Proposed Rule2022-22203
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
October 21, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for certain Dassault Aviation Model FALCON 7X airplanes. This proposed AD was prompted by a report of smoke in the flightdeck and loss of the right-hand (RH) primary display unit (PDU) and the secondary flight display (SFD). This proposed AD would require inspecting the two electrical power feeders for damage (deterioration), measuring the clearance between the two electrical power feeders and the forward lavatory bulkhead, and applicable corrective actions, 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 87 Issue 203 (Friday, October 21, 2022)</title>
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[Federal Register Volume 87, Number 203 (Friday, October 21, 2022)]
[Proposed Rules]
[Pages 63978-63980]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-22203]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1297; Project Identifier MCAI-2022-00570-T]
RIN 2120-AA64
Airworthiness Directives; Dassault Aviation Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Dassault Aviation Model FALCON 7X airplanes. This proposed
AD was prompted by a report of smoke in the flightdeck and loss of the
right-hand (RH) primary display unit (PDU) and the secondary flight
display (SFD). This proposed AD would require inspecting the two
electrical power feeders for damage (deterioration), measuring the
clearance between the two electrical power feeders and the forward
lavatory bulkhead, and applicable corrective actions, 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 December 5,
2022.
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-2022-1297; 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#3273764172575341531c5747405d42531c5747"><span class="__cf_email__" data-cfemail="6021241320050113014e0515120f10014e0515">[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 in the AD docket at <a href="http://regulations.gov">regulations.gov</a> by searching for and
locating Docket No. FAA-2022-1297.
<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, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone 206-231-3226; email
<a href="/cdn-cgi/l/email-protection#dd89b2b0f38fb2b9afb4baa8b8a79dbbbcbcf3bab2ab"><span class="__cf_email__" data-cfemail="9acef5f7b4c8f5fee8f3fdefffe0dafcfbfbb4fdf5ec">[email 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-2022-1297; Project Identifier
MCAI-2022-00570-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
[[Page 63979]]
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, Aerospace Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200 South 216th St., Des Moines, WA
98198; telephone 206-231-3226; email <a href="/cdn-cgi/l/email-protection#65310a084b370a01170c0210001f250304044b020a13"><span class="__cf_email__" data-cfemail="fca89391d2ae93988e959b899986bc9a9d9dd29b938a">[email 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 2022-0073, dated April 27, 2022
(EASA AD 2022-0073) (also referred to as the MCAI), to correct an
unsafe condition for certain Dassault Aviation Model FALCON 7X
airplanes.
This proposed AD was prompted by a report of smoke in the
flightdeck and loss of the RH PDU and the SFD. The subsequent
investigation determined that chafing and arcing of the electrical
power feeders with the forward lavatory bulkhead led to smoke and loss
of the RH PDU and the SFD power supply. The FAA is proposing this AD to
address chafing and arcing of the electrical power feeders with the
forward lavatory bulkhead, which could lead to loss of systems
supporting flight automation and flight displays and reduced
situational awareness, possibly resulting in a significant increase of
flightcrew workload and injury to occupants. See the MCAI for
additional background information.
Related Service Information Under 1 CFR Part 51
EASA AD 2022-0073 specifies procedures for inspecting the two
electrical power feeders for damage (deterioration), measuring the
clearance between the two electrical power feeders and the forward
lavatory bulkhead, and applicable corrective actions. The corrective
actions include repairing any electrical power feeder with
deterioration and modifying the forward lavatory bulkhead. If a
clearance of more than 1 millimeter (mm) but less than or equal to 13
mm is detected, the corrective action includes installing ROUNDIT200NX
sheath on the affected electrical power feeder using white binding
braid. If a clearance of more than 13 mm is detected, the corrective
action includes looking for the presence of a blue cable grip around
the electrical power feeders and installing it if it is missing. 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 the 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 2022-0073 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 2022-0073 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2022-0073 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 2022-0073 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 2022-
0073. Service information required by EASA AD 2022-0073 for compliance
will be available at <a href="http://regulations.gov">regulations.gov</a> by searching for and locating
Docket No. FAA-2022-1297 after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this proposed AD would affect 45 airplanes
of U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:
Estimated Costs for Required Actions
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Cost per Cost on U.S.
Labor cost Parts cost product operators
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2 work-hours x $85 per hour = $170........................... $0 $170 $7,650
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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:
[[Page 63980]]
Estimated Costs of On-Condition Actions
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Labor cost Parts cost Cost per product
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Up to 33 work-hours x $85 per Up to $431........ Up to $3,236.
hour = $2,805.
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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 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:
(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-2022-1297; Project Identifier
MCAI-2022-00570-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by December 5, 2022.
(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 2022-0073, dated April 27, 2022
(EASA AD 2022-0073).
(d) Subject
Air Transport Association (ATA) of America Code 24, Electrical
power.
(e) Unsafe Condition
This AD was prompted by a report of smoke in the flightdeck and
loss of the right-hand primary display unit (PDU) and the secondary
flight display (SFD). The FAA is issuing this AD to address chafing
and arcing of the electrical power feeders with the forward lavatory
bulkhead, which could lead loss of systems supporting flight
automation and flight displays and reduced situational awareness,
possibly resulting in a significant increase of flightcrew workload
and injury to occupants.
(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 2022-0073.
(h) Exceptions to EASA AD 2022-0073
(1) Where EASA AD 2022-0073 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2022-0073 does not apply
to this AD.
(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)(2) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#c6ffeb879095eb878f94ebf1f5f6eb878b898586a0a7a7e8a1a9b0"><span class="__cf_email__" data-cfemail="330a1e7265601e727a611e0400031e727e7c70735552521d545c45">[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) Related Information
(1) For EASA AD 2022-0073, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#a8e9ecdbe8cdc9dbc986cddddac7d8c986cddd"><span class="__cf_email__" data-cfemail="6c2d281f2c090d1f0d4209191e031c0d420919">[email protected]</span></a>; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu. 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.
This material may be found in the AD docket at <a href="http://regulations.gov">regulations.gov</a> by
searching for and locating Docket No. FAA-2022-1297.
(2) For more information about this AD, contact Tom Rodriguez,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone 206-231-3226; email <a href="/cdn-cgi/l/email-protection#7b2f14165529141f09121c0e1e013b1d1a1a551c140d"><span class="__cf_email__" data-cfemail="15417a783b477a71677c7260706f557374743b727a63">[email protected]</span></a>.
Issued on October 6, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-22203 Filed 10-20-22; 8:45 am]
BILLING CODE 4910-13-P
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