Airworthiness Directives; Airbus SAS Airplanes; Correction, 52024-52026 [2023-16884]
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52024
Federal Register / Vol. 88, No. 150 / Monday, August 7, 2023 / Rules and Regulations
(h) Retained Optional Mitigation for Certain
Airplanes, With No Changes
This paragraph restates the provisions of
paragraph (h) of AD 2023–12–20, with no
changes. For airplanes identified in
Bombardier Service Bulletin 650–35–002,
Revision 01, dated January 28, 2022, having,
as of the effective date of this AD, less than
6 years from the completion of the interior
modification specified in STC ST02355NY:
In lieu of accomplishing the oxygen system
hose replacement required by paragraph (g)
of this AD, comply with all conditions
specified in paragraphs (h)(1) through (3) of
this AD.
(1) The passenger oxygen system is tested
within 6 months after the effective date of
this AD, and thereafter at intervals not to
exceed 36 months, in accordance with the
Accomplishment Instructions of Bombardier
Service Bulletin 650–35–002, Revision 01,
dated January 28, 2022.
(2) If, during a test specified in paragraph
(h)(1) of this AD, any leak is found on any
hose, all oxygen system hoses having a part
number in the O2C20T1 series must be
replaced before further flight in accordance
with the Accomplishment Instructions of
Bombardier Service Bulletin 650–35–002,
Revision 01, dated January 28, 2022. Doing
this replacement terminates the tests
specified in paragraph (h)(1) of this AD.
(3) Except as specified by paragraph (h)(2)
of this AD, all oxygen system hoses having
a part number in the O2C20T1 series must be
replaced within 6 years from the completion
of the interior modification specified in STC
ST02355NY. Doing this replacement
terminates the tests specified in paragraph
(h)(1) of this AD.
ddrumheller on DSK120RN23PROD with RULES1
(i) Retained Parts Installation Prohibition,
With No Changes
This paragraph restates the requirements of
paragraph (i) of AD 2023–12–20, with no
changes. As of the effective date of this AD,
no person may install any oxygen system
hose having a part number in the O2C20T1
and O2C20T14 series on any airplane.
(j) Retained Credit for Previous Actions,
With No Changes
This paragraph restates the provisions of
paragraph (j) of AD 2023–12–20, with no
changes.
(1) This paragraph provides credit for
actions required by paragraph (g) of this AD,
if those actions were performed before the
effective date of this AD using Bombardier
Service Bulletin 605–35–006, dated August
23, 2021; or Bombardier Service Bulletin
650–35–002, dated August 23, 2021; as
applicable.
(2) This paragraph provides credit for
actions specified in paragraph (h) of this AD,
if those actions were performed before the
effective date of this AD using Bombardier
Service Bulletin 650–35–002, dated August
23, 2021.
(k) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Validation Branch, FAA, has the authority to
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15:10 Aug 04, 2023
Jkt 259001
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
responsible Flight Standards Office, as
appropriate. If sending information directly
to the manager of the International Validation
Branch, mail it to ATTN: Program Manager,
Continuing Operational Safety, at the address
identified in paragraph (l)(2) of this AD or
email to: 9-avs-nyaco-cos@faa.gov. If mailing
information, also submit information by
email.
(i) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(ii) AMOCs approved for AD 2023–12–20
are approved as AMOCs for the
corresponding provisions of this AD.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or Transport Canada; or
Bombardier, Inc.’s Transport Canada Design
Approval Organization (DAO). If approved by
the DAO, the approval must include the
DAO-authorized signature.
(l) Additional Information
(1) Refer to Transport Canada AD CF–
2022–34, dated June 20, 2022, for related
information. This Transport Canada AD may
be found in the AD docket at regulations.gov
under Docket No. FAA–2023–1654.
(2) For more information about this AD,
contact Elizabeth Dowling, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516–
228–7300; email 9-avs-nyaco-cos@faa.gov.
(3) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (m)(4) and (5) of this AD.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) 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 this AD specifies otherwise.
(3) The following service information was
approved for IBR on August 23, 2023 (88 FR
46063, July 19, 2023).
(i) Bombardier Service Bulletin 605–35–
006, Revision 01, dated January 28, 2022.
(ii) Bombardier Service Bulletin 650–35–
002, Revision 01, dated January 28, 2022.
(4) For service information identified in
this AD, contact Bombardier Business
Aircraft Customer Response Center, 400 CoˆteVertu Road West, Dorval, Que´bec H4S 1Y9,
Canada; telephone 514–855–2999; email
ac.yul@aero.bombardier.com; website
bombardier.com.
(5) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
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(6) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on July 31, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–16648 Filed 8–4–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–0927; Project
Identifier MCAI–2023–00013–T; Amendment
39–22461; AD 2023–12–03]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes; Correction
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting an
airworthiness directive (AD) that was
published in the Federal Register. That
AD applies to certain Airbus SAS Model
A350–941 and –1041 airplanes. As
published, a European Union Aviation
Safety Agency (EASA) AD number
specified in the regulatory text is
incorrect. This document corrects that
error. In all other respects, the original
document remains the same.
DATES: This correction is effective
August 7, 2023. The effective date of AD
2023–12–03 remains August 7, 2023.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of August 7, 2023 (88 FR 42598, July
3, 2023).
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–0927; 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; correction, 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.
SUMMARY:
E:\FR\FM\07AUR1.SGM
07AUR1
Federal Register / Vol. 88, No. 150 / Monday, August 7, 2023 / Rules and Regulations
Material Incorporated by Reference:
• For material incorporated by
reference in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu;
website easa.europa.eu. You may find
this IBR material on the EASA website
at ad.easa.europa.eu.
• You may view this material at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th St., 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–
2023–0927.
FOR FURTHER INFORMATION CONTACT: Dat
Le, Aviation Safety Engineer, FAA, 1600
Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516–228–7317;
email dat.v.le@faa.gov.
SUPPLEMENTARY INFORMATION:
ddrumheller on DSK120RN23PROD with RULES1
Adoption of the Amendment
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the FAA amends part 39
of the Federal Aviation Regulations (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.
[Corrected]
2. The FAA corrects § 39.13 by
correcting the airworthiness directive
published at 88 FR 42598 (July 3, 2023)
to read:
2023–12–03 Airbus SAS: Amendment 39–
22461; Docket No. FAA–2023–0927;
Project Identifier MCAI–2023–00013–T.
(a) Effective Date
This airworthiness directive (AD) is
effective August 7, 2023.
Related Service Information Under 1
CFR Part 51
EASA AD 2023–0004, dated January
6, 2023, describes new or more
restrictive airworthiness limitations for
airplane structures and safe life limits.
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.
Correction of Publication
This document corrects an error and
correctly adds the AD as an amendment
to 14 CFR 39.13. Although no other part
of the preamble or regulatory
information has been corrected, the
FAA is publishing the entire rule in the
Federal Register.
The effective date of this AD remains
August 7, 2023.
Since this action only corrects an
EASA AD reference, it has no adverse
Jkt 259001
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
■
Need for the Correction
As published, paragraph (i) in the
regulatory text of AD 2023–12–03 is
incorrect. Paragraph (i) of AD 2023–12–
03 refers to ‘‘EASA AD 2023–0017.’’ The
correct reference is ‘‘EASA AD 2023–
0004.’’
15:10 Aug 04, 2023
List of Subjects in 14 CFR Part 39
§ 39.13
Background
AD 2023–12–03, Amendment 39–
22461 (88 FR 42598, July 3, 2023) (AD
2023–12–03), requires revising the
existing maintenance or inspection
program, as applicable, to incorporate
new or more restrictive airworthiness
limitations for airplane structures and
safe life limits. That AD applies to
certain Airbus SAS Model A350–941
and –1041 airplanes.
VerDate Sep<11>2014
economic impact and imposes no
additional burden on any person.
Therefore, the FAA has determined that
notice and public procedures are
unnecessary.
(b) Affected ADs
This AD affects AD 2023–04–05,
Amendment 39–22352 (88 FR 13668, March
6, 2023) (AD 2023–04–05).
(c) Applicability
This AD applies to Airbus SAS Model
A350–941 and –1041 airplanes, certificated
in any category, with an original
airworthiness certificate or original export
certificate of airworthiness issued on or
before November 1, 2022.
(d) Subject
Air Transport Association (ATA) of
America Code: 05, Time Limits/Maintenance
Checks.
(e) Unsafe Condition
This AD was prompted by a determination
that new or more restrictive airworthiness
limitations are necessary. The FAA is issuing
this AD to address reduced structural
integrity of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Requirements
Except as specified in paragraph (h) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, European Union Aviation
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
52025
Safety Agency (EASA) AD 2023–0004, dated
January 6, 2023 (EASA AD 2023–0004).
(h) Exceptions to EASA AD 2023–0004
(1) This AD does not adopt the
requirements specified in paragraphs (1) and
(2) of EASA AD 2023–0004.
(2) Paragraph (3) of EASA AD 2023–0004
specifies revising ‘‘the approved AMP’’
within 12 months after its effective date, but
this AD requires revising the existing
maintenance or inspection program, as
applicable, within 90 days after the effective
date of this AD.
(3) The initial compliance time for doing
the tasks specified in paragraph (3) of EASA
2023–0004 is on or before the applicable
‘‘associated thresholds’’ as incorporated by
the requirements of paragraph (3) of EASA
AD 2023–0004, or within 90 days after the
effective date of this AD, whichever occurs
later.
(4) This AD does not adopt the provisions
specified in paragraph (4) of EASA AD 2023–
0004.
(5) This AD does not adopt the ‘‘Remarks’’
section of EASA AD 2023–0004.
(i) Provisions for Alternative Actions and
Intervals
After the existing maintenance or
inspection program has been revised as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) and
intervals are allowed unless they are
approved as specified in the provisions of the
‘‘Ref. Publications’’ section of EASA AD
2023–0004.
(j) Terminating Action for AD 2023–04–05
Accomplishing the actions required by this
AD terminates the corresponding
requirements of AD 2023–04–05, for the tasks
identified in the service information
referenced in EASA AD 2023–0004 only.
(k) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, International
Validation Branch, FAA, has the authority to
approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
In accordance with 14 CFR 39.19, send your
request to your principal inspector or
responsible Flight Standards Office, as
appropriate. If sending information directly
to the International Validation Branch, send
it to the attention of the person identified in
paragraph (l) of this AD. Information may be
emailed to: 9-AVS-AIR-730-AMOC@faa.gov.
Before using any approved AMOC, notify
your appropriate principal inspector, or
lacking a principal inspector, the manager of
the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, International Validation
Branch, FAA; or EASA; or Airbus SAS’s
EASA Design Organization Approval (DOA).
If approved by the DOA, the approval must
include the DOA-authorized signature.
E:\FR\FM\07AUR1.SGM
07AUR1
52026
Federal Register / Vol. 88, No. 150 / Monday, August 7, 2023 / Rules and Regulations
(l) Additional Information
For more information about this AD,
contact Dat Le, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–228–
7317; email Dat.V.Le@faa.gov.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) 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 this AD specifies otherwise.
(3) The following service information was
approved for IBR on August 7, 2023 (88 FR
42598, July 3, 2023).
(i) European Union Aviation Safety Agency
(EASA) AD 2023–0004, dated January 6,
2023.
(ii) [Reserved]
(4) For EASA AD 2023–0004, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; website
easa.europa.eu. You may find this EASA AD
on the EASA website at ad.easa.europa.eu.
(5) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South 216th
St., Des Moines, WA. For information on the
availability of this material at the FAA, call
206–231–3195.
(6) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fr.inspection@nara.gov, or go to
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on August 1, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–16884 Filed 8–3–23; 11:15 am]
BILLING CODE 4910–13–P
DEPARTMENT OF THE TREASURY
Office of Foreign Assets Control
31 CFR Part 555
Mali Sanctions Regulations
Office of Foreign Assets
Control, Treasury.
ACTION: Final rule.
AGENCY:
The Department of the
Treasury’s Office of Foreign Assets
Control (OFAC) is adopting a final rule
amending and replacing the Mali
Sanctions Regulations, published in
abbreviated form on February 7, 2020, to
further implement a July 26, 2019 Malirelated Executive order and provide a
more comprehensive set of regulations,
including additional interpretive and
ddrumheller on DSK120RN23PROD with RULES1
SUMMARY:
VerDate Sep<11>2014
15:10 Aug 04, 2023
Jkt 259001
definitional guidance, general licenses,
and other regulatory provisions.
DATES: This rule is effective August 7,
2023.
FOR FURTHER INFORMATION CONTACT:
OFAC: Assistant Director for Licensing,
202–622–2480; Assistant Director for
Regulatory Affairs, 202–622–4855; or
Assistant Director for Compliance, 202–
622–2490.
SUPPLEMENTARY INFORMATION:
Electronic Availability
This document and additional
information concerning OFAC are
available on OFAC’s website: https://
ofac.treasury.gov.
Background
On February 7, 2020, OFAC issued
the Mali Sanctions Regulations, 31 CFR
part 555 (85 FR 7223, February 7, 2020)
(the ‘‘Regulations’’), to implement
Executive Order (E.O.) 13882 of July 26,
2019, ‘‘Blocking Property and
Suspending Entry of Certain Persons
Contributing to the Situation in Mali’’
(84 FR 37055, July 30, 2019), pursuant
to authorities delegated to the Secretary
of the Treasury in E.O. 13882. The
Regulations were initially issued in
abbreviated form for the purpose of
providing immediate guidance to the
public. OFAC is revising the
Regulations to further implement E.O.
13882. OFAC is amending and reissuing
the Regulations as a more
comprehensive set of regulations that
includes additional interpretive
guidance and definitions, general
licenses, and other regulatory provisions
that will provide further guidance to the
public. Due to the number of regulatory
sections being updated or added, OFAC
is reissuing the Regulations in their
entirety.
On July 26, 2019, the President,
invoking the authority of, inter alia, the
International Emergency Economic
Powers Act (50 U.S.C. 1701 et seq.)
(IEEPA) and the United Nations
Participation Act (22 U.S.C. 287c)
(UNPA), issued E.O. 13882. In E.O.
13882, the President determined that
the situation in Mali, including repeated
violations of ceasefire arrangements
made pursuant to the 2015 Agreement
on Peace and Reconciliation in Mali; the
expansion of terrorist activities into
southern and central Mali; the
intensification of drug trafficking and
trafficking in persons, human rights
abuses, and hostage-taking; and the
intensification of attacks against
civilians, the Malian defense and
security forces, the United Nations
Multi-dimensional Integrated
Stabilizations Mission in Mali
PO 00000
Frm 00006
Fmt 4700
Sfmt 4700
(MINUSMA), and international security
presences, constituted an unusual and
extraordinary threat to the national
security and foreign policy of the United
States and declared a national
emergency to deal with that threat.
Section 1 of E.O. 13882 blocks, with
certain exceptions, all property and
interests in property that are in the
United States, that come within the
United States, or that are or come within
the possession or control of any U.S.
person of any person determined by the
Secretary of the Treasury, in
consultation with the Secretary of State
to: (i) be responsible for or complicit in,
or to have directly or indirectly engaged
in, any of the following in or in relation
to Mali: (A) actions or policies that
threaten the peace, security, or stability
of Mali; (B) actions or policies that
undermine democratic processes or
institutions in Mali; (C) a hostile act in
violation of, or an act that obstructs,
including by prolonged delay, or
threatens the implementation of, the
2015 Agreement on Peace and
Reconciliation in Mali; (D) planning,
directing, sponsoring, or conducting
attacks against local, regional, or state
institutions, the Malian defense and
security forces, any international
security presences, MINUSMA
peacekeepers, other United Nations or
associated personnel, or any other
peacekeeping operations; (E) obstructing
the delivery or distribution of, or access
to, humanitarian assistance; (F)
planning, directing, or committing an
act that violates international
humanitarian law or that constitutes a
serious human rights abuse or violation,
including an act involving the targeting
of civilians through the commission of
an act of violence, abduction or
enforced disappearance, forced
displacement, or an attack on a school,
hospital, religious site, or location
where civilians are seeking refuge; (G)
the use or recruitment of children by
armed groups or armed forces in the
context of the armed conflict in Mali;
(H) the illicit production or trafficking
of narcotics or their precursors
originating or transiting through Mali;
(I) trafficking in persons, smuggling in
migrants, or trafficking or smuggling
arms or illicitly acquired cultural
property; or (J) any transaction or series
of transactions involving bribery or
other corruption, such as the
misappropriation of Malian public
assets or expropriation of private assets
for personal gain or political purposes;
(ii) have materially assisted, sponsored,
or provided financial, material, or
technological support for, or goods or
services in support of, any person
E:\FR\FM\07AUR1.SGM
07AUR1
Agencies
[Federal Register Volume 88, Number 150 (Monday, August 7, 2023)]
[Rules and Regulations]
[Pages 52024-52026]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-16884]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-0927; Project Identifier MCAI-2023-00013-T;
Amendment 39-22461; AD 2023-12-03]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes; Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that was
published in the Federal Register. That AD applies to certain Airbus
SAS Model A350-941 and -1041 airplanes. As published, a European Union
Aviation Safety Agency (EASA) AD number specified in the regulatory
text is incorrect. This document corrects that error. In all other
respects, the original document remains the same.
DATES: This correction is effective August 7, 2023. The effective date
of AD 2023-12-03 remains August 7, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 7,
2023 (88 FR 42598, July 3, 2023).
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-0927; 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; correction, 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.
[[Page 52025]]
Material Incorporated by Reference:
For material incorporated by reference in this AD, contact
EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
8999 000; email [email protected]; website easa.europa.eu. You may
find this IBR material on the EASA website at ad.easa.europa.eu.
You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th St., 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-2023-0927.
FOR FURTHER INFORMATION CONTACT: Dat Le, Aviation Safety Engineer, FAA,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-
7317; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
AD 2023-12-03, Amendment 39-22461 (88 FR 42598, July 3, 2023) (AD
2023-12-03), requires revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations for airplane structures and safe life limits.
That AD applies to certain Airbus SAS Model A350-941 and -1041
airplanes.
Need for the Correction
As published, paragraph (i) in the regulatory text of AD 2023-12-03
is incorrect. Paragraph (i) of AD 2023-12-03 refers to ``EASA AD 2023-
0017.'' The correct reference is ``EASA AD 2023-0004.''
Related Service Information Under 1 CFR Part 51
EASA AD 2023-0004, dated January 6, 2023, describes new or more
restrictive airworthiness limitations for airplane structures and safe
life limits. 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.
Correction of Publication
This document corrects an error and correctly adds the AD as an
amendment to 14 CFR 39.13. Although no other part of the preamble or
regulatory information has been corrected, the FAA is publishing the
entire rule in the Federal Register.
The effective date of this AD remains August 7, 2023.
Since this action only corrects an EASA AD reference, it has no
adverse economic impact and imposes no additional burden on any person.
Therefore, the FAA has determined that notice and public procedures are
unnecessary.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the FAA amends part 39 of the Federal Aviation
Regulations (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 [Corrected]
0
2. The FAA corrects Sec. 39.13 by correcting the airworthiness
directive published at 88 FR 42598 (July 3, 2023) to read:
2023-12-03 Airbus SAS: Amendment 39-22461; Docket No. FAA-2023-0927;
Project Identifier MCAI-2023-00013-T.
(a) Effective Date
This airworthiness directive (AD) is effective August 7, 2023.
(b) Affected ADs
This AD affects AD 2023-04-05, Amendment 39-22352 (88 FR 13668,
March 6, 2023) (AD 2023-04-05).
(c) Applicability
This AD applies to Airbus SAS Model A350-941 and -1041
airplanes, certificated in any category, with an original
airworthiness certificate or original export certificate of
airworthiness issued on or before November 1, 2022.
(d) Subject
Air Transport Association (ATA) of America Code: 05, Time
Limits/Maintenance Checks.
(e) Unsafe Condition
This AD was prompted by a determination that new or more
restrictive airworthiness limitations are necessary. The FAA is
issuing this AD to address reduced structural integrity of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2023-0004, dated January 6, 2023 (EASA AD 2023-0004).
(h) Exceptions to EASA AD 2023-0004
(1) This AD does not adopt the requirements specified in
paragraphs (1) and (2) of EASA AD 2023-0004.
(2) Paragraph (3) of EASA AD 2023-0004 specifies revising ``the
approved AMP'' within 12 months after its effective date, but this
AD requires revising the existing maintenance or inspection program,
as applicable, within 90 days after the effective date of this AD.
(3) The initial compliance time for doing the tasks specified in
paragraph (3) of EASA 2023-0004 is on or before the applicable
``associated thresholds'' as incorporated by the requirements of
paragraph (3) of EASA AD 2023-0004, or within 90 days after the
effective date of this AD, whichever occurs later.
(4) This AD does not adopt the provisions specified in paragraph
(4) of EASA AD 2023-0004.
(5) This AD does not adopt the ``Remarks'' section of EASA AD
2023-0004.
(i) Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and intervals are allowed unless they
are approved as specified in the provisions of the ``Ref.
Publications'' section of EASA AD 2023-0004.
(j) Terminating Action for AD 2023-04-05
Accomplishing the actions required by this AD terminates the
corresponding requirements of AD 2023-04-05, for the tasks
identified in the service information referenced in EASA AD 2023-
0004 only.
(k) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Validation Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. In accordance with 14 CFR 39.19, send your request to your
principal inspector or responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send it to the attention of the person identified
in paragraph (l) of this AD. Information may be emailed to: [email protected]. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, International
Validation Branch, FAA; or EASA; or Airbus SAS's EASA Design
Organization Approval (DOA). If approved by the DOA, the approval
must include the DOA-authorized signature.
[[Page 52026]]
(l) Additional Information
For more information about this AD, contact Dat Le, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7317; email [email protected].
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) 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 this AD specifies otherwise.
(3) The following service information was approved for IBR on
August 7, 2023 (88 FR 42598, July 3, 2023).
(i) European Union Aviation Safety Agency (EASA) AD 2023-0004,
dated January 6, 2023.
(ii) [Reserved]
(4) For EASA AD 2023-0004, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(5) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(6) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on August 1, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-16884 Filed 8-3-23; 11:15 am]
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