Proposed Rule2024-15959
Airworthiness Directives; Airbus SAS Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
July 24, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to supersede Airworthiness Directive (AD) 2023-21-02, which applies to certain Airbus SAS Model A330-200 series, A330-200 Freighter series, A330-300 series, A330-800 series, and A330- 900 series airplanes. AD 2023-21-02 requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. Since the FAA issued AD 2023-21-02, the FAA has determined that new or more restrictive airworthiness limitations are necessary. This proposed AD would continue to require certain actions in AD 2023-21-02 and would require 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 proposed for incorporation by reference (IBR). The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 89 Issue 142 (Wednesday, July 24, 2024)</title>
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[Federal Register Volume 89, Number 142 (Wednesday, July 24, 2024)]
[Proposed Rules]
[Pages 59853-59857]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-15959]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1894; Project Identifier MCAI-2024-00036-T]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2023-21-02, which applies to certain Airbus SAS Model A330-200 series,
A330-200 Freighter series, A330-300 series, A330-800 series, and A330-
900 series airplanes. AD 2023-21-02 requires revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations. Since the FAA issued AD
2023-21-02, the FAA has determined that new or more restrictive
airworthiness limitations are necessary. This proposed AD would
continue to require certain actions in AD 2023-21-02 and would require
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 proposed for incorporation by reference (IBR). The FAA is proposing
this AD to address the unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by September
9, 2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
<bullet> Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-1894; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
<bullet> For EASA material, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#a3e2e7d0e3c6c2d0c28dc6d6d1ccd3c28dc6d6"><span class="__cf_email__" data-cfemail="c68782b586a3a7b5a7e8a3b3b4a9b6a7e8a3b3">[email protected]</span></a>; website easa.europa.eu. You may find this material
on the EASA website at ad.easa.europa.eu.
<bullet> You may view this material at the FAA, Airworthiness
Products Section,
[[Page 59854]]
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 at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-
2024-1894.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 206-231-3229; email <a href="/cdn-cgi/l/email-protection#186e74797c7175716a366d74617976776e587e7979367f776e"><span class="__cf_email__" data-cfemail="50263c3134393d39227e253c29313e3f26103631317e373f26">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2024-1894; Project Identifier
MCAI-2024-00036-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
<a href="http://regulations.gov">regulations.gov</a>, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Vladimir Ulyanov, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone 206-231-3229; email
<a href="/cdn-cgi/l/email-protection#1e68727f7a7773776c306b72677f7071685e787f7f30797168"><span class="__cf_email__" data-cfemail="8ef8e2efeae7e3e7fca0fbe2f7efe0e1f8cee8efefa0e9e1f8">[email protected]</span></a>. Any commentary that the FAA receives that is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.
Background
The FAA issued AD 2023-21-02, Amendment 39-22574 (88 FR 76107,
November 6, 2023) (AD 2023-21-02), for certain Airbus SAS Model 330-
201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -
322, -323, -341, -342, -343, -841 and -941 airplanes. AD 2023-21-02 was
prompted by an MCAI originated by EASA, which is the Technical Agent
for the Member States of the European Union. EASA issued AD 2022-0187,
dated September 13, 2022 (EASA AD 2022-0187) and AD 2023-0015, dated
January 19, 2023 (EASA AD 2023-0015) (which correspond to FAA AD 2023-
21-02), to correct an unsafe condition.
AD 2023-21-02 requires revising the existing maintenance or
inspection program, as applicable, to incorporate additional new or
more restrictive airworthiness limitations. The FAA issued AD 2023-21-
02 to address fatigue cracking, accidental damage, and corrosion in
principal structural elements; such fatigue cracking, accidental
damage, and corrosion could result in reduced structural integrity of
the airplane.
Actions Since AD 2023-21-02 Was Issued
Since the FAA issued AD 2023-21-02, EASA superseded AD 2022-0187
and EASA AD 2023-0015 and issued EASA AD 2024-0011, dated January 10,
2024 (EASA AD 2024-0011), for all Airbus SAS Model A330-201, -202, -
203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -
341, -342, -343, -841 and -941 airplanes. EASA AD 2024-0011 states that
new or more restrictive airworthiness limitations have been developed.
Airplanes with an original airworthiness certificate or original
export certificate of airworthiness issued after October 20, 2023, must
comply with the airworthiness limitations specified as part of the
approved type design and referenced on the type certificate data sheet;
this proposed AD therefore does not include those airplanes in the
applicability.
The FAA is proposing this AD to address fatigue cracking,
accidental damage, and corrosion in principal structural elements; such
fatigue cracking, accidental damage, and corrosion could result in
reduced structural integrity of the airplane. You may examine the MCAI
in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2024-1894.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed EASA AD 2024-0011. This material specifies new or
more restrictive airworthiness limitations for airplane structures.
This proposed AD would also require EASA AD 2022-0187 and EASA AD
2023-0015, which the Director of the Federal Register approved for
incorporation by reference as of December 11, 2023 (88 FR 76107,
November 6, 2023).
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.
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 and
service information referenced above. The FAA is issuing this NPRM
after determining that the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would retain all requirements of AD 2023-21-02.
This proposed AD would also require revising the existing maintenance
or inspection program, as applicable, to incorporate additional new or
more restrictive airworthiness limitations, which are specified in EASA
AD 2024-0011 already described, as proposed for incorporation by
reference. Any differences with EASA AD 2024-0011 are identified as
exceptions in the regulatory text of this AD.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these is required by 14 CFR 91.403(c). For airplanes
that have been previously modified, altered, or repaired in the areas
addressed by this proposed 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
(m)(1) of this proposed AD.
[[Page 59855]]
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, the
FAA proposes to retain the IBR of EASA AD 2022-0187 and EASA AD 2023-
0015 and incorporate EASA AD 2024-0011 by reference in the FAA final
rule. This proposed AD would, therefore, require compliance with EASA
AD 2024-0011, EASA AD 2022-0187, and EASA AD 2023-0015 through that
incorporation, except for any differences identified as exceptions in
the regulatory text of this proposed AD. Using common terms that are
the same as the heading of a particular section in EASA AD 2022-0187,
EASA 2023-0015, or EASA AD 2024-0011 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 2024-0011.
Service information required by EASA AD 2024-0011 for compliance will
be available at <a href="http://regulations.gov">regulations.gov</a> by searching for and locating Docket
No. FAA-2024-1894 after the FAA final rule 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 AD Provisions.'' This new format
includes a ``New Provisions for Alternative and Intervals'' paragraph
that does not specifically refer to AMOCs, but operators may still
request an AMOC to use an alternative or interval.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 126 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
The FAA estimates the total cost per operator for the retained
actions from AD 2023-21-02 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency 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.
The FAA estimates the total cost per operator for the new proposed
actions 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
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by:
0
a. Removing Airworthiness Directive (AD) 2023-21-02, Amendment 39-22574
(88 FR 76107, November 6, 2023); and
0
b. Adding the following new AD:
Airbus SAS: Docket No. FAA-2024-1894; Project Identifier MCAI-2024-
00036-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by September 9, 2024.
(b) Affected ADs
This AD replaces AD 2023-21-02, Amendment 39-22574 (88 FR 76107,
November 6, 2023) (AD 2023-21-02).
(c) Applicability
This AD applies to Airbus SAS airplanes, identified in
paragraphs (c)(1) through (5) of this AD, certificated in any
category, with an original airworthiness certificate or original
export certificate of airworthiness issued on or before October 20,
2023.
(1) Model A330-201, -202, -203, -223, and -243 airplanes.
(2) Model A330-223F and -243F airplanes.
[[Page 59856]]
(3) Model A330-301, -302, -303, -321, -322, -323, -341, -342,
and -343 airplanes.
(4) Model A330-841 airplanes.
(5) Model A330-941 airplanes.
(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 fatigue cracking, accidental damage, and
corrosion in principle structural elements. The unsafe condition, if
not addressed, could result in reduced structural integrity of the
airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Revision of the Existing Maintenance or Inspection
Program, With New Terminating Action
This paragraph restates the requirements of paragraph (j) of AD
2023-21-02, with new terminating action. For airplanes with an
original airworthiness certificate or original export certificate of
airworthiness issued on or before November 18, 2022: 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 2022-0187, dated
September 13, 2022 (EASA AD 2022-0187), and AD 2023-0015, dated
January 19, 2023 (EASA AD 2023-0015); as applicable. Where EASA AD
2023-0015 affects the same airworthiness limitations as those in
EASA AD 2022-0187, the airworthiness limitations referenced in EASA
AD 2023-0015 prevail. Accomplishing the revision of the existing
maintenance or inspection program required by paragraph (j) of this
AD terminates the requirements of this paragraph.
(h) Retained Exceptions to EASA AD 2022-0187 and EASA AD 2023-0015,
With No Changes
This paragraph restates the exceptions specified in paragraph
(k) of AD 2023-21-02, with no changes.
(1) This AD does not adopt the requirements specified in
paragraphs (1) and (2) of EASA AD 2022-0187 and of EASA AD 2023-
0015.
(2) Paragraph (3) of EASA AD 2022-0187 and of EASA AD 2023-0015
specifies revising ``the AMP'' within 12 months after the respective
EASA AD's effective date, but this AD requires revising the existing
maintenance or inspection program, as applicable, within 90 days
after December 11, 2023 (the effective date of AD 2023-21-02).
(3) The initial compliance time for doing the tasks specified in
paragraph (3) of EASA AD 2022-0187 and of EASA AD 2023-0015 is at
the applicable ``associated thresholds'' as incorporated by the
requirements of paragraph (3) of EASA AD 2022-0187 and of EASA AD
2023-0015, or within 90 days after December 11, 2023 (the effective
date of AD 2023-21-02), whichever occurs later.
(4) This AD does not adopt the provisions specified in
paragraphs (4) and (5) of EASA AD 2022-0187.
(5) Where EASA AD 2022-0187 defines ``The ALS,'' replace the
text ``Airbus A330 Airworthiness Limitations Section (ALS) Part 2
Revision 05,'' with ``Airbus A330 Airworthiness Limitations Section
(ALS) Part 2 Revision 05 Issue 02.''
(6) This AD does not adopt the provisions specified in paragraph
(4) of EASA AD 2023-0015.
(7) This AD does not require incorporating Section 4, ``Damage
Tolerant-Airworthiness Limitations Items-Tasks Beyond MPPT,'' of
``the ALS'' specified in EASA AD 2022-0187 and in EASA AD 2023-0015.
(8) This AD does not adopt the ``Remarks'' section of EASA AD
2022-0187 and of EASA AD 2023-0015.
(i) Retained Provisions for Alternative Actions and Intervals, With New
Exception
This paragraph restates the provisions of paragraph (l) of AD
2023-21-02, with a new exception. Except as required by paragraph
(j) 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 2022-0187
or of EASA AD 2023-0015.
(j) New Revision of the Existing Maintenance or Inspection Program
Except as specified in paragraph (k) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2024-0011, dated January 10, 2024 (EASA AD
2024-0011). Accomplishing the revision of the existing maintenance
or inspection program required by this paragraph terminates the
requirements of paragraph (g) of this AD.
(k) Exceptions to EASA AD 2024-0011
(1) This AD does not adopt the requirements specified in
paragraphs (1) and (2) of EASA AD 2024-0011.
(2) Paragraph (3) of EASA AD 2024-0011 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 AD 2024-0011 is at the applicable ``associated
thresholds'' as incorporated by the requirements of paragraph (3) of
EASA AD 2024-0011, 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) and (5) of EASA AD 2024-0011.
(5) This AD does not adopt the ``Remarks'' section of EASA AD
2024-0011.
(6) This AD does not require incorporating Section 4, ``Damage
Tolerant-Airworthiness Limitations Items-Tasks Beyond MPPT,'' of
``the ALS'' specified in EASA 2024-0011.
(l) New Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (j) 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 2024-0011.
(m) 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 manager of the
International Validation Branch, mail it to the address identified
in paragraph (n) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#6b52462a3d38462a2239465c585b462a2624282b0d0a0a450c041d"><span class="__cf_email__" data-cfemail="a1988ce0f7f28ce0e8f38c9692918ce0eceee2e1c7c0c08fc6ced7">[email protected]</span></a>.
(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.
(n) Additional Information
For more information about this AD, contact Vladimir Ulyanov,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 206-231-3229; email
<a href="/cdn-cgi/l/email-protection#50263c3134393d39227e253c29313e3f26103631317e373f26"><span class="__cf_email__" data-cfemail="c5b3a9a4a1aca8acb7ebb0a9bca4abaab385a3a4a4eba2aab3">[email protected]</span></a>.
(o) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the material listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless this AD specifies otherwise.
(3) The following material was approved for IBR on [DATE 35 DAYS
AFTER PUBLICATION OF THE FINAL RULE].
(i) European Union Aviation Safety Agency (EASA) AD 2024-0011,
dated January 10, 2024.
(ii) [Reserved]
(4) The following material was approved for IBR on December 11,
2023 (88 FR 76107, November 6, 2023).
(i) European Union Aviation Safety Agency (EASA) AD 2022-0187,
dated September 13, 2022.
(ii) European Union Aviation Safety Agency (EASA) AD 2023-0015,
dated January 19, 2023.
(5) For EASA AD 2022-0187, EASA AD 2023-0015, and EASA AD 2024-
0011, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#6e2f2a1d2e0b0f1d0f400b1b1c011e0f400b1b"><span class="__cf_email__" data-cfemail="7130350231141002105f1404031e01105f1404">[email protected]</span></a>; website
easa.europa.eu. You may find these EASA ADs on the EASA website at
ad.easa.europa.eu.
[[Page 59857]]
(6) 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.
(7) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit <a href="/cdn-cgi/l/email-protection#d4e8b5f4bca6b1b2e9" http: www.archives.gov federal-register cfr ibr-locationsoremailfr.inspection@nara.gov">www.archives.gov/federal-register/cfr/<span class="__cf_email__" data-cfemail="f29b9080df9e9d9193869b9d9c819d80979f939b9e9480dc9b9c81829791869b9d9cb29c938093dc959d84">[email protected]</span></a>"><a href="http://www.archives.gov/federal-register/cfr/ibr-locationsoremailfr.inspection@nara.gov">www.archives.gov/federal-register/cfr/<span class="__cf_email__" data-cfemail="d8b1baaaf5b4b7bbb9acb1b7b6abb7aabdb5b9b1b4beaaf6b1b6aba8bdbbacb1b7b698b6b9aab9f6bfb7ae">[email protected]</span></a></a>.
Issued on July 16, 2024.
Peter A. White,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-15959 Filed 7-23-24; 8:45 am]
BILLING CODE 4910-13-P
</pre><script data-cfasync="false" src="/cdn-cgi/scripts/5c5dd728/cloudflare-static/email-decode.min.js"></script></body>
</html>Indexed from Federal Register on July 24, 2024.
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