward yokes.
The unsafe condition, if not addressed, could result in loss of a
lateral engine.
(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 2023-0208.
(h) Exceptions to EASA AD 2023-0208
(1) Where paragraph (2) of EASA AD 2023-0208 specifies to
``accomplish the corrective actions,'' replace that text with
``accomplish a special detailed fatigue inspection to detect
cracking of the engine forward yoke, and replace before further
flight if any cracking is found.''
(2) This AD does not adopt the ``Remarks'' section of EASA AD
2023-0208.
(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 manager of the
International Validation Branch, mail it to the address identified
in paragraph (j) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#bf8692fee9ec92fef6ed92888c8f92fef2f0fcffd9dede91d8d0c9"><span class="__cf_email__" data-cfemail="1d24305c4b4e305c544f302a2e2d305c50525e5d7b7c7c337a726b">[email 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#cabea5a7e4b8a5aeb8a3adbfafb08aacababe4ada5bc"><span class="__cf_email__" data-cfemail="8afee5e7a4f8e5eef8e3edffeff0caecebeba4ede5fc">[email protected]</span></a>.
(k) 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.
(i) European Union Aviation Safety Agency (EASA) AD 2023-0208,
dated November 22, 2023.
(ii) [Reserved]
(3) For EASA AD 2023-0208, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#d8999cab98bdb9abb9f6bdadaab7a8b9f6bdad"><span class="__cf_email__" data-cfemail="58191c2b183d392b39763d2d2a372839763d2d">[email protected]</span></a>; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(4) 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.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a>, or email <a href="/cdn-cgi/l/email-protection#6f091d4106011c1f0a0c1b0600012f010e1d0e41080019"><span class="__cf_email__" data-cfemail="2046520e494e5350454354494f4e604e4152410e474f56">[email protected]</span></a>.
Issued on June 24, 2024.
James D. Foltz,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-15305 Filed 7-11-24; 8:45 am]
BILLING CODE 4910-13-P
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