Proposed Rule2025-03983
Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
Primary source
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Published
March 13, 2025
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran) Model ARRIUS 2F and ARRIUS 2R engines. This proposed AD was prompted by a manufacturer investigation that revealed certain high-pressure (HP) turbine blades may contain non-compliant porosity rates due to a change in the manufacturing process. This proposed AD would require replacement of affected HP turbine blades, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 90 Issue 48 (Thursday, March 13, 2025)</title>
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[Federal Register Volume 90, Number 48 (Thursday, March 13, 2025)]
[Proposed Rules]
[Pages 11914-11916]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2025-03983]
[[Page 11914]]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0341; Project Identifier MCAI-2024-00679-E]
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: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for all Safran Helicopter Engines, S.A. (Safran) Model ARRIUS 2F and
ARRIUS 2R engines. This proposed AD was prompted by a manufacturer
investigation that revealed certain high-pressure (HP) turbine blades
may contain non-compliant porosity rates due to a change in the
manufacturing process. This proposed AD would require replacement of
affected HP turbine blades, as specified in a European Union Aviation
Safety Agency (EASA) AD, which is incorporated by reference. The FAA is
proposing this AD to address the unsafe condition on these products.
DATES: The FAA must receive comments on this NPRM by April 28, 2025.
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-2025-0341; 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 EASA material identified in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999
000; email: <a href="/cdn-cgi/l/email-protection#b2f3f6c1f2d7d3c1d39cd7c7c0ddc2d39cd7c7"><span class="__cf_email__" data-cfemail="4b0a0f380b2e2a382a652e3e39243b2a652e3e">[email protected]</span></a>; website: easa.europa.eu. You may find
this material on the EASA website at ad.easa.europa.eu.
<bullet> You may view this material at the FAA, Operational Safety
Branch, 1200 District Avenue, Burlington, MA 01803. For information on
the availability of this material at the FAA, call (817) 222-5110.
FOR FURTHER INFORMATION CONTACT: David Bergeron, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: (860) 386-1805; email: <a href="/cdn-cgi/l/email-protection#1074716679743e7a3e7275627775627f7e507671713e777f66"><span class="__cf_email__" data-cfemail="771316011e13591d5915120510120518193711161659101801">[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-2025-0341; Project Identifier
MCAI-2024-00679-E'' 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 David
Bergeron, 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 EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2024-0218, dated November 18, 2024
(EASA AD 2024-0218), to correct an unsafe condition on all Safran Model
ARRIUS 2F and ARRIUS 2R engines. EASA AD 2024-0218 states that a
manufacturer investigation revealed certain HP turbine blades may have
a weakened mechanical strength and be susceptible to premature rupture
due to non-compliant porosity rates caused by a change in the
manufacturing process. Since EASA issued EASA AD 2024-0218, Safran
published a revised service bulletin to increase the use limits from
2,500 engine cycles to 4,500 engine cycles (ARRIUS 2F engines) and from
5,000 engine cycles to 9,000 engine cycles (ARRIUS 2R engines). Based
on this, EASA issued EASA AD 2024-0218R1, dated December 19, 2024 (EASA
AD 2024-0218R1) (also referred to as the MCAI). The weakened mechanical
strength and potential premature rupture of HP turbine blades, if not
corrected, could lead to an in-flight shutdown and a significant
reduction of the control of the helicopter.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2025-0341.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed EASA AD 2024-0218R1, which specifies procedures
for replacement of the affected HP turbine blades with serviceable HP
turbine blades. 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
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 referenced above. The FAA is issuing this NPRM
[[Page 11915]]
after determining that the unsafe condition described previously is
likely to exist or develop on other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in the material already described, except for any differences
identified as exceptions in the regulatory text of this AD.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 127 engines installed on helicopters of U.S. registry.
The FAA estimates the following costs to comply with this proposed
AD:
Estimated Costs
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Cost per Cost on U.S.
Action Labor cost Parts cost product operators
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Replace HP turbine blades................ 40 work-hours x $85 per $103,250 $106,650 $13,544,550
hour = $3,400.
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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(f), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Safran Helicopter Engines, S.A. (Type Certificate Previously Held by
Turbomeca S.A.): Docket No. FAA-2025-0341; Project Identifier MCAI-
2024-00679-E.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by April 28, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Safran Helicopter Engines, S.A. (type
certificate previously held by Turbomeca S.A) (Safran) Model ARRIUS
2F and ARRIUS 2R engines, as identified in European Union Aviation
Safety Agency (EASA) AD 2024-0218R1, dated December 19, 2024 (EASA
AD 2024-0218R1).
(d) Subject
Joint Aircraft System Component (JASC) Code 7250, Turbine
Section.
(e) Unsafe Condition
This AD was prompted by a manufacturer investigation that
revealed certain high-pressure (HP) turbine blades may have a
weakened mechanical strength, making them susceptible to premature
rupture due to non-compliant porosity rates caused by a change in
the manufacturing process. The FAA is issuing this AD to prevent
failure of the HP turbine blades. The unsafe condition, if not
addressed, could result in an in-flight shutdown and a significant
reduction in the 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: Comply
with all required actions and compliance times specified in, and in
accordance with EASA AD 2024-0218R1.
(h) Exceptions to EASA AD 2024-0218R1
(1) Where EASA AD 2024-0218R1 requires compliance from its
effective date, this AD requires using the effective date of this
AD.
(2) Where EASA AD 2024-0218R1 defines a serviceable part as ``A
HP turbine blade, eligible for installation in accordance with
SAFRAN instructions, that is not an affected part,'' this AD
requires replacing that text with ``Any HP turbine blade, eligible
for installation, that is not an affected part.''
(3) This AD does not adopt the ``Remarks'' section of EASA AD
2024-0218R1.
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2024-
0218R1 specifies to submit certain information to the manufacturer,
this AD does not include that requirement.
(j) 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 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: <a href="/cdn-cgi/l/email-protection#aeefe3e1edeec8cfcf80c9c1d8"><span class="__cf_email__" data-cfemail="7c3d31333f3c1a1d1d521b130a">[email protected]</span></a>.
(k) Additional Information
For more information about this AD, contact David Bergeron,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (860) 386-1805; email:
<a href="/cdn-cgi/l/email-protection#c5a1a4b3aca1ebafeba7a0b7a2a0b7aaab85a3a4a4eba2aab3"><span class="__cf_email__" data-cfemail="761217001f12581c5814130411130419183610171758111900">[email protected]</span></a>.
[[Page 11916]]
(l) 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 the AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) Emergency AD
2024-0218R1, dated December 19, 2024.
(ii) [Reserved]
(3) For EASA material identified in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 8999
000; email: <a href="/cdn-cgi/l/email-protection#cd8c89be8da8acbeace3a8b8bfa2bdace3a8b8"><span class="__cf_email__" data-cfemail="db9a9fa89bbebaa8baf5beaea9b4abbaf5beae">[email protected]</span></a>; website: easa.europa.eu. You may
find this material on the EASA website at ad.easa.europa.eu.
(4) You may view this material at the FAA, 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 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#ee889cc087809d9e8b8d9a878180ae808f9c8fc0898198"><span class="__cf_email__" data-cfemail="294f5b0740475a594c4a5d4046476947485b48074e465f">[email protected]</span></a>.
Issued on March 6, 2025.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2025-03983 Filed 3-12-25; 8:45 am]
BILLING CODE 4910-13-P
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