Rule2024-25980
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
November 12, 2024
Effective
December 17, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2023-21- 02, which applied 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 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD was prompted by a determination that new or more restrictive airworthiness limitations are necessary. This AD continues to require certain actions in AD 2023- 21-02 and 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.
Full Text
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<title>Federal Register, Volume 89 Issue 218 (Tuesday, November 12, 2024)</title>
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[Federal Register Volume 89, Number 218 (Tuesday, November 12, 2024)]
[Rules and Regulations]
[Pages 88881-88884]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-25980]
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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;
Amendment 39-22873; AD 2024-22-02]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-21-
02, which applied 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 required revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive airworthiness limitations. This AD was prompted by a
determination that new or more restrictive airworthiness limitations
are necessary. This AD continues to require certain actions in AD 2023-
21-02 and 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 December 17, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 17,
2024.
The Director of the Federal Register approved the incorporation by
reference of certain other publications listed in this AD as of
December 11, 2023 (88 FR 76107, November 6, 2023).
ADDRESSES:
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 final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
<bullet> For EASA material identified in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999
000; email <a href="/cdn-cgi/l/email-protection#8dccc9fecde8ecfeeca3e8f8ffe2fdeca3e8f8"><span class="__cf_email__" data-cfemail="92d3d6e1d2f7f3e1f3bcf7e7e0fde2f3bcf7e7">[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, 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,
[[Page 88882]]
Suite 410, Westbury, NY 11590; telephone 206-231-3229; email
<a href="/cdn-cgi/l/email-protection#a7d1cbc6c3cecaced589d2cbdec6c9c8d1e7c1c6c689c0c8d1"><span class="__cf_email__" data-cfemail="97e1fbf6f3fefafee5b9e2fbeef6f9f8e1d7f1f6f6b9f0f8e1">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2023-21-02, Amendment 39-22574 (88 FR
76107, November 6, 2023) (AD2023-21-02). AD 2023-21-02 applied to
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 required revising the existing maintenance or
inspection program, as applicable, to incorporate 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.
The NPRM published in the Federal Register on July 24, 2024 (89 FR
59853). The NPRM was prompted by AD 2024-0011, dated January 10, 2024
(EASA AD 2024-0011) (also referred to as the MCAI), issued by EASA,
which is the Technical Agent for the Member States of the European
Union. The MCAI states that new or more restrictive airworthiness
limitations have been developed.
In the NPRM, the FAA proposed to continue to require certain
actions in AD 2023-21-02 and to require revising the existing
maintenance or inspection program, as applicable, to incorporate new or
more restrictive airworthiness limitations, as specified in EASA AD
2024-0011. The FAA is issuing this AD to address the unsafe condition
on these products.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-1894.
Discussion of Final Airworthiness Directive
Comments
The FAA received a comment from Air Line Pilots Association,
International (ALPA), who supported the NPRM without change.
Conclusion
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 reviewed the relevant data, considered the
comment received, and determined that air safety requires adopting this
AD as proposed. Accordingly, the FAA is issuing this AD to address the
unsafe condition on this product. Except for minor editorial changes,
this AD is adopted as proposed in the NPRM. None of the changes will
increase the economic burden on any operator.
Material Incorporated by Reference Under 1 CFR Part 51
EASA AD 2024-0011, dated January 10, 2024, specifies new or more
restrictive airworthiness limitations for airplane structures.
This AD also requires EASA AD 2022-0187, dated September 13, 2022,
and EASA AD 2023-0015, dated January 19, 2023, 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 the ADDRESSES section.
Costs of Compliance
The FAA estimates that this AD affects 126 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this 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 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
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,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will 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 Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by:
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:
2024-22-02 Airbus SAS: Amendment 39-22873; Docket No. FAA-2024-1894;
Project Identifier MCAI-2024-00036-T.
(a) Effective Date
This airworthiness directive (AD) is effective December 17,
2024.
[[Page 88883]]
(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.
(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 a
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#d3929e9c9093b5b2b2fdb4bca5"><span class="__cf_email__" data-cfemail="cf8e82808c8fa9aeaee1a8a0b9">[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#a5d3c9c4c1ccc8ccd78bd0c9dcc4cbcad3e5c3c4c48bc2cad3"><span class="__cf_email__" data-cfemail="6f19030e0b0602061d411a03160e0100192f090e0e41080019">[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 December 17,
2024.
(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).
[[Page 88884]]
(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#81c0c5f2c1e4e0f2e0afe4f4f3eef1e0afe4f4"><span class="__cf_email__" data-cfemail="2362675063464250420d4656514c53420d4656">[email protected]</span></a>; website
easa.europa.eu. You may find these EASA ADs on the EASA website at
ad.easa.europa.eu.
(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#023e63226a7067643f" http: www.archives.gov federal-register cfr ibr-locationsoremailfr.inspection@nara.gov">www.archives.gov/federal-register/cfr/<span class="__cf_email__" data-cfemail="d3bab1a1febfbcb0b2a7babcbda0bca1b6beb2babfb5a1fdbabda0a3b6b0a7babcbd93bdb2a1b2fdb4bca5">[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="046d667629686b6765706d6b6a776b766169656d6862762a6d6a77746167706d6b6a446a6576652a636b72">[email protected]</span></a></a>.
Issued on October 23, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-25980 Filed 11-8-24; 8:45 am]
BILLING CODE 4910-13-P
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