Rule2022-26356
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 5, 2022
Effective
January 9, 2023
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A321-251N, A321-251NX, A321-252N, A321-252NX, A321- 253N, and A321-253NX airplanes. This AD was prompted by a stress analysis on the engine structure that indicated that the fail-safe lug may not be able to sustain, during one inspection interval as currently specified in an airworthiness limitations item, the loads deriving from the engagement of the secondary load path within that inspection interval for the aft engine mount system. This AD requires repetitive detailed inspections of the aft engine mount and secondary load path clearance fail-safe pin and replacement of the engine if necessary, 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 232 (Monday, December 5, 2022)</title>
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[Federal Register Volume 87, Number 232 (Monday, December 5, 2022)]
[Rules and Regulations]
[Pages 74294-74296]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-26356]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1155; Project Identifier MCAI-2022-00655-T;
Amendment 39-22243; AD 2022-24-03]
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 adopting a new airworthiness directive (AD) for all
Airbus SAS Model A321-251N, A321-251NX, A321-252N, A321-252NX, A321-
253N, and A321-253NX airplanes. This AD was prompted by a stress
analysis on the engine structure that indicated that the fail-safe lug
may not be able to sustain, during one inspection interval as currently
specified in an airworthiness limitations item, the loads deriving from
the engagement of the secondary load path within that inspection
interval for the aft engine mount system. This AD requires repetitive
detailed inspections of the aft engine mount and secondary load path
clearance fail-safe pin and replacement of the engine if necessary, 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 January 9, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 9,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2022-1155; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket
[[Page 74295]]
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 material incorporated by reference 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#b2f3f6c1f2d7d3c1d39cd7c7c0ddc2d39cd7c7"><span class="__cf_email__" data-cfemail="fcbdb88fbc999d8f9dd299898e938c9dd29989">[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 in the AD docket at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2022-1155.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, Large
Aircraft Section, International Validation Branch, FAA, 2200 South
216th Street Des Moines, WA 98198; telephone 206-231-3225; email
<a href="/cdn-cgi/l/email-protection#8ce8ede2a2fee3e8e5e2edcceaededa2ebe3fa"><span class="__cf_email__" data-cfemail="9efafff0b0ecf1faf7f0ffdef8ffffb0f9f1e8">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to all Airbus SAS Model
A321-251N, A321-251NX, A321-252N, A321-252NX, A321-253N, and A321-253NX
airplanes. The NPRM published in the Federal Register on September 12,
2022 (87 FR 55737). The NPRM was prompted by AD 2022-0089, dated May
17, 2022, issued by EASA, which is the Technical Agent for the Member
States of the European Union (referred to after this as the MCAI). The
MCAI states that the engine fail safe lug may not be able to sustain,
during one inspection interval as currently specified in airworthiness
limitation item (ALI) task 712232-01-1, the loads deriving from the
engagement of the secondary load path. This condition, if not detected
and corrected, could lead to engine mount rupture, possibly resulting
in engine loss during flight and loss of control of the airplane.
In the NPRM, the FAA proposed to require repetitive detailed
inspections of the aft engine mount and secondary load path clearance
fail-safe pin and replacement of the engine if necessary, as specified
in EASA AD 2022-0089. 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-2022-1155.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from Air Line Pilots Association,
International (ALPA) and an anonymous commenter. Both commenters
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
comments 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.
Related Service Information Under 1 CFR Part 51
EASA AD 2022-0089 specifies procedures for repetitive detailed
inspections (DET) for discrepancies of the aft engine mount and
secondary load path clearance fail-safe pin for each engine, and
replacement of any engine with discrepant findings on the secondary
load path clearance check.
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 156 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Labor cost Parts cost Cost per product Cost on U.S. operators
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Up to 4 work-hours x $85 per hour = $340 $0 Up to $340................ Up to $53,040.
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The FAA estimates that it would take 64 work-hours (at $85 per
work-hour) to replace an engine, if required based on the results of
any required actions. The FAA has received no definitive data on which
to base the estimate for the cost of a replacement engine or any
necessary additional on-condition actions that would be required by
this AD. The FAA has no way of determining the number of aircraft that
might need these on-condition actions.
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
[[Page 74296]]
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 adding the following new airworthiness
directive:
2022-24-03 Airbus SAS: Amendment 39-22243; Docket No. FAA-2022-1155;
Project Identifier MCAI-2022-00655-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 9, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Airbus SAS Model A321-251N, A321-251NX,
A321-252N, A321-252NX, A321-253N, and A321-253NX airplanes,
certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 71, Powerplant.
(e) Unsafe Condition
This AD was prompted by a stress analysis on the engine
structure that indicated that the fail-safe lug may not be able to
sustain, during one inspection interval, as currently specified in
airworthiness limitation item (ALI) task 712232-01-1, the loads
deriving from the engagement of the secondary load path within that
inspection interval for the aft engine mount system. The FAA is
issuing this AD to address potential failure of the LEAP-1A aft
engine mount waiting fail-safe male lug, which could lead to engine
mount rupture, possibly resulting in engine loss during flight and
loss of control 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
2022-0089, dated May 17, 2022 (EASA AD 2022-0089).
(h) Exceptions to EASA AD 2022-0089
(1) Where paragraph (3) of EASA AD 2022-0089 specifies
corrective action if ``discrepancies are detected, as defined in the
SB,'' for purposes of this AD, discrepancies include a fail-safe pin
that does not rotate freely, or has damage (dents, scratches, nicks,
corrosion, or cracks).
(2) The ``Remarks'' section of EASA AD 2022-0089 does not apply
to this AD.
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, 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, International Validation
Branch, send it to the attention of the person identified in
paragraph (j) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#c2fbef839491ef838b90eff5f1f2ef838f8d8182a4a3a3eca5adb4"><span class="__cf_email__" data-cfemail="b58c98f4e3e698f4fce79882868598f4f8faf6f5d3d4d49bd2dac3">[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, Large Aircraft
Section, 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.
(j) Additional Information
For more information about this AD, contact Dan Rodina,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA, 2200 South 216th Street, Des Moines, WA 98198;
telephone 206-231-3225; email <a href="/cdn-cgi/l/email-protection#2440454a0a564b404d4a45644245450a434b52"><span class="__cf_email__" data-cfemail="e286838ccc908d868b8c83a2848383cc858d94">[email protected]</span></a>.
(k) 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 2022-0089,
dated May 17, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0089, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#3170754271545042501f5444435e41501f5444"><span class="__cf_email__" data-cfemail="86c7c2f5c6e3e7f5e7a8e3f3f4e9f6e7a8e3f3">[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#0f697d2166617c7f6a6c7b6660614f616e7d6e21686079"><span class="__cf_email__" data-cfemail="3254401c5b5c41425751465b5d5c725c5340531c555d44">[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 9, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-26356 Filed 12-2-22; 8:45 am]
BILLING CODE 4910-13-P
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