Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines, 43426-43429 [2023-14585]
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Federal Register / Vol. 88, No. 130 / Monday, July 10, 2023 / Rules and Regulations
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List of Subjects in 5 CFR Part 2429
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procedure, Government employees,
Labor management relations.
For the reasons stated in the
preamble, the FLRA amends 5 CFR part
2429 as follows:
documents on that party exclusively by
email to the email address provided by
the party.
*
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(c) Proof of service. Proof of service
shall be verified by certificate of the
individual serving the papers describing
the manner of such service. When
service is by mail, the date of service
shall be the day when the matter served
is deposited in the United States mail.
When service is by facsimile, the date of
service shall be the date the facsimile
transmission is transmitted and, when
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record of transmission. When parties are
served documents by the Authority by
email, the date of service shall be the
date the email is sent.
Approved: July 3, 2023.
Rebecca J. Osborne,
Federal Register Liaison, Federal Labor
Relations Authority.
[FR Doc. 2023–14399 Filed 7–7–23; 8:45 am]
PART 2429—MISCELLANEOUS AND
GENERAL REQUIREMENTS
1. The authority citation for part 2429
continues to read as follows:
■
DEPARTMENT OF TRANSPORTATION
Authority: 5 U.S.C. 7134; § 2429.18 also
issued under 28 U.S.C. 2112(a).
Federal Aviation Administration
2. Amend § 2429.12 by revising
paragraphs (a) and (c) to read as follows:
14 CFR Part 39
■
§ 2429.12 Service of process and papers
by the Authority.
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BILLING CODE 7627–01–P
(a) Methods of service. Notices of
hearings, decisions and orders of
Regional Directors, decisions and
recommended orders of Administrative
Law Judges, decisions of the Authority,
complaints, amended complaints,
withdrawals of complaints, written
rulings on motions, and all other papers
required by this subchapter to be issued
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party under part 2423 of this
subchapter, shall be served personally,
by first-class mail, by facsimile
transmission, by certified mail, or, as
described below with respect to
documents issued by the Authority, by
electronic mail (hereinafter, ‘‘email’’).
Where facsimile equipment is available,
rulings on motions; information
pertaining to prehearing disclosure,
conferences, orders, or hearing dates,
and locations; information pertaining to
subpoenas; and other similar or time
sensitive matters may be served by
facsimile transmission. Where a party
using the FLRA’s eFiling system has
consented to electronic service of
documents issued by the Authority in a
particular case, the Authority shall serve
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[Docket No. FAA–2023–1411; Project
Identifier MCAI–2023–00710–E; Amendment
39–22499; AD 2023–13–14]
RIN 2120–AA64
Airworthiness Directives; Safran
Helicopter Engines, S.A. (Type
Certificate Previously Held by
Turbomeca, S.A.) Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2023–01–
12, which applied to all Safran
Helicopter Engines, S.A. (Safran) Model
Arriel 1C, Arriel 1C1, and Arriel 1C2
engines. AD 2023–01–12 required
replacing affected fire detectors and
prohibited installation of affected fire
detectors. Since the FAA issued AD
2023–01–12, the FAA has determined
that Model Arriel 1K1 engines are also
affected by the unsafe condition. This
AD is prompted by reports of false
engine fire warnings. This AD requires
replacing the affected fire detectors,
prohibits installation of affected fire
detectors, and adds Model Arriel 1K1
engines to the applicability, as specified
in an European Union Aviation Safety
Agency (EASA) AD, which is
incorporated by reference (IBR). The
SUMMARY:
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FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective July 25,
2023.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of July 25, 2023.
The FAA must receive comments on
this 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:
• 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–2023–1411; 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 street address for
Docket Operations is listed above.
Material Incorporated by Reference:
• For service information
incorporated by reference in this final
rule, contact EASA, Konrad-AdenauerUfer 3, 50668 Cologne, Germany; phone:
+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.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 1200 District Avenue,
Burlington, MA 01803. For information
on the availability of this material at the
FAA, call (817) 222–5110. It is also
available at regulations.gov under
Docket No. FAA–2023–1411.
FOR FURTHER INFORMATION CONTACT:
Kevin Clark, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (781) 238–
7088; email: kevin.m.clark@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written data, views, or arguments about
this final rule. Send your comments to
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an address listed under ADDRESSES.
Include ‘‘Docket No. FAA–2023–1411;
Project Identifier MCAI–2023–00710–E’’
at the beginning of your comments. The
most helpful comments reference a
specific portion of the final rule, 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 final rule 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 final rule.
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 AD 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 AD,
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 AD. Submissions containing CBI
should be sent to Kevin Clark, Aviation
Safety Engineer, FAA, 1600 Stewart
Avenue, Suite 410, Westbury, NY
11590. Any commentary that the FAA
receives which is not specifically
designated as CBI will be placed in the
public docket for this rulemaking.
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Background
The FAA issued AD 2023–01–12,
Amendment 39–22306 (88 FR 3629,
January 20, 2023) (AD 2023–01–12), for
all Safran Helicopter Engines, S.A.
(Type Certificate previously held by
Turbomeca, S.A.) Model Arriel 1C,
Arriel 1C1, and Arriel 1C2 engines. AD
2023–01–12 was prompted by an MCAI
originated by EASA, which is the
Technical Agent for the Member States
of the European Union. EASA issued
EASA AD 2022–0256, dated December
19, 2022 (EASA AD 2022–0256) to
correct an unsafe condition identified as
reports of false engine fire warnings.
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AD 2023–01–12 required replacing
the affected fire detectors and
prohibited installation of affected fire
detectors, as specified in EASA AD
2022–0256. The FAA issued AD 2023–
01–12 to prevent false engine fire
warnings.
Actions Since AD 2023–01–12 Was
Issued
Since the FAA issued AD 2023–01–
12, EASA superseded EASA AD 2022–
0256 and issued EASA AD 2023–0110,
dated May 26, 2023 (EASA AD 2023–
0110) (referred to after this as the
MCAI). The MCAI states that Safran
determined that Model Arriel 1K and
Arriel 1K1 engines may also have the
affected fire detectors installed and are
subject to the same unsafe condition.
The MCAI retains the requirements of
EASA AD 2022–0256 and expands the
applicability to include the Model
Arriel 1K and Arriel 1K1 engines.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2023–1411.
Related Service Information Under 1
CFR Part 51
The FAA reviewed EASA AD 2023–
0110, which specifies procedures for
replacing affected fire detectors. EASA
AD 2023–0110 also specifies not to
install an affected fire detector on any
engine. This service information is
reasonably available because the
interested parties have access to it
through their normal course of business
or by the means identified in
ADDRESSES.
This service information is reasonably
available because the interested parties
have access to it through their normal
course of business or by the means
identified in ADDRESSES.
FAA’s Determination
These products have been approved
by the aviation authority of another
country and are 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 described above.
The FAA is issuing this AD after
determining that the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design.
AD Requirements
This AD retains none of the
requirements of AD 2023–01–12, This
AD adds Model Arriel 1K1 engines to
the applicability and requires
accomplishing the actions specified in
the MCAI already described, except for
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43427
any differences identified as exceptions
in the regulatory text of this AD, and
except as discussed under ‘‘Differences
Between this AD and the MCAI’’.
Differences Between This AD and the
MCAI
Model Arriel 1K engines are
contained in the applicability of EASA
AD 2023–0110 but do not have an FAA
type certificate. Therefore, this AD does
not include those engines in the
applicability.
Justification for Immediate Adoption
and Determination of the Effective Date
Section 553(b)(3)(B) of the
Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies
to dispense with notice and comment
procedures for rules when the agency,
for ‘‘good cause,’’ finds that those
procedures are ‘‘impracticable,
unnecessary, or contrary to the public
interest.’’ Under this section, an agency,
upon finding good cause, may issue a
final rule without providing notice and
seeking comment prior to issuance.
Further, section 553(d) of the APA
authorizes agencies to make rules
effective in less than thirty days, upon
a finding of good cause.
An unsafe condition exists that
requires the immediate adoption of this
AD without providing an opportunity
for public comments prior to adoption.
The FAA has found that the risk to the
flying public justifies foregoing notice
and comment prior to adoption of this
rule because fire detectors that do not
conform to the type design could lead
to false engine fire warnings. Safran was
informed of three occurrences of
illumination of the engine fire alarm
without confirmed fire (untimely
illumination) on airframes equipped
with affected fire detectors. False engine
fire warnings are an unsafe condition
requiring urgent corrective action
because, if a helicopter is equipped with
two engines with an affected fire
detector installed, an engine fire
warning could occur on both engines
during the same flight. This unsafe
condition, if not addressed, could lead
to commanded in-flight engine shutdown, possibly resulting in damage to
the helicopter and reduced control of
the helicopter. Replacement of the fire
detectors for Model Arriel 1K1 engines
requires compliance within 30 flight
hours or 60 days from the effective date
of this AD. Replacement of the fire
detectors for Model Arriel 1C, Arriel
1C1, and Arriel 1C2 engines requires
compliance before further flight.
Accordingly, notice and opportunity for
prior public comment are impracticable
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Federal Register / Vol. 88, No. 130 / Monday, July 10, 2023 / Rules and Regulations
and contrary to the public interest
pursuant to 5 U.S.C. 553(b)(3)(B).
In addition, the FAA finds that good
cause exists pursuant to 5 U.S.C. 553(d)
for making this amendment effective in
less than 30 days, for the same reasons
the FAA found good cause to forgo
notice and comment.
Regulatory Flexibility Act
The requirements of the Regulatory
Flexibility Act (RFA) do not apply when
an agency finds good cause pursuant to
5 U.S.C. 553 to adopt a rule without
prior notice and comment. Because FAA
has determined that it has good cause to
adopt this rule without prior notice and
comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD
affects 30 engines installed on
helicopters of U.S. registry.
The FAA estimates the following
costs to comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Replace fire detectors ......................
1 work-hour × $85 per hour = $85 ...............................
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,
and
(2) Will not affect intrastate aviation
in Alaska.
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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,
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Parts cost
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by:
a. Removing Airworthiness Directive
2023–01–12, Amendment 39–22306 (88
FR 3629, January 20, 2023); and
■ b. Adding the following new
airworthiness directive:
■
■
2023–13–14 Safran Helicopter Engines,
S.A. (Type Certificate Previously Held
by Turbomeca, S.A.): Amendment 39–
22499; Docket No. FAA–2023–1411;
Project Identifier MCAI–2023–00710–E.
(a) Effective Date
This airworthiness directive (AD) is
effective July 25, 2023.
(b) Affected ADs
This AD replaces AD 2023–01–12,
Amendment 39–22306 (88 FR 3629, January
20, 2023) (AD 2023–01–12).
(c) Applicability
This AD applies to all Safran Helicopter
Engines, S.A. (Type Certificate previously
held by Turbomeca, S.A.) Model Arriel 1C,
Arriel 1C1, Arriel 1C2, and Arriel 1K1
engines.
(d) Subject
Joint Aircraft System Component (JASC)
Code 7200, Engine (Turbine/Turboprop).
(e) Unsafe Condition
This AD was prompted by false engine fire
warnings. The FAA is issuing this AD to
prevent false engine fire warnings. The
unsafe condition, if not addressed, could lead
to commanded in-flight engine shut-down,
possibly resulting in damage to the helicopter
and reduced control of the helicopter.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
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$1,800
Cost per
product
$1,885
Cost on U.S.
operators
$56,550
(g) Required Actions
Except as specified in paragraphs (h) and
(i) of this AD: Perform all required actions
within the compliance times specified in,
and in accordance with European Union
Aviation Safety Agency (EASA) AD 2023–
0110, dated May 26, 2023.
(h) Exceptions to EASA AD 2023–0110
(1) Where the ‘‘Reference Date’’ for Model
Arriel 1K1 engines in Table 1 of EASA AD
2023–0110 specifies ‘‘The effective date of
this [EASA] AD,’’ this AD requires using the
effective date of this AD.
(2) Where the ‘‘Reference Date’’ for Model
Arriel 1C, Arriel 1C1, and Arriel 1C2 engines
in Table 1 of EASA AD 2023–0110 specifies
‘‘02 January 2023,’’ this AD requires
compliance before further flight.
(3) This AD does not adopt the Remarks
paragraph of EASA AD 2023–0110.
(4) Although the service information
referenced in EASA AD 2023–0110 specifies
to discard any removed fire detectors, this
AD requires removing those parts from
service.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2023–0110 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(j) Alternative Methods of Compliance
(AMOCs)
(1) 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 local
Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the International Validation
Branch, send it to the attention of the person
identified in paragraph (k) of this AD and
email to: ANE-AD-AMOC@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(k) Additional Information
For more information about this AD,
contact Kevin Clark, Aviation Safety
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Federal Register / Vol. 88, No. 130 / Monday, July 10, 2023 / Rules and Regulations
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; phone: (781) 238–
7088; email: kevin.m.clark@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference 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 the AD specifies otherwise.
(i) European Union Aviation Safety Agency
AD 2023–0110, dated May 26, 2023.
(ii) [Reserved]
(3) For EASA AD 2023–0110, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; phone: +49 221 8999 000;
email: ADs@easa.europa.eu. You may find
this material on the EASA website at
ad.easa.europa.eu.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
Avenue, Burlington, MA 01803. For
information on the availability of this
material at the FAA, call (817) 222–5110.
(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: fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on June 30, 2023.
Michael Linegang,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–14585 Filed 7–6–23; 11:15 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2023–1077; Airspace
Docket No. 23–AGL–16]
RIN 2120–AA66
Amendment of Class E Airspace;
Devils Lake, ND
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action amends the Class
E airspace at Devils Lake, ND. This
action is the result of an airspace review
caused by the decommissioning of the
Devils Lake very high frequency
omnidirectional range (VOR) as part of
the VOR Minimum Operating Network
(MON) Program. The geographic
coordinates of the airport are also being
updated to coincide with the FAA’s
aeronautical database.
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SUMMARY:
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Effective 0901 UTC, October 5,
2023. The Director of the Federal
Register approves this incorporation by
reference action under 1 CFR part 51,
subject to the annual revision of FAA
Order JO 7400.11 and publication of
conforming amendments.
ADDRESSES: A copy of the Notice of
Proposed Rulemaking (NPRM), all
comments received, this final rule, and
all background material may be viewed
online at www.regulations.gov using the
FAA Docket number. Electronic
retrieval help and guidelines are
available on the website. It is available
24 hours each day, 365 days each year.
FAA Order JO 7400.11G, Airspace
Designations and Reporting Points, and
subsequent amendments can be viewed
online at www.faa.gov/air_traffic/
publications/. You may also contact the
Rules and Regulations Group, Office of
Policy, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC 20591;
telephone: (202) 267–8783.
FOR FURTHER INFORMATION CONTACT:
Jeffrey Claypool, Federal Aviation
Administration, Operations Support
Group, Central Service Center, 10101
Hillwood Parkway, Fort Worth, TX
76177; telephone (817) 222–5711.
SUPPLEMENTARY INFORMATION:
DATES:
Authority for This Rulemaking
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it amends the
Class E surface airspace and the Class E
airspace extending upward from 700
feet above the surface at Devils Lake
Regional Airport, Devils Lake, ND, to
support instrument flight rule
operations at this airport.
History
The FAA published an NPRM for
Docket No. FAA–2023–1077 in the
Federal Register (88 FR 29563; May 8,
2023) proposing to amend the Class E
airspace at Devils Lake, ND. Interested
parties were invited to participate in
this rulemaking effort by submitting
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43429
written comments on the proposal to the
FAA. No comments were received.
Incorporation by Reference
Class E airspace designations are
published in paragraphs 6002 and 6005
of FAA Order JO 7400.11, Airspace
Designations and Reporting Points,
which is incorporated by reference in 14
CFR 71.1 on an annual basis. This
document amends the current version of
that order, FAA Order JO 7400.11G,
dated August 19, 2022, and effective
September 15, 2022. FAA Order JO
7400.11G is publicly available as listed
in the ADDRESSES section of this
document. These amendments will be
published in the next update to FAA
Order JO 7400.11.
FAA Order JO 7400.11G lists Class A,
B, C, D, and E airspace areas, air traffic
service routes, and reporting points.
The Rule
This amendment to 14 CFR part 71:
Modifies the Class E surface airspace
to within a 4.3-mile (increased from a 4mile) radius of Devils Lake Regional
Airport, Devils Lake, ND; removes the
Devils Lake VOR/DME and associated
extensions from the airspace legal
description; updates the geographic
coordinates of the airport to coincide
with the FAA’s aeronautical database;
and replaces the outdated term ‘‘Notice
to Airmen’’ with ‘‘Notice to Air
Missions’’;
Modifies the Class E airspace
extending upward from 700 feet above
the surface to within a 6.8-mile
(decreased from an 8.7-mile) radius of
Devils Lake Regional Airport; removes
the Devils Lake VOR/DME from the
airspace legal description; removes the
Class E airspace extending upward from
1,200 feet above the surface as it is now
redundant with the Class E airspace
extending upward from 1,200 feet above
the surface over the State of North
Dakota; and updates geographic
coordinates of the airport to coincide
with the FAA’s aeronautical database.
Regulatory Notices and Analyses
The FAA has determined that this
regulation only involves an established
body of technical regulations for which
frequent and routine amendments are
necessary to keep them operationally
current. It, therefore: (1) is not a
‘‘significant regulatory action’’ under
Executive Order 12866; (2) is not a
‘‘significant rule’’ under DOT
Regulatory Policies and Procedures (44
FR 11034; February 26, 1979); and (3)
does not warrant preparation of a
regulatory evaluation as the anticipated
impact is so minimal. Since this is a
routine matter that only affects air traffic
E:\FR\FM\10JYR1.SGM
10JYR1
Agencies
[Federal Register Volume 88, Number 130 (Monday, July 10, 2023)]
[Rules and Regulations]
[Pages 43426-43429]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-14585]
=======================================================================
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1411; Project Identifier MCAI-2023-00710-E;
Amendment 39-22499; AD 2023-13-14]
RIN 2120-AA64
Airworthiness Directives; Safran Helicopter Engines, S.A. (Type
Certificate Previously Held by Turbomeca, S.A.) Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-01-
12, which applied to all Safran Helicopter Engines, S.A. (Safran) Model
Arriel 1C, Arriel 1C1, and Arriel 1C2 engines. AD 2023-01-12 required
replacing affected fire detectors and prohibited installation of
affected fire detectors. Since the FAA issued AD 2023-01-12, the FAA
has determined that Model Arriel 1K1 engines are also affected by the
unsafe condition. This AD is prompted by reports of false engine fire
warnings. This AD requires replacing the affected fire detectors,
prohibits installation of affected fire detectors, and adds Model
Arriel 1K1 engines to the applicability, as specified in an European
Union Aviation Safety Agency (EASA) AD, which is incorporated by
reference (IBR). The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective July 25, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 25,
2023.
The FAA must receive comments on this 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:
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-2023-1411; 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
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For service information incorporated by reference in this
final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne,
Germany; phone: +49 221 8999 000; email: [email protected]; website:
easa.europa.eu. You may find this material on the EASA website at
ad.easa.europa.eu.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110. It is
also available at regulations.gov under Docket No. FAA-2023-1411.
FOR FURTHER INFORMATION CONTACT: Kevin Clark, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (781)
238-7088; email: [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to
[[Page 43427]]
an address listed under ADDRESSES. Include ``Docket No. FAA-2023-1411;
Project Identifier MCAI-2023-00710-E'' at the beginning of your
comments. The most helpful comments reference a specific portion of the
final rule, 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 final rule 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 final rule.
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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Kevin
Clark, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590. 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 2023-01-12, Amendment 39-22306 (88 FR 3629,
January 20, 2023) (AD 2023-01-12), for all Safran Helicopter Engines,
S.A. (Type Certificate previously held by Turbomeca, S.A.) Model Arriel
1C, Arriel 1C1, and Arriel 1C2 engines. AD 2023-01-12 was prompted by
an MCAI originated by EASA, which is the Technical Agent for the Member
States of the European Union. EASA issued EASA AD 2022-0256, dated
December 19, 2022 (EASA AD 2022-0256) to correct an unsafe condition
identified as reports of false engine fire warnings.
AD 2023-01-12 required replacing the affected fire detectors and
prohibited installation of affected fire detectors, as specified in
EASA AD 2022-0256. The FAA issued AD 2023-01-12 to prevent false engine
fire warnings.
Actions Since AD 2023-01-12 Was Issued
Since the FAA issued AD 2023-01-12, EASA superseded EASA AD 2022-
0256 and issued EASA AD 2023-0110, dated May 26, 2023 (EASA AD 2023-
0110) (referred to after this as the MCAI). The MCAI states that Safran
determined that Model Arriel 1K and Arriel 1K1 engines may also have
the affected fire detectors installed and are subject to the same
unsafe condition. The MCAI retains the requirements of EASA AD 2022-
0256 and expands the applicability to include the Model Arriel 1K and
Arriel 1K1 engines.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1411.
Related Service Information Under 1 CFR Part 51
The FAA reviewed EASA AD 2023-0110, which specifies procedures for
replacing affected fire detectors. EASA AD 2023-0110 also specifies not
to install an affected fire detector on any engine. This service
information is reasonably available because the interested parties have
access to it through their normal course of business or by the means
identified in ADDRESSES.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in ADDRESSES.
FAA's Determination
These products have been approved by the aviation authority of
another country and are 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 described above. The FAA is issuing this AD after determining
that the unsafe condition described previously is likely to exist or
develop on other products of the same type design.
AD Requirements
This AD retains none of the requirements of AD 2023-01-12, This AD
adds Model Arriel 1K1 engines to the applicability and requires
accomplishing the actions specified in the MCAI already described,
except for any differences identified as exceptions in the regulatory
text of this AD, and except as discussed under ``Differences Between
this AD and the MCAI''.
Differences Between This AD and the MCAI
Model Arriel 1K engines are contained in the applicability of EASA
AD 2023-0110 but do not have an FAA type certificate. Therefore, this
AD does not include those engines in the applicability.
Justification for Immediate Adoption and Determination of the Effective
Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies foregoing notice and comment prior to adoption of this rule
because fire detectors that do not conform to the type design could
lead to false engine fire warnings. Safran was informed of three
occurrences of illumination of the engine fire alarm without confirmed
fire (untimely illumination) on airframes equipped with affected fire
detectors. False engine fire warnings are an unsafe condition requiring
urgent corrective action because, if a helicopter is equipped with two
engines with an affected fire detector installed, an engine fire
warning could occur on both engines during the same flight. This unsafe
condition, if not addressed, could lead to commanded in-flight engine
shut-down, possibly resulting in damage to the helicopter and reduced
control of the helicopter. Replacement of the fire detectors for Model
Arriel 1K1 engines requires compliance within 30 flight hours or 60
days from the effective date of this AD. Replacement of the fire
detectors for Model Arriel 1C, Arriel 1C1, and Arriel 1C2 engines
requires compliance before further flight. Accordingly, notice and
opportunity for prior public comment are impracticable
[[Page 43428]]
and contrary to the public interest pursuant to 5 U.S.C. 553(b)(3)(B).
In addition, the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days,
for the same reasons the FAA found good cause to forgo notice and
comment.
Regulatory Flexibility Act
The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because FAA has determined
that it has good cause to adopt this rule without prior notice and
comment, RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 30 engines installed on
helicopters of U.S. registry.
The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replace fire detectors................ 1 work-hour x $85 per $1,800 $1,885 $56,550
hour = $85.
----------------------------------------------------------------------------------------------------------------
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, and
(2) Will not affect intrastate aviation in Alaska.
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:
0
a. Removing Airworthiness Directive 2023-01-12, Amendment 39-22306 (88
FR 3629, January 20, 2023); and
0
b. Adding the following new airworthiness directive:
2023-13-14 Safran Helicopter Engines, S.A. (Type Certificate
Previously Held by Turbomeca, S.A.): Amendment 39-22499; Docket No.
FAA-2023-1411; Project Identifier MCAI-2023-00710-E.
(a) Effective Date
This airworthiness directive (AD) is effective July 25, 2023.
(b) Affected ADs
This AD replaces AD 2023-01-12, Amendment 39-22306 (88 FR 3629,
January 20, 2023) (AD 2023-01-12).
(c) Applicability
This AD applies to all Safran Helicopter Engines, S.A. (Type
Certificate previously held by Turbomeca, S.A.) Model Arriel 1C,
Arriel 1C1, Arriel 1C2, and Arriel 1K1 engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 7200, Engine
(Turbine/Turboprop).
(e) Unsafe Condition
This AD was prompted by false engine fire warnings. The FAA is
issuing this AD to prevent false engine fire warnings. The unsafe
condition, if not addressed, could lead to commanded in-flight
engine shut-down, possibly resulting in damage to the helicopter and
reduced control of the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Except as specified in paragraphs (h) and (i) of this AD:
Perform all required actions within the compliance times specified
in, and in accordance with European Union Aviation Safety Agency
(EASA) AD 2023-0110, dated May 26, 2023.
(h) Exceptions to EASA AD 2023-0110
(1) Where the ``Reference Date'' for Model Arriel 1K1 engines in
Table 1 of EASA AD 2023-0110 specifies ``The effective date of this
[EASA] AD,'' this AD requires using the effective date of this AD.
(2) Where the ``Reference Date'' for Model Arriel 1C, Arriel
1C1, and Arriel 1C2 engines in Table 1 of EASA AD 2023-0110
specifies ``02 January 2023,'' this AD requires compliance before
further flight.
(3) This AD does not adopt the Remarks paragraph of EASA AD
2023-0110.
(4) Although the service information referenced in EASA AD 2023-
0110 specifies to discard any removed fire detectors, this AD
requires removing those parts from service.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2023-0110
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) Alternative Methods of Compliance (AMOCs)
(1) 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 local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of the International Validation Branch, send
it to the attention of the person identified in paragraph (k) of
this AD and email to: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(k) Additional Information
For more information about this AD, contact Kevin Clark,
Aviation Safety
[[Page 43429]]
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: (781) 238-7088; email: [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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 the AD specifies otherwise.
(i) European Union Aviation Safety Agency AD 2023-0110, dated
May 26, 2023.
(ii) [Reserved]
(3) For EASA AD 2023-0110, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; phone: +49 221 8999 000; email:
[email protected]. You may find this material on the EASA website
at ad.easa.europa.eu.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110.
(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: [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on June 30, 2023.
Michael Linegang,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-14585 Filed 7-6-23; 11:15 am]
BILLING CODE 4910-13-P