Rule2022-19098
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
September 6, 2022
Effective
October 11, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is superseding Airworthiness Directive (AD) 2017-10- 24, which applied to certain Airbus SAS Model A330-200 series airplanes, Model A330-200 Freighter series airplanes, and Model A330- 300 series airplanes; AD 2018-23-14, which applied to certain Airbus SAS Model A330-200 series airplanes, Model A330-200 Freighter series airplanes, and Model A330-300 series airplanes; and AD 2021-05-12, which applied to certain Airbus SAS Model A330-200 Freighter series airplanes. AD 2017-10-24, AD 2018-23-14, and AD 2021-05-12 require 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 revises the applicability by adding airplanes. This AD continues to require the actions in AD 2018-23-14 and AD 2021-05-12, 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
<html>
<head>
<title>Federal Register, Volume 87 Issue 171 (Tuesday, September 6, 2022)</title>
</head>
<body><pre>
[Federal Register Volume 87, Number 171 (Tuesday, September 6, 2022)]
[Rules and Regulations]
[Pages 54355-54358]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-19098]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0601; Project Identifier MCAI-2021-01286-T;
Amendment 39-22152; AD 2022-18-01]
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) 2017-10-
24, which applied to certain Airbus SAS Model A330-200 series
airplanes, Model A330-200 Freighter series airplanes, and Model A330-
300 series airplanes; AD 2018-23-14, which applied to certain Airbus
SAS Model A330-200 series airplanes, Model A330-200 Freighter series
airplanes, and Model A330-300 series airplanes; and AD 2021-05-12,
which applied to certain Airbus SAS Model A330-200 Freighter series
airplanes. AD 2017-10-24, AD 2018-23-14, and AD 2021-05-12 require
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 revises the
applicability by adding airplanes. This AD continues to require the
actions in AD 2018-23-14 and AD 2021-05-12, 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 October 11, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 11,
2022.
The Director of the Federal Register approved the incorporation by
reference of certain other publications listed in this AD as of January
2, 2019 (83 FR 60754, November 27, 2018).
The Director of the Federal Register also approved the
incorporation by reference of a certain other publication listed in
this AD as of April 26, 2021 (86 FR 15092, March 22, 2021).
ADDRESSES: For EASA 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#1c5d586f5c797d6f7d3279696e736c7d327969"><span class="__cf_email__" data-cfemail="16575265567377657738736364796677387363">[email protected]</span></a>; internet
www.easa.europa.eu. You may find this IBR material on the EASA website
at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>. For Airbus service information identified
in this final rule, contact Airbus SAS, Airworthiness Office--EAL,
Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France, France;
telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email
<a href="/cdn-cgi/l/email-protection#d5b4bca7a2baa7a1bdbcbbb0a6a6fb94e6e6e5f894e6e1e595b4bca7b7a0a6fbb6bab8"><span class="__cf_email__" data-cfemail="c4a5adb6b3abb6b0acadaaa1b7b7ea85f7f7f4e985f7f0f484a5adb6a6b1b7eaa7aba9">[email protected]</span></a>; internet <a href="https://www.airbus.com">https://www.airbus.com</a>.
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> by
searching for and locating Docket No. FAA-2022-0601.
Examining the AD Docket
You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> by searching for
and locating Docket No. FAA-2022-0601; 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.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone and fax: 206-231-3229;
email <a href="/cdn-cgi/l/email-protection#c4b2a8a5a0ada9adb6eab1a8bda5aaabb284a2a5a5eaa3abb2"><span class="__cf_email__" data-cfemail="97e1fbf6f3fefafee5b9e2fbeef6f9f8e1d7f1f6f6b9f0f8e1">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0246, dated November 17, 2021
(EASA AD 2021-0246) (also referred to as the MCAI), to correct an
unsafe condition for all Airbus SAS Model A330-201, -202, -203, -223,
and -243 airplanes; Model A330-223F and -243F airplanes; Model A330-
301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes;
Model A330-841 airplanes; and Model A330-941 airplanes.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2017-10-24, Amendment 39-18898 (82 FR
24035, May 25, 2017) (AD 2017-10-24); AD 2018-23-14, Amendment 39-19501
(83 FR 60754, November 27, 2018) (AD 2018-23-14); and AD 2021-05-12,
Amendment 39-21455 (86 FR 15092, March 22, 2021) (AD 2021-05-12). AD
2017-10-24 applied to certain Airbus SAS Model A330-200 series
airplanes, Model A330-200 Freighter series airplanes, and Model A330-
300 series airplanes; AD 2018-23-14 applied to certain Airbus SAS Model
A330-200 series airplanes, Model A330-200 Freighter series airplanes,
and Model A330-300 series airplanes; and AD 2021-05-12 applied to
certain Airbus SAS Model A330-200 Freighter series airplanes. The NPRM
published in the Federal Register on June 9, 2022 (87 FR 35118). The
NPRM was prompted by a determination that new or more restrictive
airworthiness limitations are necessary. The NPRM proposed to revise
the applicability by adding
[[Page 54356]]
airplanes. The NPRM also proposed to continue to require the actions in
AD 2018-23-14 and AD 2021-05-12, and proposed to require revising the
existing maintenance or inspection program, as applicable, to
incorporate new or more restrictive airworthiness limitations, as
specified in EASA AD 2021-0246.
The FAA is issuing this AD to address fatigue cracking, accidental
damage, or corrosion in principal structural elements, and possible
failure of certain life limited parts, which could result in reduced
structural integrity of the airplane. See the MCAI for additional
background information.
Discussion of Final Airworthiness Directive
The FAA received comments from the Air Line Pilots Association,
International (ALPA) who supported the NPRM without change.
Conclusion
The FAA reviewed the relevant data, considered the comment
received, and determined that air safety requires adopting this AD as
proposed. 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. Accordingly, the FAA is issuing this AD to
address the unsafe condition on these products.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0246 specifies procedures for new or more restrictive
airworthiness limitations for airplane structures and safe life limits.
This AD also requires the following service information.
<bullet> Airbus A330 Airworthiness Limitations Section (ALS) Part
1, Safe Life Airworthiness Limitation Items (SL-ALI), Revision 09,
dated September 18, 2017, which the Director of the Federal Register
approved for incorporation by reference as of January 2, 2019 (83 FR
60754, November 27, 2018).
<bullet> Airbus A330 ALS Part 1, SL-ALI, Variation 9.2, dated
November 28, 2017, which the Director of the Federal Register approved
for incorporation by reference as of January 2, 2019 (83 FR 60754,
November 27, 2018).
<bullet> Airbus A330 ALS Part 1, SL-ALI, Variation 9.3, dated
November 29, 2017, which the Director of the Federal Register approved
for incorporation by reference as of January 2, 2019 (83 FR 60754,
November 27, 2018).
<bullet> EASA AD 2020-0190, dated August 27, 2020, which the
Director of the Federal Register approved for incorporation by
reference as of April 26, 2021 (86 FR 15092, March 22, 2021).
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 138 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 2018-23-14 and AD 2021-05-12 to be $7,650 (90 work-
hours x $85 per work-hour) per AD.
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) 2017-10-24, Amendment 39-18898
(82 FR 24035, May 25, 2017); AD 2018-23-14, Amendment 39-19501 (83 FR
60754, November 27, 2018); and AD 2021-05-12, Amendment 39-21455 (86 FR
15092, March 22, 2021); and
0
b. Adding the following new AD:
2022-18-01 Airbus SAS: Amendment 39-22152; Docket No. FAA-2022-0601;
Project Identifier MCAI-2021-01286-T.
(a) Effective Date
This airworthiness directive (AD) is effective October 11, 2022.
(b) Affected ADs
This AD replaces the ADs specified in paragraphs (b)(1) through
(3) of this AD.
(1) AD 2017-10-24, Amendment 39-18898 (82 FR 24035, May 25,
2017) (AD 2017-10-24).
(2) AD 2018-23-14, Amendment 39-19501 (83 FR 60754, November 27,
2018) (AD 2018-23-14).
(3) AD 2021-05-12, Amendment 39-21455 (86 FR 15092, March 22,
2021) (AD 2021-05-12).
(c) Applicability
This AD applies to the Airbus SAS airplanes specified 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 July 1,
2021.
(1) Model A330-201, -202, -203, -223, and -243 airplanes.
[[Page 54357]]
(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, or
corrosion in principal structural elements, and possible failure of
certain life limited parts, which 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
for AD 2018-23-14, With a New Terminating Action
This paragraph restates the requirements of paragraph (g) of AD
2018-23-14, with a new terminating action. For Airbus SAS Model
A330-200 series airplanes, Model A330-200 Freighter series
airplanes, and Model A330-300 series airplanes with an original
airworthiness certificate or original export certificate of
airworthiness issued on or before November 29, 2017: Within 90 days
after January 2, 2019 (the effective date of AD 2018-23-14), revise
the existing maintenance or inspection program, as applicable, to
incorporate the information specified in the service information
identified in paragraphs (g)(1) through (3) of this AD. The initial
compliance times for accomplishing the tasks are at the applicable
times specified in the service information identified in paragraphs
(g)(1) through (3) of this AD, or within 90 days after January 2,
2019, whichever occurs later. Accomplishing the revision of the
existing maintenance or inspection program required by paragraph (l)
of this AD terminates the requirements of this paragraph.
(1) Airbus A330 Airworthiness Limitations Section (ALS) Part 1,
Safe Life Airworthiness Limitation Items (SL-ALI), Revision 09,
dated September 18, 2017.
(2) Airbus A330 ALS Part 1, SL-ALI, Variation 9.2, dated
November 28, 2017.
(3) Airbus A330 ALS Part 1, SL-ALI, Variation 9.3, dated
November 29, 2017.
(h) Retained Restrictions on Alternative Actions and Intervals for AD
2018-23-14, With a New Exception
This paragraph restates the requirements of paragraph (i) of AD
2018-23-14, with a new exception. Except as required by paragraphs
(i) and (l) of this AD, after the existing maintenance or inspection
program, as applicable, has been revised as required by paragraph
(g) of this AD, no alternative actions (e.g., inspections) or
intervals may be used unless the actions or intervals are approved
as an alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (p)(1) of this AD.
(i) Retained Revision of the Existing Maintenance or Inspection Program
for AD 2021-05-12, With a New Terminating Action
This paragraph restates the requirements of paragraph (g) of AD
2021-05-12, with a new terminating action. For Airbus SAS Model
A330-223F and -243F airplanes with an original airworthiness
certificate or original export certificate of airworthiness issued
on or before June 29, 2020, except as specified in paragraph (j) of
this AD, comply with all required actions and compliance times
specified in, and in accordance with, EASA AD 2020-0190, dated
August 27, 2020 (EASA AD 2020-0190). Accomplishing the revision of
the existing maintenance or inspection program required by paragraph
(l) of this AD terminates the requirements of this paragraph.
(j) For AD 2021-05-12: Retained Exceptions to EASA AD 2020-0190 With No
Changes
This paragraph restates the exceptions specified in paragraph
(h) of AD 2021-05-12, with no changes.
(1) The requirements specified in paragraph (1) of EASA AD 2020-
0190 do not apply to this AD.
(2) Paragraph (2) of EASA AD 2020-0190 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, to incorporate the ``limitations'' specified in
paragraph (2) of EASA AD 2020-0190 within 90 days after April 26,
2021 (the effective date of AD 2021-05-12).
(3) The initial compliance time for doing the tasks specified in
paragraph (2) of EASA AD 2020-0190 is on or before the applicable
``limitations'' specified in paragraph (2) of EASA AD 2020-0190, or
within 90 days after April 26, 2021 (the effective date of AD 2021-
05-12), whichever occurs later.
(4) The provision specified in paragraph (3) of EASA AD 2020-
0190 does not apply to this AD.
(5) The ``Remarks'' section of EASA AD 2020-0190 does not apply
to this AD.
(k) Retained Restrictions on Alternative Actions and Intervals for AD
2021-05-12, With a New Exception
This paragraph restates the requirements of paragraph (i) of AD
2021-05-12, with a new exception. Except as required by paragraph
(l) of this AD, after the existing maintenance or inspection program
has been revised as required by paragraph (i) of this AD, no
alternative actions (e.g., inspections) or intervals are allowed
unless they are approved as specified in the provisions of the
``Ref. Publications'' section of EASA AD 2020-0190.
(l) New Revision of the Existing Maintenance or Inspection Program
Except as specified in paragraph (m) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2021-0246, dated November 17, 2021 (EASA AD 2021-0246).
Accomplishing the revision of the existing maintenance or inspection
program required by this paragraph terminates the requirements of
paragraphs (g) and (i) of this AD.
(m) Exceptions to EASA AD 2021-0246
(1) Where EASA AD 2021-0246 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The requirements specified in paragraph (1) of EASA AD 2021-
0246 do not apply to this AD.
(3) Paragraph (2) of EASA AD 2021-0246 specifies revising ``the
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.
(4) The initial compliance time for doing the tasks specified in
paragraph (2) of EASA 2021-0246 is at the applicable ``limitations''
as incorporated by the requirements of paragraph (2) of EASA AD
2021-0246, or within 90 days after the effective date of this AD,
whichever occurs later.
(5) The provisions specified in paragraphs (3) and (4) of EASA
AD 2021-0246 do not apply to this AD.
(6) The ``Remarks'' section of EASA AD 2021-0246 does not apply
to this AD.
(n) New Provisions for Alternative Actions and Intervals
After the existing maintenance or inspection program has been
revised as required by paragraph (l) 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 2021-0246.
(o) Terminating Action for Certain Requirements of Paragraph (g) of
This AD
Accomplishing the actions required by paragraph (i) of this AD
terminates the limitation for the nose landing gear lower torque
link having part number D64001, as required by paragraph (g) of AD
2018-23-14, for Model A330-223F and -243F airplanes only.
(p) Additional FAA 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, International Validation Branch, send it
to the attention of the person identified in paragraph (q) of this
AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#8fb6a2ced9dca2cec6dda2b8bcbfa2cec2c0cccfe9eeeea1e8e0f9"><span class="__cf_email__" data-cfemail="93aabed2c5c0bed2dac1bea4a0a3bed2dedcd0d3f5f2f2bdf4fce5">[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
[[Page 54358]]
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.
(q) Related Information
For more information about this AD, contact Vladimir Ulyanov,
Aerospace Engineer, Large Aircraft Section, FAA, International
Validation Branch, 2200 South 216th St., Des Moines, WA 98198;
telephone and fax: 206-231-3229; email <a href="/cdn-cgi/l/email-protection#83f5efe2e7eaeeeaf1adf6effae2edecf5c3e5e2e2ade4ecf5"><span class="__cf_email__" data-cfemail="bbcdd7dadfd2d6d2c995ced7c2dad5d4cdfbdddada95dcd4cd">[email protected]</span></a>.
(r) 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.
(3) The following service information was approved for IBR on
October 11, 2022.
(i) European Union Aviation Safety Agency (EASA) AD 2021-0246,
dated November 17, 2021.
(ii) [Reserved]
(4) The following service information was approved for IBR on
January 2, 2019 (83 FR 60754, November 27, 2018).
(i) Airbus A330 Airworthiness Limitations Section (ALS) Part 1,
Safe Life Airworthiness Limitation Items (SL-ALI), Revision 09,
dated September 18, 2017.
(ii) Airbus A330 ALS Part 1, SL-ALI, Variation 9.2, dated
November 28, 2017.
(iii) Airbus A330 ALS Part 1, SL-ALI, Variation 9.3, dated
November 29, 2017.
(5) The following service information was approved for IBR on
April 26, 2021 (86 FR 15092, March 22, 2021).
(i) European Union Aviation Safety Agency (EASA) AD 2020-0190,
dated August 27, 2020.
(ii) [Reserved]
(6) For EASA AD 2020-0190 and EASA AD 2021-0246, contact EASA,
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
8999 000; email <a href="/cdn-cgi/l/email-protection#f0b1b483b095918391de9585829f8091de9585"><span class="__cf_email__" data-cfemail="8ccdc8ffcce9edffeda2e9f9fee3fceda2e9f9">[email protected]</span></a>; internet www.easa.europa.eu. You
may find this EASA AD on the EASA website at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>. For Airbus service information identified in this
AD, contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile
Dewoitine No: 2, 31700 Blagnac Cedex, France, France; telephone +33
5 61 93 36 96; fax +33 5 61 93 45 80; email <a href="/cdn-cgi/l/email-protection#57363e25203825233f3e3932242479166464677a1664636717363e253522247934383a"><span class="__cf_email__" data-cfemail="32535b40455d40465a5b5c5741411c730101021f7301060272535b405047411c515d5f">[email protected]</span></a>; internet <a href="https://www.airbus.com">https://www.airbus.com</a>.
(7) 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.
(8) 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#fa9c88d49394898a9f998e939594ba949b889bd49d958c"><span class="__cf_email__" data-cfemail="d5b3a7fbbcbba6a5b0b6a1bcbabb95bbb4a7b4fbb2baa3">[email protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.
Issued on August 16, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-19098 Filed 9-2-22; 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 September 6, 2022.
This is legal information, not legal advice. Laws vary by jurisdiction and change frequently. Always verify current law with official sources and consult a licensed attorney in your jurisdiction for advice on your specific situation.