Proposed Rule2022-12406
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
June 10, 2022
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to supersede Airworthiness Directive (AD) 2017-10-17, which applies to certain Airbus SAS Model A330-200; A330- 200 Freighter; and A330-300 series airplanes. AD 2017-10-17 requires revising the existing maintenance or inspection program, as applicable, to incorporate new fuel airworthiness limitations. Since the FAA issued AD 2017-10-17, the FAA has determined that new or more restrictive fuel airworthiness limitations and tasks are necessary. This proposed AD would continue to require the actions in AD 2017-10-17 and require revising the existing maintenance or inspection program, as applicable, to incorporate additional new or more restrictive fuel airworthiness limitations and tasks, as specified in a European Union Aviation Safety Agency (EASA) AD, which is proposed for incorporation by reference. This proposed AD would also expand the applicability to include additional airplane models. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 87 Issue 112 (Friday, June 10, 2022)</title>
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[Federal Register Volume 87, Number 112 (Friday, June 10, 2022)]
[Proposed Rules]
[Pages 35465-35469]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2022-12406]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0673; Project Identifier MCAI-2021-01282-T]
RIN 2120-AA64
Airworthiness Directives; Airbus SAS Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2017-10-17, which applies to certain Airbus SAS Model A330-200; A330-
200 Freighter; and A330-300 series airplanes. AD 2017-10-17 requires
revising the existing maintenance or inspection program, as applicable,
to incorporate new fuel airworthiness limitations. Since the FAA issued
AD 2017-10-17, the FAA has determined that new or more restrictive fuel
airworthiness limitations and tasks are necessary. This proposed AD
would continue to require the actions in AD 2017-10-17 and require
revising the existing maintenance or inspection program, as applicable,
to incorporate additional new or more restrictive fuel airworthiness
limitations and tasks, as specified in a European Union Aviation Safety
Agency (EASA) AD, which is proposed for incorporation by reference.
This proposed AD would also expand the applicability to include
additional airplane models. The FAA is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by July 25,
2022.
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="https://www.regulations.gov">https://www.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: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590, between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
For EASA material that will be incorporated by reference (IBR) in
this
[[Page 35466]]
AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#4d0c093e0d282c3e2c6328383f223d2c632838"><span class="__cf_email__" data-cfemail="16575265567377657738736364796677387363">[email protected]</span></a>; internet
www.easa.europa.eu. You may find this material on the EASA website at
<a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>. For Airbus SAS service information
identified in this proposed AD, contact Airbus SAS, Airworthiness
Office--EAL, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex,
France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email
<a href="/cdn-cgi/l/email-protection#3859514a4f574a4c5051565d4b4b16790b0b0815790b0c087859514a5a4d4b165b5755"><span class="__cf_email__" data-cfemail="34555d46435b46405c5d5a5147471a75070704197507000474555d465641471a575b59">[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="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2022-
0673.
Examining the AD Docket
You may examine the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by
searching for and locating Docket No. FAA-2022-0673; 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 NPRM, the
mandatory continuing airworthiness information (MCAI), any comments
received, and other information. The street address for Docket
Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
Large Aircraft Section, FAA, International Validation Branch, 2200
South 216th St., Des Moines, WA 98198; telephone 206-231-3229; email
<a href="/cdn-cgi/l/email-protection#cabca6abaea3a7a3b8e4bfa6b3aba4a5bc8aacababe4ada5bc"><span class="__cf_email__" data-cfemail="a1d7cdc0c5c8ccc8d38fd4cdd8c0cfced7e1c7c0c08fc6ced7">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2022-0673; Project Identifier
MCAI-2021-01282-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, 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 proposal 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="https://www.regulations.gov">https://www.regulations.gov</a>, including any personal information you
provide. The agency will also post a report summarizing each
substantive verbal contact received about this NPRM.
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 NPRM 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 NPRM, 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 NPRM. Submissions containing CBI should be sent to
Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, FAA,
International Validation Branch, 2200 South 216th St., Des Moines, WA
98198; telephone 206-231-3229; email <a href="/cdn-cgi/l/email-protection#e1978d8085888c8893cf948d98808f8e97a1878080cf868e97"><span class="__cf_email__" data-cfemail="7d0b111c191410140f530811041c13120b3d1b1c1c531a120b">[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
The FAA issued AD 2017-10-17, Amendment 39-18891 (82 FR 24017, May
25, 2017) (AD 2017-10-17), which applies to certain Airbus SAS Model
A330-223F and -243F airplanes; Model A330-201, -202, -203, -223, and -
243 airplanes; Model A330-301, -302, -303, -321, -322, -323, -341, -
342, and -343 airplanes. AD 2017-10-17 requires revising the existing
maintenance or inspection program, as applicable, to include new fuel
airworthiness limitations. The FAA issued AD 2017-10-17 to address the
potential of ignition sources inside fuel tanks, which, in combination
with flammable fuel vapors, could result in fuel tank explosions and
consequent loss of the airplane.
Actions Since AD 2017-10-17 Was Issued
Since the FAA issued AD 2017-10-17, the FAA has determined that new
or more restrictive fuel airworthiness limitations and tasks are
necessary. In addition, Model A330-841 and -941 airplanes have been
type certificated in the United States and added to the applicability
of this proposed AD.
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0252, dated November 17, 2021
(EASA AD 2021-0252) (also referred to as the MCAI), to correct an
unsafe condition for all Airbus SAS Model A330-223F and -243F
airplanes; Model A330-201, -202, -203, -223, and -243 airplanes; Model
A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes;
A330-841 airplanes; and Model A330-941 airplanes.
Airplanes with an original airworthiness certificate or original
export certificate of airworthiness issued after July 1, 2021, must
comply with the airworthiness limitations specified as part of the
approved type design and referenced on the type certificate data sheet;
this proposed AD therefore does not include those airplanes in the
applicability.
This proposed AD was prompted by a determination that new or more
restrictive fuel airworthiness limitations and tasks are necessary. The
FAA is proposing this AD to address the potential of ignition sources
inside fuel tanks, which, in combination with flammable fuel vapors,
could result in fuel tank explosions and consequent loss of the
airplane. See the MCAI for additional background information.
Related Service Information Under 1 CFR Part 51
EASA AD 2021-0252 describes new or more restrictive fuel
airworthiness limitations and tasks.
This AD would also require Airbus A330 Airworthiness Limitations
Section (ALS) Part 5--Fuel Airworthiness Limitations (FAL), Revision
01, dated October 28, 2015, which the Director of the Federal Register
approved for incorporation by reference as of June 29, 2017 (82 FR
24017, May 25, 2017).
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
These products have been approved by the aviation authority of
another country and are approved for operation in the United States.
Pursuant to the FAA's bilateral agreement with the State of Design
Authority, it has notified the FAA of the unsafe condition described in
the MCAI and service information referenced above. The FAA is issuing
this NPRM after determining that the unsafe condition described
previously is
[[Page 35467]]
likely to exist or develop in other products of these same type
designs.
Proposed AD Requirements in This NPRM
This proposed AD would retain the requirements of AD 2017-10-17.
This proposed AD would also require revising the existing maintenance
or inspection program, as applicable, to incorporate new or more
restrictive fuel airworthiness limitations and tasks, which are
specified in EASA AD 2021-0252 described previously, as proposed for
incorporation by reference. Any differences with EASA AD 2021-0252 are
identified as exceptions in the regulatory text of this AD.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections) and
Critical Design Configuration Control Limitations (CDCCLs). Compliance
with these actions and CDCCLs is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed 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 (l)(1) of this proposed 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, the
FAA proposes to incorporate EASA AD 2021-0252 by reference in the FAA
final rule. This proposed AD would, therefore, require compliance with
EASA AD 2021-0252 through that incorporation, except for any
differences identified as exceptions in the regulatory text of this
proposed AD. Using common terms that are the same as the heading of a
particular section in EASA AD 2021-0252 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 2021-
0252. Service information required by EASA AD 2021-0252 for compliance
will be available at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and
locating Docket No. FAA-2022-0673 after the FAA final rule 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), intervals, or CDCCLs may be used unless the actions,
intervals, and CDCCLs are approved as an AMOC in accordance with the
procedures specified in the AMOCs paragraph under ``Additional FAA
Provisions.'' This new format includes a ``New Provisions for
Alternative Actions, Intervals, and CDCCLs'' paragraph that does not
specifically refer to AMOCs, but operators may still request an AMOC to
use an alternative action, interval, or CDCCL.
Costs of Compliance
The FAA estimates that this proposed AD affects 138 airplanes of
U.S. registry. The FAA estimates the following costs to comply with
this proposed AD:
The FAA estimates the total cost per operator for the retained
actions from AD 2017-10-17 to be $7,650 (90 work-hours x $85 per work-
hour).
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the agency recognizes that this number may vary from operator
to operator. Since operators incorporate maintenance or inspection
program changes for their affected fleet(s), the FAA has determined
that a per-operator estimate is more accurate than a per-airplane
estimate.
The FAA estimates the total cost per operator for the new proposed
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
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
[[Page 35468]]
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) 2017-10-17, Amendment 39-18891
(82 FR 24017, May 25, 2017); and
0
b. Adding the following new AD:
Airbus SAS: Docket No. FAA-2022-0673; Project Identifier MCAI-2021-
01282-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by July 25, 2022.
(b) Affected ADs
This AD replaces AD 2017-10-17, Amendment 39-18891 (82 FR 24017,
May 25, 2017) (AD 2017-10-17).
(c) Applicability
This AD applies to Airbus SAS Model airplanes identified in
paragraphs (c)(1) through (4) 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 A330-223F and -243F airplanes.
(2) Model A330-201, -202, -203, -223, and -243 airplanes.
(3) Model A330-301, -302, -303, -321, -322, -323, -341, -342,
and -343 airplanes.
(4) Model A330-841, and -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 fuel airworthiness limitations and tasks are necessary.
The FAA is issuing this AD to address the potential of ignition
sources inside fuel tanks, which, in combination with flammable fuel
vapors, could result in fuel tank explosions and consequent loss of
the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Revision of the Existing Maintenance or Inspection
Program, With No Changes
This paragraph restates the requirements of paragraph (j) of AD
2017-10-17, with no changes. For airplanes identified in paragraphs
(c)(1) through (3) with an original certificate of airworthiness or
original export certificate of airworthiness issued on or before
October 28, 2015: Within 3 months after June 29, 2017 (the effective
date of AD 2017-10-17), revise the existing maintenance or
inspection program, as applicable, to incorporate Airbus A330
Airworthiness Limitations Section (ALS) Part 5--Fuel Airworthiness
Limitations (FAL), Revision 01, dated October 28, 2015. The
compliance times for accomplishing the initial tasks specified in
Airbus A330 ALS Part 5--FAL, Revision 01, dated October 28, 2015,
are at the times specified in Airbus A330 ALS Part 5--FAL, Revision
01, dated October 28, 2015, or within 3 months after revising the
maintenance or inspection program as required by paragraph (g) of
this AD, whichever occurs later. Accomplishing the revision of the
existing maintenance or inspection program required by paragraph (i)
of this AD terminates the requirements of this paragraph.
(h) Retained Restrictions on Alternative Actions, Intervals, and
Critical Design Configuration Control Limitations (CDCCLs), With a New
Exception
This paragraph restates the requirements of paragraph (k) of AD
2017-10-17, with a new exception. Except as required by paragraph
(i) of this AD, after accomplishing the revision required by
paragraph (g) of this AD, no alternative actions (e.g.,
inspections), intervals, or CDCCLs may be used unless the actions,
intervals, or CDCCLs are approved as an AMOC in accordance with the
procedures specified in paragraph (l)(1) of this AD.
(i) New Revision of the Existing Maintenance or Inspection Program
Except as specified in paragraph (j) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, European Union Aviation Safety Agency (EASA) AD
2021-0252, dated November 17, 2021 (EASA AD 2021-0252).
Accomplishing the revision of the existing maintenance or inspection
program required by this paragraph terminates the requirements of
paragraph (g) of this AD.
(j) Exceptions to EASA AD 2021-0252
(1) Where EASA AD 2021-0252 refers to its effective date, this
AD requires using the effective date of this AD.
(2) The requirements specified in paragraphs (1) and (2) of EASA
AD 2021-0252 do not apply to this AD.
(3) Paragraph (3) of EASA AD 2021-0252 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 (3) of EASA AD 2021-0252 is at the applicable
``limitations'' and ``intervals'' as incorporated by the
requirements of paragraph (3) of EASA AD 2021-0252, or within 90
days after the effective date of this AD, whichever occurs later.
(5) The provisions specified in paragraphs (4) and (5) of EASA
AD 2021-0252 do not apply to this AD.
(6) The ``Remarks'' section of EASA AD 2021-0252 does not apply
to this AD.
(k) New Provisions for Alternative Actions, Intervals, and CDCCLs
After the existing maintenance or inspection program has been
revised as required by paragraph (i) of this AD, no alternative
actions (e.g., inspections), intervals, and CDCCLs are allowed
unless they are approved as specified in the provisions of the
``Ref. Publications'' section of EASA AD 2021-0252.
(l) 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 (m)(2) of
this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#d5ecf8948386f8949c87f8e2e6e5f894989a9695b3b4b4fbb2baa3"><span class="__cf_email__" data-cfemail="b78e9af6e1e49af6fee59a8084879af6faf8f4f7d1d6d699d0d8c1">[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.
(m) Related Information
(1) For EASA AD 2021-0252, contact EASA, Konrad-Adenauer-Ufer 3,
50668 Cologne, Germany; telephone +49 221 8999 000; email
<a href="/cdn-cgi/l/email-protection#5b1a1f281b3e3a283a753e2e29342b3a753e2e"><span class="__cf_email__" data-cfemail="85c4c1f6c5e0e4f6e4abe0f0f7eaf5e4abe0f0">[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>. 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. This material may be found in the AD docket at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-
2022-0673.
(2) 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 206-231-3229; email <a href="/cdn-cgi/l/email-protection#d0a6bcb1b4b9bdb9a2fea5bca9b1bebfa690b6b1b1feb7bfa6"><span class="__cf_email__" data-cfemail="82f4eee3e6ebefebf0acf7eefbe3ecedf4c2e4e3e3ace5edf4">[email protected]</span></a>.
(3) For Airbus SAS service information identified in this AD,
contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile
Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93
36 96; fax +33 5 61 93 45 80; email <a href="/cdn-cgi/l/email-protection#b7d6dec5c0d8c5c3dfded9d2c4c499f68484879af6848387f7d6dec5d5c2c499d4d8da"><span class="__cf_email__" data-cfemail="1f7e766d68706d6b7776717a6c6c315e2c2c2f325e2c2b2f5f7e766d7d6a6c317c7072">[email protected]</span></a>; internet <a href="https://www.airbus.com">https://www.airbus.com</a>. 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.
[[Page 35469]]
Issued on June 3, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022-12406 Filed 6-9-22; 8:45 am]
BILLING CODE 4910-13-P
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