Proposed Rule2025-13743
Airworthiness Directives; Airbus Helicopters
Primary source
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Published
July 22, 2025
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for certain Airbus Helicopters Model AS 350B2, AS 350B3, AS355N, AS355NP, and EC 130 B4 helicopters. This proposed AD was prompted by a report of a loss of cargo load during cargo swing operation on a helicopter due to an incorrect adjustment of the release cable of the cargo swing emergency release control. This proposed AD would require a one-time inspection of the cargo swing emergency release control and, depending on the results, corrective actions. 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 138 (Tuesday, July 22, 2025)</title>
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[Federal Register Volume 90, Number 138 (Tuesday, July 22, 2025)]
[Proposed Rules]
[Pages 34386-34388]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2025-13743]
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Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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Federal Register / Vol. 90, No. 138 / Tuesday, July 22, 2025 /
Proposed Rules
[[Page 34386]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-1363; Project Identifier MCAI-2025-00098-R]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Airbus Helicopters Model AS 350B2, AS 350B3, AS355N,
AS355NP, and EC 130 B4 helicopters. This proposed AD was prompted by a
report of a loss of cargo load during cargo swing operation on a
helicopter due to an incorrect adjustment of the release cable of the
cargo swing emergency release control. This proposed AD would require a
one-time inspection of the cargo swing emergency release control and,
depending on the results, corrective actions. The FAA is proposing this
AD to address the unsafe condition on these products.
DATES: The FAA must receive comments on this NPRM by September 5, 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-2025-1363; 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 European Union Aviation Safety Agency (EASA) material
identified in this proposed AD, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; phone: +49 221 8999 000; email:
<a href="/cdn-cgi/l/email-protection#5c1d182f1c393d2f3d7239292e332c3d723929"><span class="__cf_email__" data-cfemail="b5f4f1c6f5d0d4c6d49bd0c0c7dac5d49bd0c0">[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, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Parkway, Room 6N-
321, Fort Worth, TX 76177. For information on the availability of this
material at the FAA, call (817) 222-5110. It is also available at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2025-1363.
FOR FURTHER INFORMATION CONTACT: Steven Warwick, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: (817) 222-5225; email: <a href="/cdn-cgi/l/email-protection#6310170615060d4d114d140211140a0008230502024d040c15"><span class="__cf_email__" data-cfemail="582b2c3d2e3d36762a762f392a2f313b33183e3939763f372e">[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 using a method listed
under the ADDRESSES section. Include ``Docket No. FAA-2025-1363;
Project Identifier MCAI-2025-00098-R'' 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
Steven Warwick, 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
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2025-0025, dated January 23, 2025
(EASA AD 2025-0025) (also referred to as the MCAI), to correct an
unsafe condition on AS 350 B2, AS 350 B3, AS 355 NP, AS 355 N, and EC
130 B4 helicopters, all serial numbers, equipped with ONBOARD systems
3500LB, having part number (P/N) 704A41811035. The MCAI states a report
was received of a loss of cargo load during cargo swing operation on a
helicopter. Subsequent investigation revealed an incorrect adjustment
of the release cable of the cargo swing emergency release control.
The FAA is issuing this proposed AD to address the adjustment of
the cargo swing emergency release control. The unsafe condition, if not
addressed, could result in inflight loss of cargo load and injury to
persons on the ground.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2025-1363.
[[Page 34387]]
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed EASA AD 2025-0025, which specifies procedures for
a one-time inspection of the cargo swing emergency release control and,
depending on the results, corrective actions. Corrective actions
include adjustment of the cargo swing emergency release control or
replacement of the dropping control. 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 civil aviation authority
(CAA) 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 is issuing
this NPRM 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, as incorporated by reference, except
for any differences identified as exceptions in the regulatory text of
this AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some CAA ADs as the primary
source of information for compliance with requirements for
corresponding FAA ADs. The FAA has been coordinating this process with
manufacturers and CAAs. As a result, the FAA proposes to incorporate
EASA AD 2025-0025 by reference in the FAA final rule. This proposed AD
would, therefore, require compliance with EASA AD 2025-0025 in its
entirety through that incorporation, except for any differences
identified as exceptions in the regulatory text of this proposed AD.
Using common terms that are the same as the heading of a particular
section in EASA AD 2025-0025 does not mean that operators need comply
only with that section. For example, where the AD requirement refers to
``all required actions and compliance times,'' compliance with this AD
requirement is not limited to the section titled ``Required Action(s)
and Compliance Time(s)'' in EASA AD 2025-0025. Material required by
EASA AD 2025-0025 for compliance will be available at <a href="http://regulations.gov">regulations.gov</a>
under Docket No. FAA-2025-1363 after the FAA final rule is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 1,036 helicopters of U.S. registry. Labor rates are estimated at
$85 per work-hour. Based on these numbers, 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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Inspect cargo swing emergency release 1 work-hour x $85 per hour $0 $85 $88,060
control. = $85.
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The FAA estimates the following costs to do any necessary repairs
that would be required based on the results of the proposed inspection.
The agency has no way of determining the number of helicopters that
might need this repair:
On-Condition Costs
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Action Labor cost Parts cost Cost per product
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Adjust cargo swing emergency release control. 2 work-hours x $85 per hour = $0 $170
$170.
Replace dropping control..................... 1.5 work-hours x $85 per hour = 3,527 3,655
$128.
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The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected operators.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
[[Page 34388]]
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Airbus Helicopters: Docket No. FAA-2025-1363; Project Identifier
MCAI-2025-00098-R.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by September 5, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters Model AS 350B2, AS 350B3,
AS355N, AS355NP, and EC 130 B4 helicopters, certificated in any
category, as identified in European Union Aviation Safety Agency AD
2025-0025, dated January 23, 2025 (EASA AD 2025-0025).
(d) Subject
Joint Aircraft System Component (JASC) Code 2500, Cabin
Equipment/Furnishings.
(e) Unsafe Condition
This AD was prompted by a report of a loss of cargo load during
cargo swing operation on a helicopter due to an incorrect adjustment
of the release cable of the cargo swing emergency release control.
The FAA is issuing this AD to address the adjustment of the cargo
swing emergency release control. The unsafe condition, if not
addressed, could result in inflight loss of cargo load and injury to
persons on the ground.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
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 2025-0025.
(h) Exceptions to EASA AD 2025-0025
(1) Where EASA AD 2025-0025 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where EASA AD 2025-0025 refers to ``distance `B' '', this AD
requires replacing that text with ``distance `B', the distance
between the ball end and the manual release lever''.
(3) Where EASA AD 2025-0025 refers to ``distance `C' '', this AD
requires replacing that text with ``distance `C', the distance
between the ball end and the dropping control''.
(4) This AD does not adopt the Remarks section of EASA AD 2025-
0025.
(i) No Reporting Requirement
Although the material referenced in EASA AD 2025-0025 specifies
to submit certain information to the manufacturer, this AD does not
require that action.
(j) Special Flight Permits
Special flight permits may be issued in accordance with 14 CFR
21.197 and 21.199 to operate the helicopter to a location where the
actions of this AD can be accomplished provided that no external
load is carried in the cargo swing.
(k) 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 (l) of
this AD and email to: <a href="/cdn-cgi/l/email-protection#9ddcd0d2deddfbfcfcb3faf2eb"><span class="__cf_email__" data-cfemail="4f0e02000c0f292e2e61282039">[email protected]</span></a>.
(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.
(l) Additional Information
For more information about this AD, contact Steven Warwick,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (817) 222-5225; email:
<a href="/cdn-cgi/l/email-protection#a6d5d2c3d0c3c888d488d1c7d4d1cfc5cde6c0c7c788c1c9d0"><span class="__cf_email__" data-cfemail="27545342514249095509504655504e444c6741464609404851">[email protected]</span></a>.
(m) 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 2025-0025,
dated January 23, 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: <a href="/cdn-cgi/l/email-protection#4001043300252133216e2535322f30216e2535"><span class="__cf_email__" data-cfemail="3170754271545042501f5444435e41501f5444">[email protected]</span></a>; website: easa.europa.eu. You may
find the EASA material on the EASA website at ad.easa.europa.eu.
(4) You may view this material at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Parkway, Room 6N-
321, Fort Worth, TX 76177. 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#d6b0a4f8bfb8a5a6b3b5a2bfb9b896b8b7a4b7f8b1b9a0"><span class="__cf_email__" data-cfemail="2147530f484f5251444255484e4f614f4053400f464e57">[email protected]</span></a>.
Issued on July 17, 2025.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2025-13743 Filed 7-21-25; 8:45 am]
BILLING CODE 4910-13-P
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