Published 2026-07-30 · Federal Register document 2026-15369
Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all Safran Helicopter Engines, S.A. (Safran) Model Arriel 2E engines. This AD was prompted by the determination that new or more restrictive airworthiness limitations are necessary. This AD requires revising the existing maintenance or inspection program to incorporate the airworthiness limitations section (ALS) of the existing approved aircraft maintenance program (AMP), as applicable. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-10-11T15:01:38.908778+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2026-346456b685abaa6b
- Source row
- results[202]
- Raw source SHA-256
- 346456b685abaa6b551902467a6384e655145a0a63f9cc15222fde6cb778bdfc
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2026-15-03
- Effective date printed in this edition
- 2026-09-03
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective September 3,
2026.
Exact source excerpt. Text positions 23183–23275, end exclusive, in the original decoded publication. SHA-256: b7951386aeea1f18624f2c9efbb22385d6c200ff2fe436b6c8dd56b7055fe8c9
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 23275–23304, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to all Safran Helicopter Engines, S.A. (type
certificate previously
[[Page 47946]]
held by Turbomeca S.A.) Model Arriel 2E engines.
Exact source excerpt. Text positions 23304–23479, end exclusive, in the original decoded publication. SHA-256: 481928bfd44b5aec779df3b7ab74b727e541dd1fa42763d769fe0eabdc5c64c1
Subject
(d) Subject
Joint Aircraft System Component (JASC) Code 7250, Turbine
Section.
Exact source excerpt. Text positions 23479–23565, end exclusive, in the original decoded publication. SHA-256: 0a22a80cf75c2450c6093c2ef5ee35332eb90935fd467639e0772a85d4a57974
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by the determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to prevent failure of life-limited parts. The unsafe
condition, if not addressed, could result in failure of one or more
engines, loss of thrust control, and consequent reduced control of
the helicopter.
Exact source excerpt. Text positions 23565–23940, end exclusive, in the original decoded publication. SHA-256: b08afc43a4fc83bc78a78fa1af88bbfc19147f9b87a86e12494a804bc8d25fca
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 23940–24042, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Required Actions
(g) Required Actions
(1) 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 AD
2025-0079, dated April 10, 2025 (EASA AD 2025-0079).
(2) The action required by paragraph (g)(1) of this AD may be
performed by the owner/operator (pilot) holding at least a private
pilot certificate and must be entered into the aircraft records
showing compliance with this AD in accordance with 14 CFR 43.9(a)
and 91.417(a)(2)(v). The record must be maintained as required by 14
CFR 91.417, 121.380, or 135.439.
Exact source excerpt. Text positions 24042–24693, end exclusive, in the original decoded publication. SHA-256: 8ca13987795f05b8059d069e713f92778797c2d2f14ca82149115921fecacacd
Exceptions to EASA AD 2025-0079
(h) Exceptions to EASA AD 2025-0079
(1) Where EASA AD 2025-0079 refers to its effective date, this
AD requires using the effective date of this AD.
(2) This AD does not require compliance with paragraphs (1),
(2), (4), and (5) of EASA AD 2025-0079.
(3) Where paragraph (3) of EASA AD 2025-0079 requires revising
the approved aircraft maintenance program (AMP) within 12 months
after the effective date of EASA AD 2025-0079, this AD requires
incorporating the actions and associated thresholds and intervals,
including life limits and maintenance tasks, into the existing
approved maintenance or inspection program, as applicable, within 90
days after the effective date of this AD.
(4) This AD does not adopt the ``Remarks'' section of EASA AD
2025-0079.
Exact source excerpt. Text positions 24693–25475, end exclusive, in the original decoded publication. SHA-256: 9450f00cfe7e3b5494a6c243db2afdb57b346800518aba83e4ec944f8effbcef
Provisions for Alternative Actions and Intervals
(i) Provisions for Alternative Actions and Intervals
After performing the actions required by paragraph (g) of this
AD, no alternative actions and associated thresholds and intervals,
including life limits, are allowed unless they are approved as
specified in the provisions of the ``Ref. Publications'' section of
EASA AD 2025-0079.
Exact source excerpt. Text positions 25475–25819, end exclusive, in the original decoded publication. SHA-256: e9957f332e45441789a3b154410c7b3a8336cf07897e01752dd879b44094e537
Alternative Methods of Compliance (AMOCs)
(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.
Exact source excerpt. Text positions 25819–26591, end exclusive, in the original decoded publication. SHA-256: 2a80f313ba24f7f406023983ccbbecce57b8ad70170ae7d6cc06ea4d2c02b045
Additional Information
(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:
[email protected].
Exact source excerpt. Text positions 26591–26819, end exclusive, in the original decoded publication. SHA-256: 78c6715c6b559b120c8a7f056cd9d2d21b8a65780878c006d700bd26e021da82
Material Incorporated by Reference
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) AD 2025-0079,
dated April 10, 2025.
(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: [email protected]; 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, 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 www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Exact source excerpt. Text positions 26819–28005, end exclusive, in the original decoded publication. SHA-256: e6d572e9e1eac9fd560d0ebd0d196c03787c9c0151f3de53425ae87c668699e3
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2026-15-03 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 5bf627b2bc053f3dc5ebbfd7d72bc894b44310dc258ceb42e950db8f92e66477. Source manifest: 5f5587bacf8eb3066de0b33e3042e9b865d94c43eee31fa4f104cc21edb522fe.
Official source · 2026-07-30
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 91, Number 145 (Thursday, July 30, 2026)]
[Rules and Regulations]
[Pages 47942-47946]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2026-15369]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-2557; Project Identifier MCAI-2025-00533-E;
Amendment 39-23415; AD 2026-15-03]
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.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Safran Helicopter Engines, S.A. (Safran) Model Arriel 2E engines. This
AD was prompted by the determination that new or more restrictive
airworthiness limitations are necessary. This AD requires revising the
existing maintenance or inspection program to incorporate the
airworthiness limitations section (ALS) of the existing approved
aircraft maintenance program (AMP), as applicable. The FAA is issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective September 3, 2026.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of September 3,
2026.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2025-2557; 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
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 European Union Aviation Safety Agency (EASA) material
identified in this AD, 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.
<bullet> You may view this material at the FAA, Airworthiness
Products Section,
[[Page 47943]]
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-2025-2557.
FOR FURTHER INFORMATION CONTACT: David Bergeron, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: (860) 386-1805; email: [email protected].
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 all Safran Model Arriel
2E engines. The NPRM was published in the Federal Register on September
26, 2025 (90 FR 46368). The NPRM was prompted by EASA AD 2025-0079,
dated April 10, 2025 (EASA AD 2025-0079) (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 new or more
restrictive airworthiness limitations have been developed, and the
restrictive limitations include replacing life-limited parts before
exceeding the applicable life limit, performing applicable maintenance
tasks, and revising the approved aircraft maintenance program.
In the NPRM, the FAA proposed to require revising the existing
maintenance or inspection program to incorporate the ALS of the
existing approved AMP, as applicable. The FAA is issuing this AD to
address the unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2025-2557.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from the Citizens Rulemaking Alliance.
The following presents the comments received on the NPRM and the FAA's
response to each comment.
Request To Issue an NPRM or Justify Forgoing Notice
The Citizens Rulemaking Alliance requested that the FAA either
provide its justification for finding good cause to bypass notice and
comment procedures or convert this action to an NPRM with a delayed 30-
day effective date. The commenter asserted the FAA has not adequately
justified use of the good cause exemption to bypass notice and comment
and the 30-day delayed effective date.
The FAA notes the comment was submitted in response to an NPRM for
which the FAA provided a 45-day comment period. This final rule is
effective 35 days after its publication in the Federal Register.
Therefore, the FAA did not change this AD as a result of this comment.
Request To Make Incorporation by Reference (IBR) Materials Reasonably
Available
The Citizens Rulemaking Alliance requested that the FAA make IBR
material available and free to the public during the comment period.
Alternatively, they requested that material be published in the Federal
Register. The commenter asserted that this AD incorporates by reference
manufacturer service information.
The FAA notes that this AD incorporates by reference EASA AD 2025-
0079, not the manufacturer service information referenced in that EASA
AD. The FAA posted EASA AD 2025-0079 to the AD docket when the NPRM was
published in the Federal Register. The material referenced in EASA AD
2025-0079 may only be posted before the final rule's publication if it
is already publicly available or if there is written consent from the
owner of that material. Additionally, the FAA provided notice in the
NPRM that the material referenced in EASA AD 2025-0079 will be
available in the AD docket after this AD is published. The FAA did not
change this AD as a result of this comment.
Request To Consider Impact on Small Entities
The Citizens Rulemaking Alliance requested that the FAA either
provide the factual basis for its Regulatory Flexibility Act (RFA)
certification that the AD will not have a significant economic impact
on a substantial number of small entities or prepare an initial
regulatory flexibility analysis.
FAA has considered the AD's impact on small businesses and provides
the following factual basis for its RFA certification.
The Regulatory Flexibility Act of 1980, Public Law 96-354, 94 Stat.
1164 (5 U.S.C. 601-612), as amended by the Small Business Regulatory
Enforcement Fairness Act of 1996 (Pub. L. 104-121, 110 Stat. 857, Mar.
29, 1996) and the Small Business Jobs Act of 2010 (Pub. L. 111-240, 124
Stat. 2504, Sept. 27, 2010), requires Federal agencies to consider the
effects of the regulatory action on small business and other small
entities and to minimize any significant economic impact. The term
``small entities'' comprises small businesses and not-for-profit
organizations that are independently owned and operated and are not
dominant in their fields, and governmental jurisdictions with
populations of less than 50,000.
Small Entities to Which This AD Applies
The FAA used the definition of small entities in the RFA for this
analysis. The RFA defines small entities as small businesses, small
governmental jurisdictions, or small organizations. In 5 U.S.C. 601(3),
the RFA defines ``small business'' to have the same meaning as ``small
business concern'' under section 3 of the Small Business Act. The Small
Business Act authorizes the Small Business Administration (SBA) to
define ``small business'' by issuing regulations.
The SBA has established size standards for various types of
economic activities, or industries, under the North American Industry
Classification System (NAICS). These size standards generally define
small businesses based on the number of employees or annual receipts.
The following table provides the SBA size standards for all industries
with at least one known entity impacted by this AD. Note that the SBA
definition of a small business applies to the parent company and all
affiliates as a single entity.
Small Business Size Standards
------------------------------------------------------------------------
NAICS code NAICS category Size standard
------------------------------------------------------------------------
221121........................ Electric Bulk Power 950 Employees.
Transmission and
Control.
221122........................ Electric Power 1,100 Employees.
Distribution.
481211........................ Nonscheduled Chartered 1,500 Employees.
Passenger Air
Transportation.
481212........................ Nonscheduled Chartered 1,500 Employees.
Freight Air
Transportation.
[[Page 47944]]
488190........................ Other Support $40,000,000.
Activities for Air
Transportation.
518210........................ Computing $40,000,000.
Infrastructure
Providers, Data
Processing, Web
Hosting, and Related
Services.
523910........................ Miscellaneous $47,000,000.
Intermediation.
531120........................ Lessors of $34,000,000.
Nonresidential
Buildings (except
Mini-warehouses).
531390........................ Other Activities $19,500,000.
Related to Real
Estate.
532411........................ Commercial Air, Rail, $45,500,000.
and Water
Transportation
Equipment Rental and
Leasing.
541611........................ Administrative $24,500,000.
Management and
General Management
Consulting Services.
551112........................ Offices of Other $45,500,000.
Holding Companies.
611512........................ Flight Training....... $34,000,000.
621910........................ Ambulance Services.... $22,500,000.
622110........................ General Medical and $47,000,000.
Surgical Hospitals.
921110........................ Law Enforcement....... 50,000
Population.
------------------------------------------------------------------------
To identify small entities, the FAA first identified the primary
NAICS of the entity or parent company, and then used data from
different sources (e.g., company annual reports, Bureau of
Transportation Statistics) to determine whether the entity meets the
applicable size standard. This AD affects 24 identifiable domestic
entities, of which 11 are small entities. The following table displays
the industries of the small entities, their average annual revenue, and
the AD's estimated cost burden relative to average annual revenue.
Number of Small Entities Affect by Industry and Cost Significance
----------------------------------------------------------------------------------------------------------------
Number of Cost per AD/
NAICS code Description affected small Average annual annual revenue
entities revenue (%)
----------------------------------------------------------------------------------------------------------------
481211............................. Nonscheduled Chartered 1 $428,180 0.02
Passenger Air
Transportation.
481211............................. Nonscheduled Chartered 1 15,290,000 0.00
Passenger Air
Transportation.
481212............................. Nonscheduled Chartered 1 12,510,000 0.00
Freight Air Transportation.
488190............................. Other Support Activities 1 4,690,000 0.00
for Air Transportation.
518210............................. Computing Infrastructure 1 137,080 0.06
Providers, Data
Processing, Web Hosting,
and Related Services.
531120............................. Lessors of Nonresidential 1 90,500 0.09
Buildings (except Mini-
warehouses).
531390............................. Other Activities Related to 1 151,760 0.06
Real Estate.
532411............................. Commercial Air, Rail, and 1 850,000 0.01
Water Transportation
Equipment Rental and
Leasing.
541611............................. Administrative Management 1 1,050,000 0.01
and General Management
Consulting Services.
611512............................. Flight Training............ 1 3,480,000 0.00
921110............................. Law Enforcement............ 1 143,650,000 0.00
----------------------------------------------------------------------------------------------------------------
RFA Conclusions
While FAA has determined that this final AD affects a substantial
number of identifiable small entities, the compliance cost of the AD
relative to each small entity's annual revenue is minimal. The FAA
estimates the total cost per affected entity to be $85 (1 work-hour x
$85 per work-hour), which is 0.02% of the average small entity's total
annual revenue. Therefore, as provided in section 605(b), the FAA
certifies this AD will not result in a significant economic impact on a
substantial number of small entities. The FAA did not change this AD as
a result of this comment.
Request To Comply With the Paperwork Reduction Act (PRA)
The Citizens Rulemaking Alliance requested that the FAA revise the
proposed AD to comply with the PRA if reporting is required. If
reporting is not required, the commenter requested the FAA clarify that
in the AD.
The FAA notes this AD does not require reporting. If an AD were to
require reporting, the preamble of the AD would include a paragraph
titled ``Paperwork Reduction Act'' that would provide the applicable
OMB control number, required PRA statements, and the estimated time to
collect the required information (burden). Any costs associated with
the reporting requirement would be included in the Costs of Compliance
section in the preamble of the AD. Therefore, the FAA did not change
this AD as a result of this comment.
Request To Consider Compliance Alternatives
The Citizens Rulemaking Alliance requested that, if the proposed AD
requires parts replacement or shop visits, the FAA adjust compliance
times or provide alternative method of compliance (AMOC) pathways to
reflect parts availability and maintenance capacity constraints, while
maintaining an appropriate margin of safety.
The FAA disagrees with the request. The FAA notes that this AD
requires revising the existing maintenance or inspection program, which
requires neither replacement parts nor a shop visit. Furthermore, AMOC
pathways already exist under the provisions of paragraph (j) of this
AD. The FAA will
[[Page 47945]]
consider requests for approval of an extension of the compliance time
or other AMOCs if sufficient data are submitted to substantiate that
the new compliance time or alternative method would provide an
acceptable level of safety. The commenter did not provide specific data
regarding parts availability or maintenance capacity constraints for
the FAA to consider. Therefore, the FAA did not change this AD as a
result of this comment.
Conclusion
These products have been approved by the civil 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, that authority has notified the FAA of the unsafe condition
described in the MCAI referenced above. The FAA reviewed the relevant
data, considered any comments received, and determined that air safety
requires adopting this AD as proposed. Accordingly, the FAA is issuing
this AD to address the unsafe condition on these products. 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.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed EASA AD 2025-0079, which specifies procedures for
replacing components before exceeding their life limits and
accomplishing all applicable maintenance tasks within thresholds and
intervals specified in the ALS as defined in EASA AD 2025-0079.
Depending on the results of the maintenance tasks, EASA AD 2025-0079
requires accomplishing corrective action(s) or contacting Safran
Helicopters for approved instructions and accomplishing those
instructions.
Additionally, EASA AD 2025-0079 specifies procedures for
accomplishing the actions specified in the applicable ALS, including
performing maintenance tasks, replacing life-limited parts, and
specifies procedures for revising the AMP by incorporating the
limitations, tasks, and associated thresholds and intervals described
in the specified ALS, as applicable. Revising the AMP constitutes
terminating action for the requirement to record accomplishment of the
actions of replacing components before exceeding their life limits and
accomplishing maintenance tasks within thresholds and intervals
specified in the applicable ALS as required by EASA AD 2025-0079 for
demonstration of AD compliance on a continued basis.
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.
Differences Between This AD and the MCAI
EASA AD 2025-0079 applies to Safran Model Arriel 2D, 2E, 2H, 2L2,
and 2N engines, whereas this AD applies to Safran Model Arriel 2E
engines. The ALS revisions required by this AD do not include Safran
Model Arriel 2D engines, and Safran Model Arriel 2H, 2L2, and 2N
engines do not have an FAA type certificate.
Costs of Compliance
The FAA estimates that this AD affects 136 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
----------------------------------------------------------------------------------------------------------------
Revise the ALS and the existing 1 work-hour x $85 per $0 $85 $11,560
approved AMP. 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,
(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:
2026-15-03 Safran Helicopter Engines, S.A. (Type Certificate
Previously Held by Turbomeca S.A.): Amendment 39-23415; Docket No.
FAA-2025-2557; Project Identifier MCAI-2025-00533-E.
(a) Effective Date
This airworthiness directive (AD) is effective September 3,
2026.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Safran Helicopter Engines, S.A. (type
certificate previously
[[Page 47946]]
held by Turbomeca S.A.) Model Arriel 2E engines.
(d) Subject
Joint Aircraft System Component (JASC) Code 7250, Turbine
Section.
(e) Unsafe Condition
This AD was prompted by the determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to prevent failure of life-limited parts. The unsafe
condition, if not addressed, could result in failure of one or more
engines, loss of thrust control, and consequent reduced control of
the helicopter.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) 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 AD
2025-0079, dated April 10, 2025 (EASA AD 2025-0079).
(2) The action required by paragraph (g)(1) of this AD may be
performed by the owner/operator (pilot) holding at least a private
pilot certificate and must be entered into the aircraft records
showing compliance with this AD in accordance with 14 CFR 43.9(a)
and 91.417(a)(2)(v). The record must be maintained as required by 14
CFR 91.417, 121.380, or 135.439.
(h) Exceptions to EASA AD 2025-0079
(1) Where EASA AD 2025-0079 refers to its effective date, this
AD requires using the effective date of this AD.
(2) This AD does not require compliance with paragraphs (1),
(2), (4), and (5) of EASA AD 2025-0079.
(3) Where paragraph (3) of EASA AD 2025-0079 requires revising
the approved aircraft maintenance program (AMP) within 12 months
after the effective date of EASA AD 2025-0079, this AD requires
incorporating the actions and associated thresholds and intervals,
including life limits and maintenance tasks, into the existing
approved maintenance or inspection program, as applicable, within 90
days after the effective date of this AD.
(4) This AD does not adopt the ``Remarks'' section of EASA AD
2025-0079.
(i) Provisions for Alternative Actions and Intervals
After performing the actions required by paragraph (g) of this
AD, no alternative actions and associated thresholds and intervals,
including life limits, are allowed unless they are approved as
specified in the provisions of the ``Ref. Publications'' section of
EASA AD 2025-0079.
(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 David Bergeron,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (860) 386-1805; email:
[email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) AD 2025-0079,
dated April 10, 2025.
(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: [email protected]; 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, 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 www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on July 14, 2026.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2026-15369 Filed 7-29-26; 8:45 am]
BILLING CODE 4910-13-P
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