Rule2022-27686
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
December 22, 2022
Effective
January 6, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
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 maintenance requirements and airworthiness tasks are necessary. This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness tasks, 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 87 Issue 245 (Thursday, December 22, 2022)</title>
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[Federal Register Volume 87, Number 245 (Thursday, December 22, 2022)]
[Rules and Regulations]
[Pages 78524-78527]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-27686]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1569; Project Identifier MCAI-2022-01267-T;
Amendment 39-22267; AD 2022-25-11]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; request for comments.
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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 maintenance requirements and
airworthiness tasks are necessary. This AD requires revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness tasks, 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 becomes effective January 6, 2023.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of January 6,
2023.
The FAA must receive comments on this AD by February 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:
<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-2022-1569; 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
[[Page 78525]]
other information. The street address for Docket Operations is listed
above.
Material Incorporated by Reference:
<bullet> For material incorporated by reference (IBR) 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#eeafaa9dae8b8f9d8fc08b9b9c819e8fc08b9b"><span class="__cf_email__" data-cfemail="ffbebb8cbf9a9e8c9ed19a8a8d908f9ed19a8a">[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 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. It is also available at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-1569.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, Large
Aircraft Section, FAA, International Validation Branch, 2200 South
216th St., Des Moines, WA 98198; telephone (206) 231-3225; email
<a href="/cdn-cgi/l/email-protection#5034313e7e223f34393e31103631317e373f26"><span class="__cf_email__" data-cfemail="bfdbded191cdd0dbd6d1deffd9dede91d8d0c9">[email protected]</span></a>.
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-2022-1569; Project Identifier MCAI-
2022-01267-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
<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 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, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone (206) 231-3225; email <a href="/cdn-cgi/l/email-protection#ed898c83c39f828984838cad8b8c8cc38a829b"><span class="__cf_email__" data-cfemail="7216131c5c001d161b1c13321413135c151d04">[email protected]</span></a>. Any commentary that
the FAA receives which is not specifically designated as CBI will be
placed in the public docket for this rulemaking.
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2022-0193, dated September 23, 2022
(EASA AD 2022-0193) (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 tasks related to the center fuselage are necessary to
address fatigue cracking, damage, or corrosion in principal structural
elements. EASA AD 2022-0193 specifies that it requires tasks
(limitations) already in Airbus A310 Airworthiness Limitations Section
(ALS), Part 2, Damage Tolerant Airworthiness Limitation Items (DT-ALI),
Revision 03, dated December 14, 2018, that is required by EASA AD 2019-
0091 (which corresponds to FAA AD 2019-20-06, Amendment 39-19759 (84 FR
55859, October 18, 2019) (AD 2019-20-06)), and that incorporation of
EASA AD 2022-0193 invalidates (terminates) prior instructions for those
tasks. This AD therefore terminates the limitations for the
corresponding tasks, as required by paragraph (g) of AD 2019-20-06.
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 effects of aging on airplane systems. Such
effects could change system characteristics, leading to an increased
potential for failure of certain life-limited parts. See the MCAI for
additional background information.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-1569.
Related Service Information Under 1 CFR part 51
EASA AD 2022-0193 describes new or more restrictive airworthiness
tasks for airplane structure (center fuselage). 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
described 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.
Requirements of This AD
This AD requires revising the existing maintenance or inspection
program, as applicable, to incorporate new or more restrictive
airworthiness tasks, which are specified in EASA AD 2022-0193 described
previously, as incorporated by reference. Any differences with EASA AD
2022-0193 are identified as exceptions in the regulatory text of this
AD.
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 2022-0193
[[Page 78526]]
is incorporated by reference in this AD. This AD requires compliance
with EASA AD 2022-0193 in its entirety through that incorporation,
except for any differences identified as exceptions in the regulatory
text of this AD. Using common terms that are the same as the heading of
a particular section in EASA AD 2022-0193 does not mean that operators
need comply only with that section. For example, where the AD
requirement refers to ``all required actions and compliance times,''
compliance with this AD requirement is not limited to the section
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2022-
0193. Service information required by EASA AD 2022-0193 for compliance
will be available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-1569
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 AD 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.
FAA's Justification and Determination of the Effective Date
Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
There are currently no domestic operators of these products.
Accordingly, notice and opportunity for prior public comment are
unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the
foregoing 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 workhour).
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866, and
(2) Will not affect intrastate aviation in Alaska.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
2022-25-11 Airbus SAS: Amendment 39-22267; Docket No. FAA-2022-1569;
Project Identifier MCAI-2022-01267-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 6, 2023.
(b) Affected ADs
This AD affects AD 2019-20-06, Amendment 39-19759 (84 FR 55859,
October 18, 2019) (AD 2019-20-06).
[[Page 78527]]
(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 tasks are necessary. The FAA is issuing
this AD to address fatigue cracking, damage, or corrosion in
principal 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) 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
2022-0193, dated September 23, 2022 (EASA AD 2022-0193).
(h) Exceptions to EASA AD 2022-0193
(1) The requirements specified in paragraphs (1) and (2) of EASA
AD 2022-0193 do not apply to this AD.
(2) Paragraph (3) of EASA AD 2022-0193 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 (1) of EASA AD 2022-0193 is at the applicable ``associated
thresholds'' as incorporated by the requirements of paragraph (3) of
EASA AD 2022-0193, or within 90 days after the effective date of
this AD, whichever occurs later.
(4) The provisions specified in paragraph (4) of EASA AD 2022-
0193 do not apply to this AD.
(5) This AD does not adopt the ``Remarks'' paragraph of EASA AD
2022-0193.
(i) Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and intervals are allowed unless they
are approved as specified in the provisions of the ``Ref.
Publications'' section of EASA AD 2022-0193.
(j) Terminating Action for AD 2019-20-06
Accomplishing the actions required by this AD terminates the
corresponding requirements of AD 2019-20-06 only for the tasks
identified in the service information referenced in EASA AD 2022-
0193.
(k) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, 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 Large Aircraft Section, send it to the attention of the person
identified in paragraph (l) of this AD. Information may be emailed
to: <a href="/cdn-cgi/l/email-protection#f2cbdfb3a4a1dfb3bba0dfc5c1c2dfb3bfbdb1b2949393dc959d84"><span class="__cf_email__" data-cfemail="4d74600c1b1e600c041f607a7e7d600c00020e0d2b2c2c632a223b">[email protected]</span></a>. 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 (k)(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.
(l) Additional Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone (206) 231-3225; email <a href="/cdn-cgi/l/email-protection#f195909fdf839e95989f90b1979090df969e87"><span class="__cf_email__" data-cfemail="4e2a2f20603c212a27202f0e282f2f60292138">[email protected]</span></a>.
(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 2022-0193,
dated September 23, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0193, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#ffbebb8cbf9a9e8c9ed19a8a8d908f9ed19a8a"><span class="__cf_email__" data-cfemail="a6e7e2d5e6c3c7d5c788c3d3d4c9d6c788c3d3">[email protected]</span></a>; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(4) 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.
(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
<a href="/cdn-cgi/l/email-protection#f79185d99e9984879294839e9899b799968596d9909881"><span class="__cf_email__" data-cfemail="096f7b2760677a796c6a7d6066674967687b68276e667f">[email protected]</span></a>, or go to: <a href="http://www.archives.gov/federal-register/cfr/ibr-locations.html">www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on November 29, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-27686 Filed 12-21-22; 8:45 am]
BILLING CODE 4910-13-P
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