Airworthiness Directives; Airbus SAS Airplanes, 32631-32634 [2023-10785]
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Federal Register / Vol. 88, No. 98 / Monday, May 22, 2023 / Rules and Regulations
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(4) Model A321–111, –112, –131, –211,
–212, –213, –231, –232, –251N, –252N,
–253N, –271N, –272N, –251NX, –252NX,
–253NX, –271NX, and –272NX airplanes.
(d) Subject
Air Transport Association (ATA) of
America Code 36, Pneumatic.
(e) Unsafe Condition
This AD was prompted by a report that
certain overheat detection system (OHDS)
sensing elements installed at certain
positions might not properly detect thermal
bleed leak events due to a quality escape
during the manufacturing process. The FAA
is issuing this AD to address OHDS sensing
elements that do not properly detect thermal
bleed leak events. The unsafe condition, if
not addressed, could result in an air leak
remaining undetected by the OHDS at an
affected position and not being isolated
during flight, possibly resulting in localized
areas of the main landing gear bay and keel
beam being exposed to high temperatures,
and consequent reduced structural integrity
of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
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(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 2022–0147, dated
July 14, 2022; corrected August 17, 2022
(EASA AD 2022–0147).
(h) Exceptions to EASA AD 2022–0147
(1) Where EASA AD 2022–0147 defines
‘‘Affected part’’ and identifies part numbers
and corresponding date codes as those
‘‘listed in Section 1.A of the VSB,’’ for this
AD, those part numbers and corresponding
date codes are listed in Section 1.A. of Kidde
Aerospace & Defense Service Bulletin CFD–
26–3, dated January 13, 2022; or Revision 1,
dated March 29, 2022. The date codes listed
in Section 1.A. of Kidde Aerospace & Defense
Service Bulletin CFD–26–3, dated January 13,
2022; and Revision 1, dated March 29, 2022;
do not apply to parts produced prior to
November 24, 2004, or after January 31, 2021.
(2) Where EASA AD 2022–0147 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) Where paragraph (2) of EASA AD 2022–
0147 refers to ‘‘any discrepancy as defined in
the SB,’’ for this AD, a discrepancy is an
incorrect electronic centralized aircraft
monitor (ECAM) alert (one not related to AIR
L WING LEAK) being displayed following the
inspection of any OHDS sensing element.
(4) Where the service information
referenced in EASA AD 2022–0147 specifies
to send an affected part to the manufacturer,
this AD does not include that requirement.
(5) This AD does not adopt the ‘‘Remarks’’
section of EASA AD 2022–0147.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2022–0147 specifies
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(j) 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 (k) 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.
(3) Required for Compliance (RC): Except
as required by paragraph (j)(2) of this AD, if
any service information contains procedures
or tests that are identified as RC, those
procedures and tests must be done to comply
with this AD; any procedures or tests that are
not identified as RC are recommended. Those
procedures and tests that are not identified
as RC may be deviated from using accepted
methods in accordance with the operator’s
maintenance or inspection program without
obtaining approval of an AMOC, provided
the procedures and tests identified as RC can
be done and the airplane can be put back in
an airworthy condition. Any substitutions or
changes to procedures or tests identified as
RC require approval of an AMOC.
(k) Additional Information
For more information about this AD,
contact Timothy Dowling, Aerospace
Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200 South
216th Street, Des Moines, WA 98198;
telephone 206–231–3667; email
timothy.p.dowling@faa.gov.
(l) 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.
(i) European Union Aviation Safety Agency
(EASA) AD 2022–0147, dated July 14, 2022;
corrected August 17, 2022.
(ii) Kidde Aerospace & Defense Service
Bulletin CFD–26–3, dated January 13, 2022.
(iii) Kidde Aerospace & Defense Service
Bulletin CFD–26–3, Revision 1, dated March
29, 2022.
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32631
(3) For EASA AD 2022–0147, 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.
(4) For Kidde Aerospace & Defense service
information identified in this AD, contact
Kidde Aerospace & Defense, 4200 Airport
Drive NW, Wilson, NC 27896; phone: 252–
246–7134; fax: 252–246–7181; email:
avionicssupport@collins.com; website
kiddeaerospace.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.
(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 April 28, 2023.
Gaetano A. Sciortino,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–10786 Filed 5–19–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–0936; Project
Identifier MCAI–2023–00135–T; Amendment
39–22426; AD 2023–09–03]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Airbus SAS Model A310 series
airplanes. This AD was prompted by a
determination that new or more
restrictive airworthiness limitations are
necessary. This AD requires revising the
existing maintenance or inspection
program, as applicable, to incorporate
new or more restrictive airworthiness
limitations, 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 June 6, 2023.
The Director of the Federal Register
approved the incorporation by reference
SUMMARY:
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Federal Register / Vol. 88, No. 98 / Monday, May 22, 2023 / Rules and Regulations
of a certain publication listed in this AD
as of June 6, 2023.
The FAA must receive comments on
this AD by July 6, 2023.
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–2023–0936; 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 street address for
Docket Operations is listed above.
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 material on the EASA website:
ad.easa.europa.eu.
• You may view this service
information 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 at
regulations.gov under Docket No. FAA–
2023–0936.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Validation Branch, FAA,
1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone (206)
231–3225; email dan.rodina@faa.gov.
SUPPLEMENTARY INFORMATION:
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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–2023–0936;
Project Identifier MCAI–2023–00135–T’’
at the beginning of your comments. The
most helpful comments reference a
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17:13 May 19, 2023
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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 Dan Rodina,
Aerospace Engineer, International
Validation Branch, FAA, 1600 Stewart
Avenue, Suite 410, Westbury, NY
11590; telephone (206) 231–3225; email
dan.rodina@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 2023–0018,
dated January 23, 2023 (EASA AD
2023–0018) (also referred to as the
MCAI), to correct an unsafe condition
for all Airbus SAS Model A310–203,
–203C, –204, –221, –222, –304, –308,
–322, –324 and –325 airplanes. Model
A310–203C and –308 airplanes are not
certificated by the FAA and are not
included on the U.S. type certificate
data sheet; this AD therefore does not
include those airplanes in the
applicability.
The MCAI states that new or more
restrictive airworthiness limitations and
tasks are necessary. EASA AD 2023–
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0018 specifies that it requires a
limitations and tasks already in Airbus
A310 Airworthiness Limitations Section
(ALS), Part 4, System Equipment
Maintenance Requirements (SEMR),
Revision 03, dated August 28, 2017, that
is required by EASA AD 2017–0202,
dated October 12, 2017 (which
corresponds to FAA AD 2018–18–21,
Amendment 39–19400 (83 FR 47054,
September 18, 2018) (AD 2018–18–21)),
and that incorporation of EASA AD
2023–0018 invalidates (terminates) prior
instructions for that task. This AD,
therefore, for the tasks identified in the
service information referenced in EASA
AD 2023–0018, terminates the
limitations for the corresponding tasks
required by paragraph (g) of AD 2018–
18–21, for Model A310 series airplanes
only.
The FAA is issuing this AD to address
the effects of aging on airplane systems.
Such effects could change system
characteristics, leading to an increased
potential for failure of certain lifelimited parts. You may examine the
MCAI in the AD docket at
regulations.gov under Docket No. FAA–
2023–0936.
Related Service Information Under 1
CFR Part 51
EASA AD 2023–0018 specifies 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.
FAA’s Determination
This product has been approved by
the aviation authority of another
country and is 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 the MCAI referenced above. The FAA
is issuing this AD after determining that
the unsafe condition described
previously is likely to exist or develop
on other products of the same type
design.
AD Requirements
This AD requires revising the existing
maintenance or inspection program, as
applicable, to incorporate new or more
restrictive airworthiness limitations,
which are specified in EASA AD 2023–
0018 described previously, as
incorporated by reference. Any
differences with EASA AD 2023–0018
are identified as exceptions in the
regulatory text of this AD.
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Federal Register / Vol. 88, No. 98 / Monday, May 22, 2023 / Rules and Regulations
This AD requires revisions to certain
operator maintenance documents to
include new actions (e.g., inspections).
Compliance with these actions is
required by 14 CFR 91.403(c). For
airplanes that have been previously
modified, altered, or repaired in the
areas addressed by this AD, the operator
may not be able to accomplish the
actions described in the revisions. In
this situation, to comply with 14 CFR
91.403(c), the operator must request
approval for an alternative method of
compliance (AMOC) according to
paragraph (k)(1) of this AD.
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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 2023–0018
is incorporated by reference in this AD.
This AD requires compliance with
EASA AD 2023–0018 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 2023–0018 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 2023–0018.
Service information required by EASA
AD 2023–0018 for compliance will be
available at regulations.gov under
Docket No. FAA–2023–0936 after this
AD is published.
Airworthiness Limitation ADs Using
the New Process
The FAA’s process of incorporating
by reference MCAI ADs as the primary
source of information for compliance
with corresponding FAA ADs has been
limited to certain MCAI ADs (primarily
those with service bulletins as the
primary source of information for
accomplishing the actions required by
the FAA AD). However, the FAA is now
expanding the process to include MCAI
ADs that require a change to
airworthiness limitation documents,
such as airworthiness limitation
sections.
For these ADs that incorporate by
reference an MCAI AD that changes
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airworthiness limitations, the FAA
requirements are unchanged. Operators
must revise the existing maintenance or
inspection program, as applicable, to
incorporate the information specified in
the new airworthiness limitation
document. The airworthiness
limitations must be followed according
to 14 CFR 91.403(c) and 91.409(e).
The previous format of the
airworthiness limitation ADs included a
paragraph that specified that no
alternative actions (e.g., inspections) or
intervals may be used unless the actions
and intervals are approved as an AMOC
in accordance with the procedures
specified in the AMOCs paragraph
under ‘‘Additional FAA Provisions.’’
This new format includes a ‘‘New
Provisions for Alternative Actions and
Intervals’’ paragraph that does not
specifically refer to AMOCs, but
operators may still request an AMOC to
use an alternative action or interval.
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 forgoing reason(s), 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 (RFA)
The requirements of the 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 notice and comment, RFA
analysis is not required.
Costs of Compliance
Currently, there are no affected U.S.registered airplanes. If an affected
airplane is imported and placed on the
U.S. Register in the future, the FAA
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32633
provides the following cost estimates to
comply with this AD:
The FAA has determined that revising
the existing maintenance or inspection
program takes an average of 90 workhours per operator, although the FAA
recognizes that this number may vary
from operator to operator. Since
operators incorporate maintenance or
inspection program changes for their
affected fleet(s), the FAA has
determined that a per-operator estimate
is more accurate than a per-airplane
estimate. Therefore, the FAA estimates
the total cost per operator to be $7,650
(90 work-hours × $85 per work-hour).
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,
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Federal Register / Vol. 88, No. 98 / Monday, May 22, 2023 / Rules and Regulations
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:
■
2023–09–03 Airbus SAS: Amendment 39–
22426; Docket No. FAA–2023–0936;
Project Identifier MCAI–2023–00135–T.
(a) Effective Date
This airworthiness directive (AD) is
effective June 6, 2023.
(c) Applicability
This AD applies to all Airbus SAS Model
A310–203, –204, –221, –222, –304, –322,
–324, and –325 airplanes, certificated in any
category.
(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 the risks associated with
the effects of aging on airplane systems. The
unsafe condition, if not addressed, could
change system characteristics, leading to an
increased potential for failure of certain lifelimited parts, and reduced structural
integrity or controllability of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
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(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 2023–0018, dated
January 23, 2023 (EASA AD 2023–0018).
(h) Exceptions to EASA AD 2023–0018
(1) This AD does not adopt the
requirements specified in paragraphs (1) and
(2) of EASA AD 2023–0018.
(2) Paragraph (3) of EASA AD 2023–0018
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
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Jkt 259001
(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) or
intervals are allowed unless they are
approved as specified in the provisions of the
‘‘Ref. Publications’’ section of EASA AD
2023–0018.
(j) Terminating Action for AD 2018–18–21
(b) Affected ADs
This AD affects AD 2018–18–21,
Amendment 39–19400 (83 FR 47054,
September 18, 2018) (AD 2018–18–21).
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2023–0018 is on or before the applicable
‘‘limitations’’ as incorporated by the
requirements of paragraph (3) of EASA AD
2023–0018, or within 90 days after the
effective date of this AD, whichever occurs
later.
(4) This AD does not adopt the provisions
specified in paragraphs (4) of EASA AD
2023–0018.
(5) This AD does not adopt the ‘‘Remarks’’
section of EASA AD 2023–0018.
For Model A310 series airplanes only:
Accomplishing the actions required by this
AD terminates the corresponding
requirements of AD 2018–18–21, for the tasks
identified in the service information
referenced in EASA AD 2023–0018 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.
(l) Additional Information
For more information about this AD,
contact Dan Rodina, Aerospace Engineer,
International Validation Branch, FAA, 1600
Stewart Avenue, Suite 410, Westbury, NY
11590; telephone (206) 231–3225; email
dan.rodina@faa.gov.
(m) 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.
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Sfmt 4700
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency
(EASA) AD 2023–0018, dated January 23,
2023.
(ii) [Reserved]
(3) For EASA AD 2023–0018, 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: ad.easa.europa.eu.
(4) 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.
(5) You may view this material 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 April 28, 2023.
Gaetano A. Sciortino,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–10785 Filed 5–19–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2022–0939; Airspace
Docket No. 21–AEA–25]
RIN 2120–AA66
Amendment of VOR Federal Airways;
Northeast United States
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action amends Very High
Frequency (VHF) Omnidirectional
Range (VOR) Federal airway V–260 in
support of the FAA’s VOR Minimum
Operational Network (MON) program.
DATES: Effective date 0901 UTC, August
10, 2023. The Director of the Federal
Register approves this incorporation by
reference action under 1 CFR part 51,
subject to the annual revision of FAA JO
Order 7400.11 and publication of
conforming amendments.
ADDRESSES: A copy of the Notice of
Proposed Rulemaking (NPRM), all
comments received, this final rule, and
all background material may be viewed
online at www.regulations.gov using the
FAA Docket number. Electronic
retrieval help and guidelines are
SUMMARY:
E:\FR\FM\22MYR1.SGM
22MYR1
]]>Agencies
[Federal Register Volume 88, Number 98 (Monday, May 22, 2023)]
[Rules and Regulations]
[Pages 32631-32634]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-10785]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-0936; Project Identifier MCAI-2023-00135-T;
Amendment 39-22426; AD 2023-09-03]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Airbus SAS Model A310 series airplanes. This AD was prompted by a
determination that new or more restrictive airworthiness limitations
are necessary. This AD requires revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations, 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 June 6, 2023.
The Director of the Federal Register approved the incorporation by
reference
[[Page 32632]]
of a certain publication listed in this AD as of June 6, 2023.
The FAA must receive comments on this AD by July 6, 2023.
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-2023-0936; 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
street address for Docket Operations is listed above.
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 material on the EASA website: ad.easa.europa.eu.
You may view this service information 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 at
regulations.gov under Docket No. FAA-2023-0936.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Validation Branch, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone (206) 231-3225; 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-2023-0936; Project Identifier MCAI-
2023-00135-T'' 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 Dan
Rodina, Aerospace Engineer, International Validation Branch, FAA, 1600
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone (206) 231-
3225; 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 2023-0018, dated January 23, 2023
(EASA AD 2023-0018) (also referred to as the MCAI), to correct an
unsafe condition for all Airbus SAS Model A310-203, -203C, -204, -221,
-222, -304, -308, -322, -324 and -325 airplanes. Model A310-203C and -
308 airplanes are not certificated by the FAA and are not included on
the U.S. type certificate data sheet; this AD therefore does not
include those airplanes in the applicability.
The MCAI states that new or more restrictive airworthiness
limitations and tasks are necessary. EASA AD 2023-0018 specifies that
it requires a limitations and tasks already in Airbus A310
Airworthiness Limitations Section (ALS), Part 4, System Equipment
Maintenance Requirements (SEMR), Revision 03, dated August 28, 2017,
that is required by EASA AD 2017-0202, dated October 12, 2017 (which
corresponds to FAA AD 2018-18-21, Amendment 39-19400 (83 FR 47054,
September 18, 2018) (AD 2018-18-21)), and that incorporation of EASA AD
2023-0018 invalidates (terminates) prior instructions for that task.
This AD, therefore, for the tasks identified in the service information
referenced in EASA AD 2023-0018, terminates the limitations for the
corresponding tasks required by paragraph (g) of AD 2018-18-21, for
Model A310 series airplanes only.
The FAA is issuing this AD to address the effects of aging on
airplane systems. Such effects could change system characteristics,
leading to an increased potential for failure of certain life-limited
parts. You may examine the MCAI in the AD docket at regulations.gov
under Docket No. FAA-2023-0936.
Related Service Information Under 1 CFR Part 51
EASA AD 2023-0018 specifies 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.
FAA's Determination
This product has been approved by the aviation authority of another
country and is 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 the MCAI
referenced above. The FAA is issuing this AD after determining that the
unsafe condition described previously is likely to exist or develop on
other products of the same type design.
AD Requirements
This AD requires revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness limitations, which are specified in EASA AD 2023-0018
described previously, as incorporated by reference. Any differences
with EASA AD 2023-0018 are identified as exceptions in the regulatory
text of this AD.
[[Page 32633]]
This AD requires revisions to certain operator maintenance
documents to include new actions (e.g., inspections). Compliance with
these actions is required by 14 CFR 91.403(c). For airplanes that have
been previously modified, altered, or repaired in the areas addressed
by this AD, the operator may not be able to accomplish the actions
described in the revisions. In this situation, to comply with 14 CFR
91.403(c), the operator must request approval for an alternative method
of compliance (AMOC) according to paragraph (k)(1) of this AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some 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 2023-0018 is incorporated by reference in this AD. This AD
requires compliance with EASA AD 2023-0018 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 2023-0018 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 2023-
0018. Service information required by EASA AD 2023-0018 for compliance
will be available at regulations.gov under Docket No. FAA-2023-0936
after this AD is published.
Airworthiness Limitation ADs Using the New Process
The FAA's process of incorporating by reference MCAI ADs as the
primary source of information for compliance with corresponding FAA ADs
has been limited to certain MCAI ADs (primarily those with service
bulletins as the primary source of information for accomplishing the
actions required by the FAA AD). However, the FAA is now expanding the
process to include MCAI ADs that require a change to airworthiness
limitation documents, such as airworthiness limitation sections.
For these ADs that incorporate by reference an MCAI AD that changes
airworthiness limitations, the FAA requirements are unchanged.
Operators must revise the existing maintenance or inspection program,
as applicable, to incorporate the information specified in the new
airworthiness limitation document. The airworthiness limitations must
be followed according to 14 CFR 91.403(c) and 91.409(e).
The previous format of the airworthiness limitation ADs included a
paragraph that specified that no alternative actions (e.g.,
inspections) or intervals may be used unless the actions and intervals
are approved as an AMOC in accordance with the procedures specified in
the AMOCs paragraph under ``Additional FAA Provisions.'' This new
format includes a ``New Provisions for Alternative Actions and
Intervals'' paragraph that does not specifically refer to AMOCs, but
operators may still request an AMOC to use an alternative action or
interval.
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
forgoing reason(s), 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 (RFA)
The requirements of the 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 notice and comment, RFA analysis is not required.
Costs of Compliance
Currently, there are no affected U.S.-registered airplanes. If an
affected airplane is imported and placed on the U.S. Register in the
future, the FAA provides the following cost estimates to comply with
this AD:
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the FAA recognizes that this number may vary from operator to
operator. Since operators incorporate maintenance or inspection program
changes for their affected fleet(s), the FAA has determined that a per-
operator estimate is more accurate than a per-airplane estimate.
Therefore, the FAA estimates the total cost per operator to be $7,650
(90 work-hours x $85 per work-hour).
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,
[[Page 32634]]
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:
2023-09-03 Airbus SAS: Amendment 39-22426; Docket No. FAA-2023-0936;
Project Identifier MCAI-2023-00135-T.
(a) Effective Date
This airworthiness directive (AD) is effective June 6, 2023.
(b) Affected ADs
This AD affects AD 2018-18-21, Amendment 39-19400 (83 FR 47054,
September 18, 2018) (AD 2018-18-21).
(c) Applicability
This AD applies to all Airbus SAS Model A310-203, -204, -221, -
222, -304, -322, -324, and -325 airplanes, certificated in any
category.
(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 the risks associated with the effects of
aging on airplane systems. The unsafe condition, if not addressed,
could change system characteristics, leading to an increased
potential for failure of certain life-limited parts, and reduced
structural integrity or controllability 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
2023-0018, dated January 23, 2023 (EASA AD 2023-0018).
(h) Exceptions to EASA AD 2023-0018
(1) This AD does not adopt the requirements specified in
paragraphs (1) and (2) of EASA AD 2023-0018.
(2) Paragraph (3) of EASA AD 2023-0018 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 2023-0018 is on or before the applicable
``limitations'' as incorporated by the requirements of paragraph (3)
of EASA AD 2023-0018, or within 90 days after the effective date of
this AD, whichever occurs later.
(4) This AD does not adopt the provisions specified in
paragraphs (4) of EASA AD 2023-0018.
(5) This AD does not adopt the ``Remarks'' section of EASA AD
2023-0018.
(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) or intervals are allowed unless they are
approved as specified in the provisions of the ``Ref. Publications''
section of EASA AD 2023-0018.
(j) Terminating Action for AD 2018-18-21
For Model A310 series airplanes only: Accomplishing the actions
required by this AD terminates the corresponding requirements of AD
2018-18-21, for the tasks identified in the service information
referenced in EASA AD 2023-0018 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.
(l) Additional Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, International Validation Branch, FAA, 1600
Stewart Avenue, Suite 410, Westbury, NY 11590; telephone (206) 231-
3225; email [email protected].
(m) 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 this AD specifies otherwise.
(i) European Union Aviation Safety Agency (EASA) AD 2023-0018,
dated January 23, 2023.
(ii) [Reserved]
(3) For EASA AD 2023-0018, 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: ad.easa.europa.eu.
(4) 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.
(5) You may view this material 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 April 28, 2023.
Gaetano A. Sciortino,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-10785 Filed 5-19-23; 8:45 am]
BILLING CODE 4910-13-P
