Airworthiness Directives; Airbus Helicopters, 83437-83440 [2024-23796]
Download as PDF
83437
Proposed Rules
Federal Register
Vol. 89, No. 200
Wednesday, October 16, 2024
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.
column, correct the RIN to read: ‘‘0581–
AE31.’’
Melissa Bailey,
Associate Administrator, Agricultural
Marketing Service.
[FR Doc. 2024–23793 Filed 10–15–24; 8:45 am]
BILLING CODE P
DEPARTMENT OF AGRICULTURE
DEPARTMENT OF TRANSPORTATION
Agricultural Marketing Service
Federal Aviation Administration
7 CFR Part 800
14 CFR Part 39
[Doc. No. AMS–FGIS–24–0027]
[Docket No. FAA–2024–2332; Project
Identifier MCAI–2022–01479–R]
RIN 0581–AE31
RIN 2120–AA64
Formulas for Calculating Hourly and
Unit Fees for FGIS Services;
Correction
Airworthiness Directives; Airbus
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
Agricultural Marketing Service,
Department of Agriculture (USDA).
AGENCY:
Notice of proposed rulemaking;
correction.
ACTION:
The Agricultural Marketing
Service (AMS), Federal Grain Inspection
Service (FGIS or Service) published a
proposed rulemaking in the Federal
Register of October 8, 2024, concerning
amendments to its user fee regulations
to establish standardized formulas the
agency would use to calculate hourly
and unit fees. This document will
correct the Regulation Identifier Number
(RIN) used in the proposed rule.
SUMMARY:
Comments are due on or before
November 22, 2024.
DATES:
FOR FURTHER INFORMATION CONTACT:
Denise Ruggles, Executive Program
Analyst, USDA, AMS, FGIS, Telephone:
816–702–3897, Email:
Denise.M.Ruggles@usda.gov; or
Anthony Goodeman, Senior Policy
Advisor, USDA, AMS, FGIS, Telephone:
202–720–2091, Email:
Anthony.T.Goodeman@usda.gov.
lotter on DSK11XQN23PROD with PROPOSALS1
SUPPLEMENTARY INFORMATION:
Correction
In the proposed rulemaking FR Doc.
2024–23192, on page 81396 in the issue
of October 8, 2024, making the
following correction in the preamble
header. On page 81396, in the first
VerDate Sep<11>2014
16:01 Oct 15, 2024
Jkt 265001
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Airbus Helicopters Model
AS332C, AS332C1, AS332L, AS332L1,
AS332L2, AS355E, AS355F, AS355F1,
AS355F2, AS355N, AS355NP, AS–
365N2, AS 365 N3, EC 155B, EC155B1,
EC225LP, SA–365N, and SA–365N1
helicopters. This proposed AD was
prompted by a report of an
unintentional activation of the hoist
shear-button (shear-button) on the
collective pitch handle during a night
flight. This proposed AD would require
checking the operation of the shearbutton safety-cap on each applicable
collective pitch handle and prohibit
installing certain part-numbered
collective pitch handles or collective
sticks with those part-numbered
collective pitch handles installed unless
certain requirements are met. The FAA
is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments
on this NPRM by December 2, 2024.
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–
SUMMARY:
PO 00000
Frm 00001
Fmt 4702
Sfmt 4702
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–2024–2332; 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, any comments
received, and other information. The
street address for Docket Operations is
listed above.
Related Material: For Airbus
Helicopters material identified in this
AD, contact Airbus Helicopters, 2701
North Forum Drive, Grand Prairie, TX
75052; phone: (972) 641–0000 or (800)
232–0323; fax: (972) 641–3775; or at
airbus.com/en/products-services/
helicopters/hcare-services/airbusworld.
Dan
McCully, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (404) 474–
5548; email: william.mccully@faa.gov.
FOR FURTHER INFORMATION CONTACT:
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–2024–2332; Project Identifier
MCAI–2022–01479–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
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this NPRM.
E:\FR\FM\16OCP1.SGM
16OCP1
83438
Federal Register / Vol. 89, No. 200 / Wednesday, October 16, 2024 / Proposed Rules
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 Dan McCully,
Aviation Safety Engineer, FAA, 1600
Stewart Avenue, Suite 410, Westbury,
NY 11590; phone: (404) 474–5548;
email: william.mccully@faa.gov. Any
commentary that the FAA receives
which is not specifically designated as
CBI will be placed in the public docket
for this rulemaking.
lotter on DSK11XQN23PROD with PROPOSALS1
Background
The European Union Aviation Safety
Agency (EASA), which is the Technical
Agent for the Member States of the
European Union, has issued EASA AD
2022–0220, dated November 16, 2022
(EASA AD 2022–0020), to correct an
unsafe condition on Airbus Helicopters
Model AS 355 E, AS 355 F, AS 3555 F1,
AS 355 F2, AS 355 N, AS 355 NP, SA
365 N, SA 365 N1, AS 365 N2, AS 365
N3, EC 155 B, EC 155 B1, AS 332 C, AS
332 C1, AS 332 L, AS 332 L1, AS 332
L2, and EC 225 LP helicopters, all serial
numbers equipped with hoist provisions
(hoist fixed parts).
EASA AD 2022–0020 advises of a
report of an inadvertent activation of the
shear-button on a collective pitch
handle. EASA AD 2022–0020 states this
occurred during a night flight when the
pilot was turning on the headlight
adjacent to the shear-button, which is
protected by a safety-cap that is fitted
with a spring. Additionally, EASA AD
2022–0220 states that further
investigation determined aging of the
spring may have led to improper
functioning of the safety-cap.
Accordingly, EASA AD 2022–0220
requires accomplishing an operational
check of the shear-button safety-cap of
each applicable collective pitch handle
and, depending on the results, replacing
the spring or deferring replacement of
the spring by fabricating and installing
a placard prohibiting use of the hoist
VerDate Sep<11>2014
16:01 Oct 15, 2024
Jkt 265001
during night flights, informing all flight
crew, and operating the helicopter
accordingly. EASA AD 2022–0220 also
prohibits installing certain partnumbered collective pitch handles or
certain part-numbered collective sticks
with those part-numbered collective
pitch handles installed unless the
operational check and as applicable,
corrective action is done, or it is a new
collective pitch handle.
You may examine EASA AD 2022–
0220 in the AD docket at regulations.gov
under Docket No. FAA–2024–2332.
Related Material
The FAA reviewed Airbus Helicopters
Alert Service Bulletin (ASB) AS332–
25.03.97, Revision 0, dated October 4,
2022; Airbus Helicopters ASB AS355–
25.01.38, Revision 0, dated October 4,
2022; Airbus Helicopters ASB AS365–
25.01.91, Revision 1, dated November 3,
2022; Airbus Helicopters ASB EC155–
25A160, Revision 0, dated October 4,
2022; and Airbus Helicopters ASB
EC225–25A293, Revision 0, dated
October 4, 2022. This material specifies
procedures for inspecting the spring of
the shear-button safety-cap on the
collective pitch handle to determine
whether the safety-cap maintains either
in a fully closed or fully open position.
Depending on the results, this material
specifies procedures for replacing an
affected spring or attaching a label
(placard) to prohibit night flights.
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 its AD. The FAA is issuing
this NPRM after determining that the
unsafe condition described previously is
likely to exist or develop on other
products of these same type designs.
Proposed AD Requirements in This
NPRM
This proposed AD would require
checking the spring of the collective
pitch handle for correct positioning of
the shear-button safety-cap and,
depending on the results, replacing the
spring or deferring replacement of the
spring and installing a placard and
prohibiting night flying during the
deferment. The owner/operator (pilot)
holding at least a private pilot certificate
may perform the check and must enter
compliance with the applicable
paragraphs of the proposed AD into the
helicopter maintenance records in
accordance with 14 CFR 43.9(a) and
PO 00000
Frm 00002
Fmt 4702
Sfmt 4702
91.417(a)(2)(v). The pilot may perform
this check because it only involves
lifting the safety-cap and verifying
whether it automatically returns to an
intended position. This check could be
performed equally well by a pilot or a
mechanic. This is an exception to the
FAA’s standard maintenance
regulations.
This proposed AD would also
prohibit installing certain partnumbered collective pitch handles or
collective sticks with those partnumbered collective pitch handles
installed unless the operational check
and, as applicable, corrective action, is
done, or it is a new collective pitch
handle.
Differences Between This Proposed AD
and EASA AD 2022–0220
EASA AD 2022–0220 specifies a onetime inspection of the spring, whereas
this proposed AD would require
repetitively inspecting the spring at
intervals not to exceed 12 months timein-service.
EASA AD 2022–0220 allows deferring
replacement of a deficient spring
provided that a placard prohibiting use
of the hoist at night is installed, all
flight crew are informed and, thereafter,
that the helicopter is operated
accordingly, whereas this proposed AD
would not require informing any flight
crew. Compliance with such
requirements in an AD is impracticable
to demonstrate or track on an ongoing
basis; therefore, an AD requirement to
inform all flight crew is unenforceable.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 66
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.
Checking each safety-cap would take
1 work-hour for an estimated cost of up
to $85 per helicopter and $5,610 for the
U.S. fleet, per check cycle.
If required, replacing a spring would
take 1 work-hour and parts would cost
$25 for an estimated cost of $110 per
replacement.
Fabricating and installing a placard
would take 0.5 work-hour and parts
would cost $25 for an estimated cost of
$68 per helicopter.
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
E:\FR\FM\16OCP1.SGM
16OCP1
Federal Register / Vol. 89, No. 200 / Wednesday, October 16, 2024 / Proposed Rules
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
1. The authority citation for part 39
continues to read as follows:
■
lotter on DSK11XQN23PROD with PROPOSALS1
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Airbus Helicopters: Docket No. FAA–2024–
2332; Project Identifier MCAI–2022–
01479–R.
VerDate Sep<11>2014
16:01 Oct 15, 2024
Jkt 265001
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by December 2,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters
AS332C, AS332C1, AS332L, AS332L1,
AS332L2, AS355E, AS355F, AS355F1,
AS355F2, AS355N, AS355NP, AS–365N2,
AS 365 N3, EC 155B, EC155B1, EC225LP,
SA–365N, and SA–365N1 helicopters,
certificated in any category, with a collective
pitch handle installed on a pilot or co-pilot
collective stick having part number (P/N)
704A41–1100–42, 704A41–1100–50,
704A41–1100–56, 704A41–1100–57,
704A41–1100–60, 704A41–1100–67,
704A41–1100–68, 704A41–1100–97,
704A41–1100–98, 704A41–1100–99,
704A41–1101–14, 704A41–1101–30, or
704A41–1101–32, as applicable to your
model helicopter.
(d) Subject
Joint Aircraft System Component (JASC)
Code: 2510, Flight compartment equipment.
(e) Unsafe Condition
This AD was prompted by a report of an
unintentional activation of the hoist shearbutton on the collective pitch handle during
a night flight. The FAA is issuing this AD to
detect and address fatigue of the spring in the
hoist shear-button safety-cap on the left and
right collective pitch handles. The unsafe
condition, if not addressed, could result in an
unintended shearing of the hoist cable and
subsequent injury to the hoisted person.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
(1) For helicopters identified in paragraph
(c) of this AD that have a hoist installed,
within 50 hours time-in-service (TIS) after
the effective date of this AD, and thereafter
at intervals not to exceed 12 months TIS,
check the operation of the hoist shear-button
safety-cap on each applicable collective pitch
handle by accomplishing the actions required
by paragraphs (g)(1)(i) through (iii) of this
AD, as applicable. The owner/operator (pilot)
holding at least a private pilot certificate may
perform the checks required by paragraphs
(g)(1)(i) through (iii) of this AD and must
enter compliance with these paragraphs into
the helicopter maintenance records 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.
(i) Place your thumb under the safety-cap
and lift the safety-cap to a less-than halfway
position. Remove your thumb and verify that
the safety-cap goes to the fully open position
or that the safety-cap returns to the fully
closed position. Repeat these actions no less
than two more times. If the safety-cap stays
in the less-than halfway position, or the
safety-cap does not fully close or fully open
PO 00000
Frm 00003
Fmt 4702
Sfmt 4702
83439
during any instance of the actions required
by this paragraph, before further flight, a
person authorized under 14 CFR 43.3 must
accomplish the actions required by paragraph
(g)(2) of this AD.
(ii) Place your thumb under the safety-cap
and lift the safety-cap to a halfway position.
Remove your thumb and verify that the
safety-cap goes to the fully open position or
that the safety-cap returns to the fully closed
position. Repeat these actions no less than
two more times. If the safety-cap stays in the
halfway position, or the safety-cap does not
fully close or fully open during any instance
of the actions required by this paragraph,
before further flight, a person authorized
under 14 CFR 43.3 must accomplish the
actions required by paragraph (g)(2) of this
AD.
(iii) Place your thumb under the safety-cap
and lift the safety-cap to a more-than halfway
position. Remove your thumb and verify the
safety-cap goes to the fully open position or
that the safety-cap returns to the fully closed
position. Repeat these actions no less than
two more times. If the safety-cap stays in the
more-than halfway position, or the safety-cap
does not fully close or fully open during any
instance of the actions required by this
paragraph, before further flight, a person
authorized under 14 CFR 43.3 must
accomplish the actions required by paragraph
(g)(2) of this AD.
(2) If the safety-cap stays in the less-than
halfway, halfway, or more-than halfway
position, or the safety-cap does not fully
close or fully open during any of instance of
the actions required by paragraphs (g)(1)(i)
through (iii) of this AD, before further flight,
remove the spring from service and replace
it with an airworthy spring.
(3) As an alternative to replacing the spring
as required by paragraph (g)(2) of this AD,
accomplish the actions required by
paragraphs (g)(3)(i) and (ii) of this AD.
(i) Before further flight, fabricate a placard
with a font size greater than or equal to 4 mm
(.157 in), stating the following: ‘‘NIGHT
HOIST OPERATIONS PROHIBITED’’. The
placard must have a red background with
white font color or a white background with
red font color. The placard must not be
erasable and must be attached to the
instrument panel, visible to the pilot and copilot.
(ii) Within 150 hours TIS after
accomplishing the actions required by
paragraph (g)(3)(i) of this AD, remove the
spring of the safety-cap from service and
replace it with an airworthy spring, and
remove the placard from service.
(4) For helicopters identified in paragraph
(c) of this AD that do not have a hoist
installed, before installation of a hoist’s
removable parts on the helicopter,
accomplish the check and as applicable,
corrective action, required by paragraphs
(g)(1) through (3) of this AD.
(h) Parts Installation Limitations
As of the effective date of this AD, do not
install on any helicopter a collective pitch
handle having a P/N identified in paragraph
(c) of this AD, or any pilot or co-pilot
collective stick with a collective pitch handle
having a P/N identified in paragraph (c) of
E:\FR\FM\16OCP1.SGM
16OCP1
83440
Federal Register / Vol. 89, No. 200 / Wednesday, October 16, 2024 / Proposed Rules
this AD installed, unless the check and as
applicable, corrective action, required by
paragraphs (g)(1) and (2) of this AD have
been done or the collective pitch handle is
new (zero total hours TIS).
(i) 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 (j) of this AD.
Information may be emailed to: 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.
(j) Related Information
For more information about this AD,
contact Dan McCully, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; phone: (404) 474–
5548; email: william.mccully@faa.gov.
(k) Material Incorporated by Reference
None.
Issued on October 9, 2024.
Steven W. Thompson,
Acting Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2024–23796 Filed 10–15–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF COMMERCE
National Oceanic and Atmospheric
Administration
50 CFR Part 648
[Docket No. 241009–0267]
RTID 0648–XE226
Fisheries of the Northeastern United
States; 2025 Specifications for the
Summer Flounder, Scup, Black Sea
Bass, and Bluefish Fisheries
National Marine Fisheries
Service (NMFS), National Oceanic and
Atmospheric Administration (NOAA),
Commerce.
ACTION: Proposed rule; request for
comments.
lotter on DSK11XQN23PROD with PROPOSALS1
AGENCY:
NMFS proposes 2025
specifications for the summer flounder,
scup, black sea bass, and bluefish
fisheries. The implementing regulations
for the Summer Flounder, Scup, and
Black Sea Bass Fishery Management
SUMMARY:
VerDate Sep<11>2014
16:01 Oct 15, 2024
Jkt 265001
Plan and the Bluefish Fishery
Management Plan require us to publish
specifications for the upcoming fishing
year for each of these species and to
provide an opportunity for public
comment. The proposed specifications
establish allowable harvest levels for
these species that will prevent
overfishing, consistent with the most
recent scientific information.
Comments must be received on
or before October 31, 2024.
DATES:
A plain language summary
of this proposed rule is available at
https://www.regulations.gov/docket/
NOAA-NMFS-2024-0117. You may
submit comments on this document,
identified by NOAA–NMFS–2024–0117,
by the following method:
• Electronic Submission: Submit all
electronic public comments via the
Federal e-Rulemaking Portal. Visit
https://www.regulations.gov and type
NOAA–NMFS–2024–0117 in the Search
box. Click on the ‘‘Comment’’ icon,
complete the required fields, and enter
or attach your comments.
Instructions: Comments sent by any
other method, to any other address or
individual, or received after the end of
the comment period, may not be
considered by NMFS. All comments
received are a part of the public record
and will generally be posted for public
viewing on https://www.regulations.gov
without change. All personal identifying
information (e.g., name, address, etc.),
confidential business information, or
otherwise sensitive information
submitted voluntarily by the sender will
be publicly accessible. NMFS will
accept anonymous comments (enter ‘‘N/
A’’ in the required fields if you wish to
remain anonymous).
A Supplemental Information Report
(SIR) was prepared for the 2025 black
sea bass specifications. Environmental
Assessments (EA) were prepared for the
2024 and projected 2025 summer
flounder and scup specifications and
2024 and projected 2025 bluefish
specifications. Copies of the EAs are
available on request from Dr.
Christopher M. Moore, Executive
Director, Mid-Atlantic Fishery
Management Council, Suite 201, 800
North State Street, Dover, DE 19901.
The EAs are also accessible via the
internet at https://www.mafmc.org/
supporting-documents.
ADDRESSES:
FOR FURTHER INFORMATION CONTACT:
Emily Keiley, Fishery Policy Analyst,
(978) 281–9116, or emily.keiley@
noaa.gov.
SUPPLEMENTARY INFORMATION:
PO 00000
Frm 00004
Fmt 4702
Sfmt 4702
General Background
The Mid-Atlantic Fishery
Management Council (Council) and the
Atlantic States Marine Fisheries
Commission (Commission)
cooperatively develop management
measures for the summer flounder,
scup, black sea bass, and bluefish
fisheries. The Council, pursuant to the
Magnuson-Stevens Fishery
Conservation and Management Act
(Magnuson-Stevens Act) develops
recommendations regarding fisheries in
Federal waters seaward of New York,
New Jersey, Delaware, Pennsylvania,
Maryland, Virginia, and North Carolina.
The Commission, pursuant to the
Atlantic Coastal Fisheries Cooperative
Management Act, addresses fisheries in
state waters from Florida to Maine.
These bodies work together in the
development of complementary fishery
management plans (FMP) for species
like summer flounder, scup, black sea
bass, and bluefish that are harvested in
both Federal and state waters, and each
year these bodies work together to
develop specifications for these
fisheries. The Council provides its
recommendations to NMFS, and NMFS
engages in a Federal rulemaking process
by which the agency adopts
specifications that become binding on
the Federal fisheries. Specifications in
these fisheries include various catch
and landing subdivisions, such as the
commercial and recreational sector
annual catch limits (ACL), annual catch
targets (ACT), and sector-specific
landing limits (i.e., the commercial
fishery quota and recreational harvest
limit (RHL)) established for 1 to 3 years
at a time. Adjustments to commercial
management measures are also
considered in the specifications process.
The process for measures used to
manage the recreational fisheries (i.e.,
minimum fish sizes, seasonal closures,
and possession restrictions) for these
four species occurs separately and is not
discussed further in this proposed rule.
The Summer Flounder, Scup, and
Black Sea Bass FMP and the Bluefish
FMP and their implementing
regulations establish the process for
establishing specifications for each of
those four species. All requirements of
the Magnuson-Stevens Act, including
the 10 national standards, also apply to
specifications. The FMPs also contain
formulas to divide the catch limits into
commercial and recreational fishery
allocations, state-by-state quotas, and
quota periods, depending on the species
in question. This proposed rule outlines
the application of the existing allocation
provisions for each species and provides
E:\FR\FM\16OCP1.SGM
16OCP1
Agencies
[Federal Register Volume 89, Number 200 (Wednesday, October 16, 2024)]
[Proposed Rules]
[Pages 83437-83440]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-23796]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2332; Project Identifier MCAI-2022-01479-R]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1,
AS332L2, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS-365N2,
AS 365 N3, EC 155B, EC155B1, EC225LP, SA-365N, and SA-365N1
helicopters. This proposed AD was prompted by a report of an
unintentional activation of the hoist shear-button (shear-button) on
the collective pitch handle during a night flight. This proposed AD
would require checking the operation of the shear-button safety-cap on
each applicable collective pitch handle and prohibit installing certain
part-numbered collective pitch handles or collective sticks with those
part-numbered collective pitch handles installed unless certain
requirements are met. The FAA is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments on this NPRM by December 2, 2024.
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-2024-2332; 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, any comments received, and other
information. The street address for Docket Operations is listed above.
Related Material: For Airbus Helicopters material identified in
this AD, contact Airbus Helicopters, 2701 North Forum Drive, Grand
Prairie, TX 75052; phone: (972) 641-0000 or (800) 232-0323; fax: (972)
641-3775; or at airbus.com/en/products-services/helicopters/hcare-services/airbusworld.
FOR FURTHER INFORMATION CONTACT: Dan McCully, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (404)
474-5548; email: [email protected].
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-2024-2332; Project Identifier
MCAI-2022-01479-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
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
[[Page 83438]]
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 Dan
McCully, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (404) 474-5548; email:
[email protected]. 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 European Union Aviation Safety Agency (EASA), which is the
Technical Agent for the Member States of the European Union, has issued
EASA AD 2022-0220, dated November 16, 2022 (EASA AD 2022-0020), to
correct an unsafe condition on Airbus Helicopters Model AS 355 E, AS
355 F, AS 3555 F1, AS 355 F2, AS 355 N, AS 355 NP, SA 365 N, SA 365 N1,
AS 365 N2, AS 365 N3, EC 155 B, EC 155 B1, AS 332 C, AS 332 C1, AS 332
L, AS 332 L1, AS 332 L2, and EC 225 LP helicopters, all serial numbers
equipped with hoist provisions (hoist fixed parts).
EASA AD 2022-0020 advises of a report of an inadvertent activation
of the shear-button on a collective pitch handle. EASA AD 2022-0020
states this occurred during a night flight when the pilot was turning
on the headlight adjacent to the shear-button, which is protected by a
safety-cap that is fitted with a spring. Additionally, EASA AD 2022-
0220 states that further investigation determined aging of the spring
may have led to improper functioning of the safety-cap.
Accordingly, EASA AD 2022-0220 requires accomplishing an
operational check of the shear-button safety-cap of each applicable
collective pitch handle and, depending on the results, replacing the
spring or deferring replacement of the spring by fabricating and
installing a placard prohibiting use of the hoist during night flights,
informing all flight crew, and operating the helicopter accordingly.
EASA AD 2022-0220 also prohibits installing certain part-numbered
collective pitch handles or certain part-numbered collective sticks
with those part-numbered collective pitch handles installed unless the
operational check and as applicable, corrective action is done, or it
is a new collective pitch handle.
You may examine EASA AD 2022-0220 in the AD docket at
regulations.gov under Docket No. FAA-2024-2332.
Related Material
The FAA reviewed Airbus Helicopters Alert Service Bulletin (ASB)
AS332-25.03.97, Revision 0, dated October 4, 2022; Airbus Helicopters
ASB AS355-25.01.38, Revision 0, dated October 4, 2022; Airbus
Helicopters ASB AS365-25.01.91, Revision 1, dated November 3, 2022;
Airbus Helicopters ASB EC155-25A160, Revision 0, dated October 4, 2022;
and Airbus Helicopters ASB EC225-25A293, Revision 0, dated October 4,
2022. This material specifies procedures for inspecting the spring of
the shear-button safety-cap on the collective pitch handle to determine
whether the safety-cap maintains either in a fully closed or fully open
position. Depending on the results, this material specifies procedures
for replacing an affected spring or attaching a label (placard) to
prohibit night flights.
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
its AD. The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of these same type designs.
Proposed AD Requirements in This NPRM
This proposed AD would require checking the spring of the
collective pitch handle for correct positioning of the shear-button
safety-cap and, depending on the results, replacing the spring or
deferring replacement of the spring and installing a placard and
prohibiting night flying during the deferment. The owner/operator
(pilot) holding at least a private pilot certificate may perform the
check and must enter compliance with the applicable paragraphs of the
proposed AD into the helicopter maintenance records in accordance with
14 CFR 43.9(a) and 91.417(a)(2)(v). The pilot may perform this check
because it only involves lifting the safety-cap and verifying whether
it automatically returns to an intended position. This check could be
performed equally well by a pilot or a mechanic. This is an exception
to the FAA's standard maintenance regulations.
This proposed AD would also prohibit installing certain part-
numbered collective pitch handles or collective sticks with those part-
numbered collective pitch handles installed unless the operational
check and, as applicable, corrective action, is done, or it is a new
collective pitch handle.
Differences Between This Proposed AD and EASA AD 2022-0220
EASA AD 2022-0220 specifies a one-time inspection of the spring,
whereas this proposed AD would require repetitively inspecting the
spring at intervals not to exceed 12 months time-in-service.
EASA AD 2022-0220 allows deferring replacement of a deficient
spring provided that a placard prohibiting use of the hoist at night is
installed, all flight crew are informed and, thereafter, that the
helicopter is operated accordingly, whereas this proposed AD would not
require informing any flight crew. Compliance with such requirements in
an AD is impracticable to demonstrate or track on an ongoing basis;
therefore, an AD requirement to inform all flight crew is
unenforceable.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 66 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.
Checking each safety-cap would take 1 work-hour for an estimated
cost of up to $85 per helicopter and $5,610 for the U.S. fleet, per
check cycle.
If required, replacing a spring would take 1 work-hour and parts
would cost $25 for an estimated cost of $110 per replacement.
Fabricating and installing a placard would take 0.5 work-hour and
parts would cost $25 for an estimated cost of $68 per helicopter.
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
[[Page 83439]]
detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Airbus Helicopters: Docket No. FAA-2024-2332; Project Identifier
MCAI-2022-01479-R.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by December 2, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters AS332C, AS332C1, AS332L,
AS332L1, AS332L2, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP,
AS-365N2, AS 365 N3, EC 155B, EC155B1, EC225LP, SA-365N, and SA-
365N1 helicopters, certificated in any category, with a collective
pitch handle installed on a pilot or co-pilot collective stick
having part number (P/N) 704A41-1100-42, 704A41-1100-50, 704A41-
1100-56, 704A41-1100-57, 704A41-1100-60, 704A41-1100-67, 704A41-
1100-68, 704A41-1100-97, 704A41-1100-98, 704A41-1100-99, 704A41-
1101-14, 704A41-1101-30, or 704A41-1101-32, as applicable to your
model helicopter.
(d) Subject
Joint Aircraft System Component (JASC) Code: 2510, Flight
compartment equipment.
(e) Unsafe Condition
This AD was prompted by a report of an unintentional activation
of the hoist shear-button on the collective pitch handle during a
night flight. The FAA is issuing this AD to detect and address
fatigue of the spring in the hoist shear-button safety-cap on the
left and right collective pitch handles. The unsafe condition, if
not addressed, could result in an unintended shearing of the hoist
cable and subsequent injury to the hoisted person.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
(1) For helicopters identified in paragraph (c) of this AD that
have a hoist installed, within 50 hours time-in-service (TIS) after
the effective date of this AD, and thereafter at intervals not to
exceed 12 months TIS, check the operation of the hoist shear-button
safety-cap on each applicable collective pitch handle by
accomplishing the actions required by paragraphs (g)(1)(i) through
(iii) of this AD, as applicable. The owner/operator (pilot) holding
at least a private pilot certificate may perform the checks required
by paragraphs (g)(1)(i) through (iii) of this AD and must enter
compliance with these paragraphs into the helicopter maintenance
records 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.
(i) Place your thumb under the safety-cap and lift the safety-
cap to a less-than halfway position. Remove your thumb and verify
that the safety-cap goes to the fully open position or that the
safety-cap returns to the fully closed position. Repeat these
actions no less than two more times. If the safety-cap stays in the
less-than halfway position, or the safety-cap does not fully close
or fully open during any instance of the actions required by this
paragraph, before further flight, a person authorized under 14 CFR
43.3 must accomplish the actions required by paragraph (g)(2) of
this AD.
(ii) Place your thumb under the safety-cap and lift the safety-
cap to a halfway position. Remove your thumb and verify that the
safety-cap goes to the fully open position or that the safety-cap
returns to the fully closed position. Repeat these actions no less
than two more times. If the safety-cap stays in the halfway
position, or the safety-cap does not fully close or fully open
during any instance of the actions required by this paragraph,
before further flight, a person authorized under 14 CFR 43.3 must
accomplish the actions required by paragraph (g)(2) of this AD.
(iii) Place your thumb under the safety-cap and lift the safety-
cap to a more-than halfway position. Remove your thumb and verify
the safety-cap goes to the fully open position or that the safety-
cap returns to the fully closed position. Repeat these actions no
less than two more times. If the safety-cap stays in the more-than
halfway position, or the safety-cap does not fully close or fully
open during any instance of the actions required by this paragraph,
before further flight, a person authorized under 14 CFR 43.3 must
accomplish the actions required by paragraph (g)(2) of this AD.
(2) If the safety-cap stays in the less-than halfway, halfway,
or more-than halfway position, or the safety-cap does not fully
close or fully open during any of instance of the actions required
by paragraphs (g)(1)(i) through (iii) of this AD, before further
flight, remove the spring from service and replace it with an
airworthy spring.
(3) As an alternative to replacing the spring as required by
paragraph (g)(2) of this AD, accomplish the actions required by
paragraphs (g)(3)(i) and (ii) of this AD.
(i) Before further flight, fabricate a placard with a font size
greater than or equal to 4 mm (.157 in), stating the following:
``NIGHT HOIST OPERATIONS PROHIBITED''. The placard must have a red
background with white font color or a white background with red font
color. The placard must not be erasable and must be attached to the
instrument panel, visible to the pilot and co-pilot.
(ii) Within 150 hours TIS after accomplishing the actions
required by paragraph (g)(3)(i) of this AD, remove the spring of the
safety-cap from service and replace it with an airworthy spring, and
remove the placard from service.
(4) For helicopters identified in paragraph (c) of this AD that
do not have a hoist installed, before installation of a hoist's
removable parts on the helicopter, accomplish the check and as
applicable, corrective action, required by paragraphs (g)(1) through
(3) of this AD.
(h) Parts Installation Limitations
As of the effective date of this AD, do not install on any
helicopter a collective pitch handle having a P/N identified in
paragraph (c) of this AD, or any pilot or co-pilot collective stick
with a collective pitch handle having a P/N identified in paragraph
(c) of
[[Page 83440]]
this AD installed, unless the check and as applicable, corrective
action, required by paragraphs (g)(1) and (2) of this AD have been
done or the collective pitch handle is new (zero total hours TIS).
(i) 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 (j) of
this AD. Information may be emailed 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.
(j) Related Information
For more information about this AD, contact Dan McCully,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: (404) 474-5548; email:
[email protected].
(k) Material Incorporated by Reference
None.
Issued on October 9, 2024.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-23796 Filed 10-15-24; 8:45 am]
BILLING CODE 4910-13-P