Airworthiness Directives; Airbus Helicopters, 11718-11720 [2024-03137]
Download as PDF
11718
Federal Register / Vol. 89, No. 32 / Thursday, February 15, 2024 / Rules and Regulations
Issued on January 26, 2024.
Michael Linegang,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–03082 Filed 2–14–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–0039; Project
Identifier MCAI–2023–00966–R; Amendment
39–22665; AD 2024–02–01]
RIN 2120–AA64
Airworthiness Directives; Airbus
Helicopters
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Airbus Helicopters Model EC225LP
helicopters. This AD was prompted by
a report of incorrect door opening
instructions on the placards located on
the right hand (RH) side of the VIP flap
door. This AD requires installing a
placard specifying jettisoning
instructions, as specified in a European
Union Aviation Safety Agency (EASA)
AD, which is incorporated by reference.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective March 1,
2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of March 1, 2024.
The FAA must receive comments on
this AD by April 1, 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–2024–0039; or in person at
khammond on DSKJM1Z7X2PROD with RULES
SUMMARY:
VerDate Sep<11>2014
16:35 Feb 14, 2024
Jkt 262001
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this final rule, the EASA AD,
any comments received, and other
information. The street address for
Docket Operations is listed above.
Material Incorporated by Reference:
• For EASA material incorporated by
reference in this final rule, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu.
You may find this material on the EASA
website at https://ad.easa.europa.eu.
• You may view this material at the
FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood
Pkwy., Room 6N–321, Fort Worth, TX
76177. For information on the
availability of this material at the FAA,
call (817) 222–5110. The EASA material
is also available at regulations.gov under
Docket No. FAA–2024–0039.
Other Related Service Information:
For Airbus Helicopters service
information identified in this final rule,
contact Airbus Helicopters, 2701 North
Forum Drive, Grand Prairie, TX 75052;
telephone (972) 641–0000 or (800) 232–
0323; fax (972) 641–3775; or at
airbus.com/en/products-services/
helicopters/hcare-services/airbusworld.
You may also view this service
information at the FAA contact
information under Material
Incorporated by Reference above.
FOR FURTHER INFORMATION CONTACT:
William McCully, Aviation Safety
Engineer, FAA, International Validation
Branch, FAA, 1600 Stewart Ave., Suite
410, Westbury, NY 11590; phone (404)
474–5548; email william.mccully@
faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written data, views, or arguments about
this final rule. Send your comments to
an address listed under ADDRESSES.
Include ‘‘Docket No. FAA–2024–0039;
Project Identifier MCAI–2023–00966–R’’
at the beginning of your comments. The
most helpful comments reference a
specific portion of the final rule, explain
the reason for any recommended
change, and include supporting data.
The FAA will consider all comments
received by the closing date and may
amend this final rule because of those
comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
regulations.gov, including any personal
information you provide. The agency
will also post a report summarizing each
substantive verbal contact received
about this final rule.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this AD contain
commercial or financial information
that is customarily treated as private,
that you actually treat as private, and
that is relevant or responsive to this AD,
it is important that you clearly designate
the submitted comments as CBI. Please
mark each page of your submission
containing CBI as ‘‘PROPIN.’’ The FAA
will treat such marked submissions as
confidential under the FOIA, and they
will not be placed in the public docket
of this AD. Submissions containing CBI
should be sent to William McCully,
Aviation Safety Engineer, FAA,
International Validation Branch, FAA,
1600 Stewart Ave., 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.
Background
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA AD 2022–0072,
dated April 26, 2022 (EASA AD 2022–
0072), to correct an unsafe condition on
Airbus Helicopters Model EC 225 LP
helicopters, serial numbers 2650, 2651,
2653, 2684, 2712, and 2796.
This AD was prompted by a report
that placards located on the RH side of
the VIP flap door of the passenger cabin
do not provide adequate door opening
instructions necessary to operate the RH
side VIP flap door in case of the
helicopter ditching. The unsafe
condition, if not addressed, could
prevent jettisoning of the RH side VIP
flap door during an emergency
situation, possibly obstructing
evacuation and resulting in injury to
occupants.
You may examine the EASA AD in
the AD docket at regulations.gov under
Docket No. FAA–2024–0039.
Related Service Information Under 1
CFR Part 51
EASA AD 2022–0072 requires
installing a placard over the current
placard, which correctly specifies
E:\FR\FM\15FER1.SGM
15FER1
Federal Register / Vol. 89, No. 32 / Thursday, February 15, 2024 / Rules and Regulations
jettisoning instructions for the RH side
of the VIP flap door.
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 ADDRESSES.
Other Related Service Information
The FAA reviewed Airbus Helicopters
Alert Service Bulletin (ASB) No. EC225–
52A023, Revision 0, dated January 22,
2020 for Model EC225LP helicopters.
This service information specifies
instructions for covering the existing
incorrect placard with a correct placard,
and reporting certain information to the
manufacturer.
FAA’s Determination
These helicopters have been approved
by EASA and are approved for operation
in the United States. Pursuant to the
FAA’s bilateral agreement with the
European Union, EASA has notified the
FAA about the unsafe condition
described in its AD. The FAA is issuing
this AD after evaluating all known
relevant information and determining
that the unsafe condition described
previously is likely to exist or develop
on other helicopters of the same type
design.
khammond on DSKJM1Z7X2PROD with RULES
AD Requirements
This AD requires accomplishing the
actions specified in EASA AD 2022–
0072, described previously, as
incorporated by reference, except for
any differences identified as exceptions
in the regulatory text of this AD and
except as discussed under ‘‘Differences
Between this AD and the EASA 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 civil aviation authority (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, EASA AD 2022–0072
will be incorporated by reference in this
FAA final rule. This AD would,
therefore, require compliance with
EASA AD 2022–0072 in its entirety
through that incorporation, except for
any differences identified as exceptions
in the regulatory text of this AD. Using
common terms that are the same as the
heading of a particular section in EASA
AD 2022–0072 does not mean that
operators need comply only with that
section. For example, where the AD
requirement refers to ‘‘all required
VerDate Sep<11>2014
16:35 Feb 14, 2024
Jkt 262001
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 2022–0072.
Service information referenced in EASA
AD 2022–0072 for compliance will be
available at regulations.gov under
Docket No. FAA–2024–0039.
Differences Between This AD and the
EASA AD
Service information referenced in
EASA AD 2022–0072 specified
reporting certain information to Airbus
Helicopters, including sending pictures,
whereas this AD does not require
reporting any information or sending
any pictures.
Justification for Immediate Adoption
and Determination of the Effective Date
Section 553(b)(3)(B) of the
Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies
to dispense with notice and comment
procedures for rules when the agency,
for ‘‘good cause,’’ finds that those
procedures are ‘‘impracticable,
unnecessary, or contrary to the public
interest.’’ Under this section, an agency,
upon finding good cause, may issue a
final rule without providing notice and
seeking comment prior to issuance.
Further, section 553(d) of the APA
authorizes agencies to make rules
effective in less than thirty days, upon
a finding of good cause.
There are currently no domestic
operators of these products.
Accordingly, notice and opportunity for
prior public comment are unnecessary,
pursuant to 5 U.S.C. 553(b)(3)(B). In
addition, for the foregoing reasons, the
FAA finds that good cause exists
pursuant to 5 U.S.C. 553(d) for making
this amendment effective in less than 30
days.
Regulatory Flexibility Act
The requirements of the Regulatory
Flexibility Act (RFA) do not apply when
an agency finds good cause pursuant to
5 U.S.C. 553 to adopt a rule without
prior notice and comment. Because the
FAA has determined that it has good
cause to adopt this rule without prior
notice and comment, RFA analysis is
not required.
11719
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
and
(2) Will not affect intrastate aviation
in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
Costs of Compliance
There are no costs of compliance with
this AD because there are no helicopters
with this type certificate on the U.S.
Registry.
2024–02–01 Airbus Helicopters:
Amendment 39–22665; Docket No.
FAA–2024–0039; Project Identifier
MCAI–2023–00966–R.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
(a) Effective Date
This airworthiness directive (AD) is
effective March 1, 2024.
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
E:\FR\FM\15FER1.SGM
15FER1
11720
Federal Register / Vol. 89, No. 32 / Thursday, February 15, 2024 / Rules and Regulations
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters
Model EC225LP helicopters, serial numbers
2650, 2651, 2653, 2684, 2712, and 2796,
certificated in any category.
(d) Subject
Joint Aircraft System Component (JASC)
Code: 5210, Passenger crew doors.
(e) Unsafe Condition
This AD was prompted by a report of
incorrect door opening instructions on the
placard located on the right-hand (RH) side
of the VIP flap door. The FAA is issuing this
AD to address and correct placards on the RH
side VIP flap door. The unsafe condition, if
not addressed, could prevent jettisoning of
the RH side VIP flap door during an
emergency situation, possibly obstructing
evacuation and resulting in injury to
occupants.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Except as specified in paragraphs (h) and
(i) of this AD: Comply with all required
actions and compliance times specified in,
and in accordance with, European Union
Aviation Safety Agency (EASA) AD 2022–
0072, dated April 26, 2022 (EASA AD 2022–
0072).
(h) Exceptions to EASA AD 2022–0072
(1) Where EASA AD 2022–0072 refers to its
effective date, this AD requires using the
effective date of this AD.
(2) Where EASA AD 2022–0072 refers to
flight hours, this AD requires using hours
time-in-service.
(3) Where the paragraph defined as placard
installation in EASA AD 2022–0072 states
‘‘in accordance with the instructions of the
ASB,’’ for this AD, replace that text with ‘‘in
accordance with the Accomplishment
Instructions, paragraph 3.B of the ASB.’’
khammond on DSKJM1Z7X2PROD with RULES
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2022–0072 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(j) Alternative Methods of Compliance
(AMOCs)
The Manager, International Validation
Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in § 39.19. In accordance
with § 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. Information may be
emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
(1) Before using any approved AMOC,
notify your appropriate principal inspector,
VerDate Sep<11>2014
16:35 Feb 14, 2024
Jkt 262001
(k) Related Information
For more information about this AD,
contact William McCully, Aviation Safety
Engineer, FAA, International Validation
Branch, FAA, 1600 Stewart Ave., Suite 410,
Westbury, NY 11590; phone (404) 474–5548;
email william.mccully@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference of
the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) European Union Aviation Safety Agency
(EASA) AD 2022–0072, dated April 26, 2022.
(ii) [Reserved]
(3) For EASA AD 2022–0072, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet
easa.europa.eu. You may find the EASA
material on the EASA website at
ad.easa.europa.eu.
(4) You may view this service information
at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy.,
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 www.archives.gov/federal-register/cfr/
ibr-locations or email fr.inspection@nara.gov.
Issued on January 24, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2024–03137 Filed 2–14–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–2136; Project
Identifier MCAI–2023–00759–T; Amendment
39–22659; AD 2024–01–08]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is superseding
Airworthiness Directive (AD) 2019–16–
11, which applied to certain Airbus SAS
Model A300 F4–605R and FR–622R
airplanes. AD 2019–16–11 required
SUMMARY:
PO 00000
Frm 00020
Fmt 4700
Sfmt 4700
repetitive high frequency eddy current
(HFEC) inspections of the aft lower deck
cargo door (LDCD) frame forks; a onetime check of the LDCD clearances; a
one-time detailed visual inspection of
hooks, eccentric bushes, and x-stops;
and corrective actions if necessary. This
AD was prompted by a determination
that the threshold for the (repetitive)
HFEC inspection needs to be corrected,
and the LDCD frame forks modified.
This AD continues to require the actions
in AD 2019–16–11, requires correcting
the HFEC inspection threshold and
modifying the LDCD frame forks, and
prohibits the installation of affected
LDCDs under certain conditions; as
specified in a European Union Aviation
Safety Agency (EASA) AD, which is
incorporated by reference. The FAA is
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective March 21,
2024.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of March 21, 2024.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–2136; 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:
• For EASA material identified in this
final rule, contact EASA, KonradAdenauer-Ufer 3, 50668 Cologne,
Germany; telephone +49 221 8999 000;
email ADs@easa.europa.eu; website
easa.europa.eu. You may find this
material on the EASA website
ad.easa.europa.eu.
• You may view this material at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th Street, Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
It is also available in the AD docket at
regulations.gov under Docket No. FAA–
2023–2136.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aviation Safety Engineer, FAA,
1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 206–
231–3225; email dan.rodina@faa.gov.
SUPPLEMENTARY INFORMATION:
E:\FR\FM\15FER1.SGM
15FER1
Agencies
[Federal Register Volume 89, Number 32 (Thursday, February 15, 2024)]
[Rules and Regulations]
[Pages 11718-11720]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-03137]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-0039; Project Identifier MCAI-2023-00966-R;
Amendment 39-22665; AD 2024-02-01]
RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Airbus Helicopters Model EC225LP helicopters. This AD was
prompted by a report of incorrect door opening instructions on the
placards located on the right hand (RH) side of the VIP flap door. This
AD requires installing a placard specifying jettisoning instructions,
as specified in a European Union Aviation Safety Agency (EASA) AD,
which is incorporated by reference. The FAA is issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective March 1, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 1,
2024.
The FAA must receive comments on this AD by April 1, 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-2024-0039; 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 EASA AD, any comments received,
and other information. The street address for Docket Operations is
listed above.
Material Incorporated by Reference:
For EASA material incorporated by reference in this final
rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email [email protected]. You may find this
material on the EASA website at https://ad.easa.europa.eu.
You may view this material at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
Fort Worth, TX 76177. For information on the availability of this
material at the FAA, call (817) 222-5110. The EASA material is also
available at regulations.gov under Docket No. FAA-2024-0039.
Other Related Service Information: For Airbus Helicopters service
information identified in this final rule, contact Airbus Helicopters,
2701 North Forum Drive, Grand Prairie, TX 75052; telephone (972) 641-
0000 or (800) 232-0323; fax (972) 641-3775; or at airbus.com/en/products-services/helicopters/hcare-services/airbusworld. You may also
view this service information at the FAA contact information under
Material Incorporated by Reference above.
FOR FURTHER INFORMATION CONTACT: William McCully, Aviation Safety
Engineer, FAA, International Validation Branch, FAA, 1600 Stewart Ave.,
Suite 410, Westbury, NY 11590; phone (404) 474-5548; email
[email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2024-0039; Project Identifier MCAI-
2023-00966-R'' at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this final rule because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this final rule.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this AD contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this AD, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this AD. Submissions containing CBI should be sent to William
McCully, Aviation Safety Engineer, FAA, International Validation
Branch, FAA, 1600 Stewart Ave., 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
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2022-0072, dated April 26, 2022
(EASA AD 2022-0072), to correct an unsafe condition on Airbus
Helicopters Model EC 225 LP helicopters, serial numbers 2650, 2651,
2653, 2684, 2712, and 2796.
This AD was prompted by a report that placards located on the RH
side of the VIP flap door of the passenger cabin do not provide
adequate door opening instructions necessary to operate the RH side VIP
flap door in case of the helicopter ditching. The unsafe condition, if
not addressed, could prevent jettisoning of the RH side VIP flap door
during an emergency situation, possibly obstructing evacuation and
resulting in injury to occupants.
You may examine the EASA AD in the AD docket at regulations.gov
under Docket No. FAA-2024-0039.
Related Service Information Under 1 CFR Part 51
EASA AD 2022-0072 requires installing a placard over the current
placard, which correctly specifies
[[Page 11719]]
jettisoning instructions for the RH side of the VIP flap door.
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 ADDRESSES.
Other Related Service Information
The FAA reviewed Airbus Helicopters Alert Service Bulletin (ASB)
No. EC225-52A023, Revision 0, dated January 22, 2020 for Model EC225LP
helicopters. This service information specifies instructions for
covering the existing incorrect placard with a correct placard, and
reporting certain information to the manufacturer.
FAA's Determination
These helicopters have been approved by EASA and are approved for
operation in the United States. Pursuant to the FAA's bilateral
agreement with the European Union, EASA has notified the FAA about the
unsafe condition described in its AD. The FAA is issuing this AD after
evaluating all known relevant information and determining that the
unsafe condition described previously is likely to exist or develop on
other helicopters of the same type design.
AD Requirements
This AD requires accomplishing the actions specified in EASA AD
2022-0072, described previously, as incorporated by reference, except
for any differences identified as exceptions in the regulatory text of
this AD and except as discussed under ``Differences Between this AD and
the EASA 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 civil aviation
authority (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,
EASA AD 2022-0072 will be incorporated by reference in this FAA final
rule. This AD would, therefore, require compliance with EASA AD 2022-
0072 in its entirety through that incorporation, except for any
differences identified as exceptions in the regulatory text of this AD.
Using common terms that are the same as the heading of a particular
section in EASA AD 2022-0072 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 2022-0072. Service information
referenced in EASA AD 2022-0072 for compliance will be available at
regulations.gov under Docket No. FAA-2024-0039.
Differences Between This AD and the EASA AD
Service information referenced in EASA AD 2022-0072 specified
reporting certain information to Airbus Helicopters, including sending
pictures, whereas this AD does not require reporting any information or
sending any pictures.
Justification for Immediate Adoption and Determination of the Effective
Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
There are currently no domestic operators of these products.
Accordingly, notice and opportunity for prior public comment are
unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the
foregoing reasons, the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days.
Regulatory Flexibility Act
The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because the FAA has determined
that it has good cause to adopt this rule without prior notice and
comment, RFA analysis is not required.
Costs of Compliance
There are no costs of compliance with this AD because there are no
helicopters with this type certificate on the U.S. Registry.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866, and
(2) Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2024-02-01 Airbus Helicopters: Amendment 39-22665; Docket No. FAA-
2024-0039; Project Identifier MCAI-2023-00966-R.
(a) Effective Date
This airworthiness directive (AD) is effective March 1, 2024.
[[Page 11720]]
(b) Affected ADs
None.
(c) Applicability
This AD applies to Airbus Helicopters Model EC225LP helicopters,
serial numbers 2650, 2651, 2653, 2684, 2712, and 2796, certificated
in any category.
(d) Subject
Joint Aircraft System Component (JASC) Code: 5210, Passenger
crew doors.
(e) Unsafe Condition
This AD was prompted by a report of incorrect door opening
instructions on the placard located on the right-hand (RH) side of
the VIP flap door. The FAA is issuing this AD to address and correct
placards on the RH side VIP flap door. The unsafe condition, if not
addressed, could prevent jettisoning of the RH side VIP flap door
during an emergency situation, possibly obstructing evacuation and
resulting in injury to occupants.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Except as specified in paragraphs (h) and (i) of this AD: Comply
with all required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2022-0072, dated April 26, 2022 (EASA AD 2022-0072).
(h) Exceptions to EASA AD 2022-0072
(1) Where EASA AD 2022-0072 refers to its effective date, this
AD requires using the effective date of this AD.
(2) Where EASA AD 2022-0072 refers to flight hours, this AD
requires using hours time-in-service.
(3) Where the paragraph defined as placard installation in EASA
AD 2022-0072 states ``in accordance with the instructions of the
ASB,'' for this AD, replace that text with ``in accordance with the
Accomplishment Instructions, paragraph 3.B of the ASB.''
(i) No Reporting Requirement
Although the service information referenced in EASA AD 2022-0072
specifies to submit certain information to the manufacturer, this AD
does not include that requirement.
(j) Alternative Methods of Compliance (AMOCs)
The Manager, International Validation Branch, FAA, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in Sec. 39.19. In accordance with Sec. 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. Information may be emailed to: [email protected].
(1) 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) Related Information
For more information about this AD, contact William McCully,
Aviation Safety Engineer, FAA, International Validation Branch, FAA,
1600 Stewart Ave., Suite 410, Westbury, NY 11590; phone (404) 474-
5548; email [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless the AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2022-0072,
dated April 26, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0072, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; internet easa.europa.eu. You may find the EASA
material on the EASA website at ad.easa.europa.eu.
(4) You may view this service information at the FAA, Office of
the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., 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 www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on January 24, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2024-03137 Filed 2-14-24; 8:45 am]
BILLING CODE 4910-13-P