Published 2023-04-07 · Federal Register document 2023-07095
Airworthiness Directives; Airbus SAS Airplanes
Publication summary
The FAA is superseding Airworthiness Directive (AD) 2020-21- 07, which applied to all Airbus SAS Model A350-941 and -1041 airplanes. AD 2020-21-07 required replacement of affected passenger oxygen masks (which includes re-identifying the parts). This AD was prompted by a determination that additional parts are subject to the unsafe condition. This AD continues to require the actions in AD 2020-21-07, and also requires replacing additional affected parts; as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference. This AD also prohibits installation of affected parts. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[98]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-05-07
- Effective date printed in this edition
- 2023-05-12
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective May 12, 2023.
Exact source excerpt. Text positions 10230–10316, end exclusive, in the original decoded publication. SHA-256: 2cbc8c6c8df0595e73f9c96d6cb4abcc3542104099303edd1985827ac2e8e4bd
Affected ADs
(b) Affected ADs
This AD replaces AD 2020-21-07, Amendment 39-21280 (85 FR 64949,
October 14, 2020) (AD 2020-21-07).
Exact source excerpt. Text positions 10316–10440, end exclusive, in the original decoded publication. SHA-256: 108034eb24ec428493bf79d95678815fb7f5b27b0b45c13a41fd142c70c348d9
Applicability wording · Applicability
(c) Applicability
This AD applies to all Airbus SAS Model A350-941 and -1041
airplanes, certificated in any category.
Exact source excerpt. Text positions 10440–10565, end exclusive, in the original decoded publication. SHA-256: b8809250b937f40e871dbcc174b1bccd06ceae21327c6080f47df821013d024a
Subject
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
Exact source excerpt. Text positions 10565–10643, end exclusive, in the original decoded publication. SHA-256: beebdc11ca55a698e6bba23e8dc2d9b64bbafa16f2e35342201f0a7331ad0a62
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report that sticking effects have been
observed affecting the breathing bag on certain passenger oxygen
masks, and by a determination that additional parts are subject to
the unsafe condition. The FAA is issuing this AD to address sticking
of the breathing bag on certain passenger oxygen masks. The unsafe
condition, if not addressed, could prevent the breathing bag from
fully inflating, and possibly injure cabin occupants following a
depressurization event.
Exact source excerpt. Text positions 10643–11165, end exclusive, in the original decoded publication. SHA-256: 425deae38adb756e0e4ecb48ff7b26a44eb02da1bd8834f560ae99e9fa99f8f9
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11165–11267, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Requirements
(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
2022-0112, dated June 17, 2022 (EASA AD 2022-0112).
Exact source excerpt. Text positions 11267–11534, end exclusive, in the original decoded publication. SHA-256: f72cd20ee8ba30fd02b24fb4f7e5e5a7b8c22626f9ec240c877c1b5de1fb691f
Exceptions to EASA AD 2022-0112
(h) Exceptions to EASA AD 2022-0112
(1) Where EASA AD 2022-0112 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2022-0112 does not apply
to this AD.
(3) Where EASA AD 2022-0112 specifies to do the replacement and
re-identification specified in Airbus Service Bulletin A350-35-P013,
Revision 02, dated March 8, 2022, which specifies to inspect for the
part number and serial number and then do a replacement; this AD
only requires the replacement and re-identification.
(4) Where service information identified in EASA AD 2022-0112
specifies to do an inspection for the date of manufacture of the
affected part, this AD does not require that inspection.
(5) Where Table 3 of EASA AD 2022-0112 specifies a compliance
time for airplanes on which ``the SB'' has not been embodied, for
this AD the compliance time for those airplanes is ``before
exceeding 72 months since airplane date of manufacture or within 30
days after the effective date of this AD, whichever occurs later.''
Exact source excerpt. Text positions 11534–12620, end exclusive, in the original decoded publication. SHA-256: 9423aa73cee8452ca5e9970c560c430272ae8f550b2597a3f22c08908dbf2e03
Additional AD Provisions
(i) Additional AD Provisions
The following provisions also apply to this AD:
[[Page 20732]]
(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 International
Validation Branch, send it to the attention of the person identified
in paragraph (j) 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.
(3) Required for Compliance (RC): Except as required by
paragraph (i)(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.
Exact source excerpt. Text positions 12620–14561, end exclusive, in the original decoded publication. SHA-256: 993a835361bc27a34f0c88b19d27d1c5af86766107e4d92fbb9c399a12b16412
Additional Information
(j) Additional Information
For more information about this AD, contact Dat Le, Aerospace
Engineer, Large Aircraft Section, FAA, International Validation
Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 516-
228-7317; email [email protected].
Exact source excerpt. Text positions 14561–14824, end exclusive, in the original decoded publication. SHA-256: d11618a25c111a360576c92035ea0a339c7a7de0fa8e14e00b243f4a3ace5c2f
Material Incorporated by Reference
(k) 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 2022-0112,
dated June 17, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0112, 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 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
[email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 14824–16055, end exclusive, in the original decoded publication. SHA-256: 61a33fd2ccd9f93e1c6e520edc93978c8d426ab8e5348211f7b1941ebc8e9a6c
Explicit historical replacement wording
Find all recorded historical references to AD 2023-05-07 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 65df148eb548c01e66a6cecb7274ea409757fcf48c1b84d243a0ca42e47372b5. Source manifest: 513e2d76219be39cc976c2205af9fea5c21ca2a4fc0d84de474c48180ccf053b.
Official source · 2023-04-07
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 88, Number 67 (Friday, April 7, 2023)]
[Rules and Regulations]
[Pages 20730-20732]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-07095]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1643; Project Identifier MCAI-2022-00799-T;
Amendment 39-22376; AD 2023-05-07]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2020-21-
07, which applied to all Airbus SAS Model A350-941 and -1041 airplanes.
AD 2020-21-07 required replacement of affected passenger oxygen masks
(which includes re-identifying the parts). This AD was prompted by a
determination that additional parts are subject to the unsafe
condition. This AD continues to require the actions in AD 2020-21-07,
and also requires replacing additional affected parts; as specified in
a European Union Aviation Safety Agency (EASA) AD, which is
incorporated by reference. This AD also prohibits installation of
affected parts. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective May 12, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of May 12,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1643; 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 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 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
regulations.gov under Docket No. FAA-2022-1643.
FOR FURTHER INFORMATION CONTACT: Dat Le, Aerospace Engineer, Large
Aircraft Section, FAA, International Validation Branch, 2200 South
216th St., Des Moines, WA 98198; telephone 516-228-7317; email
[email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2020-21-07, Amendment 39-21280 (85 FR
64949, October 14, 2020) (AD 2020-21-07). AD 2020-21-07 applied to all
Airbus SAS Model A350-941 and -1041 airplanes. AD 2020-21-07 required
replacement of affected passenger oxygen masks (which includes re-
identifying the parts). The FAA issued AD 2020-21-07 to address
sticking of the breathing bag on certain passenger oxygen masks, which
could prevent the breathing bag from fully inflating, and possibly
injure cabin occupants following a depressurization event.
The NPRM published in the Federal Register on December 22, 2022 (87
FR 78612). The NPRM was prompted by AD 2022-0112, dated June 17, 2022,
issued by EASA, which is the Technical Agent for the Member States of
the European Union (EASA AD 2022-0112) (referred to after this as the
MCAI). The MCAI states that additional affected parts (emergency
passenger oxygen container assembly having serial number BEHJ-XXXX)
have been identified as being subject to the same unsafe condition.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1643.
In the NPRM, the FAA proposed to continue to require the actions in
AD 2020-21-07 and to require replacing additional affected parts, as
specified in EASA AD 2022-0112. The NPRM also proposed to prohibit the
installation of affected parts. The FAA is issuing this AD to address
sticking of the breathing bag on certain passenger oxygen masks, which
could prevent the breathing bag from fully inflating, and possibly
injure cabin occupants following a depressurization event.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Additional Changes Made to This Final Rule
Since the NPRM was published, the FAA received a parts cost
estimate for the passenger oxygen masks. The FAA has revised the Costs
of Compliance section of this final rule to include this parts cost.
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 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, and any other changes described
previously, 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 2022-0112 specifies procedures for replacing the affected
passenger oxygen masks (those passenger oxygen masks contained in each
affected emergency passenger oxygen container assembly), and re-
identifying each affected part. EASA AD
[[Page 20731]]
2022-0112 also prohibits the installation of affected parts.
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 30 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Retained actions from AD 2020-21- 6 work-hours x $85 Up to $4,250 (per $4,760 $61,880
07 (13 airplanes). per hour = $510. mask assembly).
New actions....................... 6 work-hours x $85 Up to $4,250 (per 4,760 142,800
per hour = $510. mask assembly).
----------------------------------------------------------------------------------------------------------------
According to the manufacturer, some or all of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all known costs
in the cost estimate.
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) 2020-21-07, Amendment 39-21280
(85 FR 64949, October 14, 2020); and
0
b. Adding the following new AD:
2023-05-07 Airbus SAS: Amendment 39-22376; Docket No. FAA-2022-1643;
Project Identifier MCAI-2022-00799-T.
(a) Effective Date
This airworthiness directive (AD) is effective May 12, 2023.
(b) Affected ADs
This AD replaces AD 2020-21-07, Amendment 39-21280 (85 FR 64949,
October 14, 2020) (AD 2020-21-07).
(c) Applicability
This AD applies to all Airbus SAS Model A350-941 and -1041
airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Unsafe Condition
This AD was prompted by a report that sticking effects have been
observed affecting the breathing bag on certain passenger oxygen
masks, and by a determination that additional parts are subject to
the unsafe condition. The FAA is issuing this AD to address sticking
of the breathing bag on certain passenger oxygen masks. The unsafe
condition, if not addressed, could prevent the breathing bag from
fully inflating, and possibly injure cabin occupants following a
depressurization event.
(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
2022-0112, dated June 17, 2022 (EASA AD 2022-0112).
(h) Exceptions to EASA AD 2022-0112
(1) Where EASA AD 2022-0112 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2022-0112 does not apply
to this AD.
(3) Where EASA AD 2022-0112 specifies to do the replacement and
re-identification specified in Airbus Service Bulletin A350-35-P013,
Revision 02, dated March 8, 2022, which specifies to inspect for the
part number and serial number and then do a replacement; this AD
only requires the replacement and re-identification.
(4) Where service information identified in EASA AD 2022-0112
specifies to do an inspection for the date of manufacture of the
affected part, this AD does not require that inspection.
(5) Where Table 3 of EASA AD 2022-0112 specifies a compliance
time for airplanes on which ``the SB'' has not been embodied, for
this AD the compliance time for those airplanes is ``before
exceeding 72 months since airplane date of manufacture or within 30
days after the effective date of this AD, whichever occurs later.''
(i) Additional AD Provisions
The following provisions also apply to this AD:
[[Page 20732]]
(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 International
Validation Branch, send it to the attention of the person identified
in paragraph (j) 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.
(3) Required for Compliance (RC): Except as required by
paragraph (i)(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.
(j) Additional Information
For more information about this AD, contact Dat Le, Aerospace
Engineer, Large Aircraft Section, FAA, International Validation
Branch, 2200 South 216th St., Des Moines, WA 98198; telephone 516-
228-7317; email [email protected].
(k) 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 2022-0112,
dated June 17, 2022.
(ii) [Reserved]
(3) For EASA AD 2022-0112, 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 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
[email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on March 5, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-07095 Filed 4-6-23; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.