[Federal Register Volume 85, Number 138 (Friday, July 17, 2020)]
[Proposed Rules]
[Pages 43499-43503]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-15335]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0581; Product Identifier 2020-NM-057-AD]
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) 
2015-22-08, which applies to all Airbus SAS Model A318 series 
airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 
airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes. 
The FAA also proposes to supersede AD 2018-17-19, which applies to 
certain Airbus SAS Model A318 series airplanes; Model A319-111, -112, -
113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, 
-214, -216, -231, -232, -233, -251N, and -271N airplanes; and Model 
A321-111, -112, -131, -211, -212, -213, -231, -232, -251N, -253N, and -
271N airplanes. The FAA also proposes to supersede AD 2019-19-15, which 
applies to certain Airbus SAS Model A318 series airplanes; Model A319-
111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model 
A320-211, -212, -214, -216, -231, -232, -233, -251N, and -271N 
airplanes; and Model A321 series airplanes. AD 2019-19-15 requires 
revising the existing maintenance or inspection program, as applicable, 
to incorporate new or more restrictive airworthiness limitations. Since 
the FAA issued AD 2019-19-15, the FAA has determined that new or more 
restrictive airworthiness limitations are necessary. This proposed AD 
would require 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 will be incorporated by reference. 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 August 31, 
2020.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     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.
     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 AD, contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, 
Germany; telephone +49 221 89990 1000; email [email protected]; 
internet www.easa.europa.eu. You may find this IBR material on the EASA 
website at https://ad.easa.europa.eu.
    For the Airbus material identified in this proposed AD that will 
continue to be incorporated by reference, contact Airbus SAS, 
Airworthiness Office--EIAS, Rond-Point Emile Dewoitine No: 2, 31700 
Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 
51; email [email protected]; internet https://www.airbus.com.
    You may view this IBR 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 on the 
internet at https://www.regulations.gov by searching for and locating 
Docket No. FAA-2020-0581.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
0581; 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, any comments received, and other information. The street 
address for Docket Operations is listed above.

[[Page 43500]]

Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Sanjay Ralhan, Aerospace Engineer, 
Large Aircraft Section, International Validation Branch, FAA, 2200 
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3223; 
email [email protected].

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 the ADDRESSES section. Include ``Docket No. FAA-2020-0581; 
Product Identifier 2020-NM-057-AD'' 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 NPRM based on 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 that are received, without 
change, to https://www.regulations.gov, including any personal 
information you provide. The FAA will also post a report summarizing 
each substantive verbal contact the FAA receives 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 the 
attention of the person identified in the FOR FURTHER INFORMATION 
CONTACT section. Any commentary that the FAA receives which is not 
specifically designated as CBI will be placed in the public docket for 
this rulemaking.

Discussion

    The FAA issued AD 2019-19-15, Amendment 39-19751 (84 FR 54480, 
October 10, 2019) (``AD 2019-19-15''), for certain Airbus SAS Model 
A318 series airplanes; Model A319-111, -112, -113, -114, -115, -131, -
132, and -133 airplanes; Model A320-211, -212, -214, -216, -231, -232, 
-233, -251N, and -271N airplanes; and Model A321 series airplanes. AD 
2019-19-15 requires revising the existing maintenance or inspection 
program, as applicable, to incorporate new or more restrictive 
airworthiness limitations. The FAA issued AD 2019-19-15 to address the 
failure of certain life-limited parts, which could result in reduced 
structural integrity of the airplane. AD 2019-19-15 specifies that 
accomplishing the revision required by that AD terminates all 
requirements of AD 2018-17-19, Amendment 39-19373 (83 FR 44460, August 
31, 2018) (``AD 2018-17-19''). AD 2018-17-19 specifies that 
accomplishing the revisions required by that AD terminates all 
requirements of AD 2015-22-08, Amendment 39-18313 (80 FR 68434, 
November 5, 2015) (``AD 2015-22-08'') and AD 2015-05-02, Amendment 39-
18112 (80 FR 15152, March 23, 2015) (``AD 2015-05-02''). AD 2015-05-02 
was already superseded by AD 2017-22-03, Amendment 39-19083 (82 FR 
49091, October 24, 2017) (``AD 2017-22-03'').
    AD 2018-17-19 corresponds to EASA AD 2017-0215, dated October 24, 
2017 (``EASA AD 2017-0215''), and requires revising the maintenance or 
inspection program to incorporate Airbus A318/A319/A320/A321 
Airworthiness Limitations Section (ALS) Part 1 Safe Life Airworthiness 
Limitations (SL-ALI), Revision 05, Issue 02, dated April 19, 2017 
(``ALS Part 1, Revision 05''). EASA AD 2017-0215 superseded EASA AD 
2014-0141, dated June 4, 2014 (``EASA AD 2014-0141''), which 
corresponds with FAA AD 2015-22-08. EASA AD 2017-0215 stated it 
supersedes EASA AD 2014-0141 and requires accomplishment of the actions 
specified in A318/A319/A320/A321 ALS Part 1 Revision 05 (which includes 
the life limits required by EASA AD 2014-0141).
    Although the applicability of EASA AD 2017-0215 was all airplanes, 
the corresponding FAA AD 2018-17-19 only applied to airplanes with an 
original airworthiness certificate or original export certificate of 
airworthiness issued on or before April 19, 2017 (the date of approval 
of ALS Part 1, Revision 05). Airplanes with an original airworthiness 
certificate or original export certificate of airworthiness issued 
after April 19, 2017, 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 would supersede AD 2019-19-15, AD 2018-17-19, and 
AD 2015-22-08.

Actions Since AD 2019-19-15 Was Issued

    Since the FAA issued AD 2019-19-15, the FAA has determined that new 
or more restrictive airworthiness limitations are necessary.
    The EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2020-0080, dated April 1, 2020 
(``EASA AD 2020-0080'') (also referred to as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for all Model A318-111, -112, -121, and -122 airplanes; Model 
A319-111, -112, -113, -114, -115, -131, -132, -133, -151N, and -153N 
airplanes; Model A320-211, -212, -214, -215, -216, -231, -232, -233, -
251N, -252N, -253N, -271N, -272N, and -273N airplanes; and Model A321-
111, -112, -131, -211, -212, -213, -231, -232, -251N, -252N, -253N, -
271N, -272N, -251NX, -252NX, -253NX, -271NX, and -272NX airplanes. 
Model A320-215 airplanes are not certificated by the FAA and are not 
included on the U.S. type certificate data sheet; this AD therefore 
does not include those airplanes in the applicability.
    Airplanes with an original airworthiness certificate or original 
export certificate of airworthiness issued after November 13, 2019, 
must comply with the airworthiness limitations specified as part of the 
approved type design and referenced on the type certificate data sheet; 
this AD therefore does not include those airplanes in the 
applicability.
    This proposed AD was prompted by a determination that new or more 
restrictive airworthiness limitations are necessary. The FAA is 
proposing this AD to address the failure of certain life-limited parts, 
which could result in reduced structural integrity of the airplane. See 
the MCAI for additional background information.

Related IBR Material Under 1 CFR Part 51

    EASA AD 2020-0080 describes new or more restrictive airworthiness 
limitations for airplane structures and safe life limits.
    This AD would also require Airbus A318/A319/A320/A321 Airworthiness

[[Page 43501]]

Limitations Section (ALS) Part 1 Safe Life Airworthiness Limitations 
(SL-ALI), Revision 06, Issue 02, dated November 30, 2018, which the 
Director of the Federal Register approved for incorporation by 
reference as of November 14, 2019 (84 FR 54480, October 10, 2019).
    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 and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with the State of Design Authority, the FAA 
has been notified of the unsafe condition described in the MCAI and 
service information referenced above. The FAA is proposing this AD 
because the FAA has evaluated all pertinent information and determined 
an unsafe condition exists and is likely to exist or develop on other 
products of the same type design.

Proposed AD Requirements

    This proposed AD would retain the requirements of AD 2019-19-15. 
This proposed AD would also require revising the existing maintenance 
or inspection program, as applicable, to incorporate new or more 
restrictive airworthiness limitations, which are specified in EASA AD 
2020-0080 described previously, as incorporated by reference. Any 
differences with EASA AD 2020-0080 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). 
Compliance with these actions is required by 14 CFR 91.403(c). For 
airplanes that have been previously modified, altered, or repaired in 
the areas addressed by this 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 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 initially worked with Airbus and EASA to develop a 
process to use certain EASA ADs as the primary source of information 
for compliance with requirements for corresponding FAA ADs. The FAA has 
since coordinated with other manufacturers and civil aviation 
authorities (CAAs) to use this process. As a result, EASA AD 2020-0080 
will be incorporated by reference in the FAA final rule. This proposed 
AD would, therefore, require compliance with EASA AD 2020-0080 in its 
entirety, 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 the EASA AD 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 the EASA AD.
    Service information specified in EASA AD 2020-0080 that is required 
for compliance with EASA AD 2020-0080 will be available on the internet 
at https://www.regulations.gov by searching for and locating Docket No. 
FAA-2020-0581 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).

Costs of Compliance

    The FAA estimates that this proposed AD affects 1,553 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 2019-19-15 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. In the past, the agency has estimated that this action 
takes 1 work-hour per airplane. 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) 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 43502]]

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:

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) 2015-22-08, Amendment 39-18313 
(80 FR 68434, November 5, 2015); AD 2018-17-19, Amendment 39-19373 (83 
FR 44460, August 31, 2018); and AD 2019-19-15, Amendment 39-19751 (84 
FR 54480, October 10, 2019); and
0
b. Adding the following new AD:

Airbus SAS: Docket No. FAA-2020-0581; Product Identifier 2020-NM-
057-AD.

(a) Comments Due Date

    The FAA must receive comments by August 31, 2020.

(b) Affected ADs

    This AD replaces AD 2015-22-08, Amendment 39-18313 (80 FR 68434, 
November 5, 2015) (``AD 2015-22-08''); AD 2018-17-19, Amendment 39-
19373 (83 FR 44460, August 31, 2018) (``AD 2018-17-19''); and AD 
2019-19-15, Amendment 39-19751 (84 FR 54480, October 10, 2019) (``AD 
2019-19-15'').

(c) Applicability

    This AD applies to the Airbus SAS airplanes specified 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 November 13, 
2019.
    (1) Model A318-111, -112, -121, and -122 airplanes.
    (2) Model A319-111, -112, -113, -114, -115, -131, -132, -133, -
151N, and -153N airplanes.
    (3) Model A320-211, -212, -214, -216, -231, -232, -233, -251N, -
252N, -253N, -271N, -272N, and -273N airplanes.
    (4) Model A321-111, -112, -131, -211, -212, -213, -231, -232, -
251N, -252N, -253N, -271N, -272N, -251NX, -252NX, -253NX, -271NX, 
and -272NX airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 05, Time Limits/
Maintenance Checks.

(e) Reason

    This AD was prompted by a determination that new or more 
restrictive airworthiness limitations are necessary. The FAA is 
issuing this AD to address the 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 Maintenance or Inspection Program Revision, With No 
Changes

    This paragraph restates the requirements of paragraph (g) of AD 
2019-19-15, with no changes. For airplanes with an original 
airworthiness certificate or original export certificate of 
airworthiness issued on or before November 30, 2018: Within 90 days 
after November 14, 2019 (the effective date of AD 2019-19-15), 
revise the existing maintenance or inspection program, as 
applicable, to incorporate Airbus SAS A318/A319/A320/A321 
Airworthiness Limitations Section (ALS) Part 1 Safe Life 
Airworthiness Limitations (SL-ALI), Revision 06, Issue 02, dated 
November 30, 2018. The initial compliance time for doing the revised 
actions is at the applicable time specified in Airbus SAS A318/A319/
A320/A321 ALS Part 1 Safe Life Airworthiness Limitations (SL-ALI), 
Revision 06, Issue 02, dated November 30, 2018, or within 90 days 
after November 14, 2019, whichever occurs later. Accomplishing the 
maintenance or inspection program revision required by paragraph (i) 
of this AD terminates the requirements of this paragraph.

(h) Retained Restrictions on Alternative Actions and Intervals With a 
New Exception

    This paragraph restates the requirements of paragraph (h) of AD 
2019-19-15, with a new exception. Except as required by paragraph 
(i) of this AD, after the maintenance or inspection program has been 
revised as required by paragraph (g) of this AD, no alternative life 
limits may be used unless approved as an alternative method of 
compliance (AMOC) in accordance with the procedures specified in 
paragraph (l)(1) of this AD.

(i) New Maintenance or Inspection Program Revision

    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 
2020-0080, dated April 1, 2020 (``EASA AD 2020-0080''). 
Accomplishing the maintenance or inspection program revision 
required by this paragraph terminates the requirements of paragraph 
(g) of this AD.

(j) Exceptions to EASA AD 2020-0080

    (1) The requirements specified in paragraph (1), (3), and (4) of 
EASA AD 2020-0080 do not apply to this AD.
    (2) Paragraph (2) of EASA AD 2020-0080 specifies revising ``the 
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 (3) of EASA AD 2020-0080 within 90 days after the 
effective date of this AD.
    (3) The initial compliance time for doing the tasks specified in 
paragraph (2) of EASA AD 2020-0080 is at the applicable compliance 
times specified in paragraph (2) of EASA AD 2020-0080, or within 90 
days after the effective date of this AD, whichever occurs later.
    (4) The ``Remarks'' section of EASA AD 2020-0080 does not apply 
to this AD.

(k) New Provisions for Alternative Actions and Intervals

    After the 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 except as specified in the 
provisions of the ``Ref. Publications'' section of EASA AD 2020-
0080.

(l) Other 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 local Flight 
Standards District 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)(4) of this AD. Information may be emailed to: [email protected].
    (i) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.
    (ii) AMOCs approved previously for AD 2019-19-15 are approved as 
AMOCs for the corresponding provisions of EASA AD 2020-0080 that are 
required by paragraph (g) of this AD.
    (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.
    (3) Required for Compliance (RC): For any service information 
referenced in EASA AD 2020-0080 that contains RC procedures and 
tests: Except as required by paragraph (l)(2) of this AD, RC 
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

[[Page 43503]]

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.

(m) Related Information

    (1) For information about EASA AD 2020-0080, contact the EASA, 
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 
89990 6017; email [email protected]; internet www.easa.europa.eu. 
You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.
    (2) For information about the Airbus material identified in this 
AD, contact Airbus SAS, Airworthiness Office--EIAS, Rond-Point Emile 
Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 
36 96; fax +33 5 61 93 44 51; email [email protected]; 
internet https://www.airbus.com.
    (3) 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 on the internet at https://www.regulations.gov by searching 
for and locating Docket No. FAA-2020-0581.
    (4) For more information about this AD, contact Sanjay Ralhan, 
Aerospace Engineer, Large Aircraft Section, International Validation 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3223; email [email protected].

    Issued on July 9, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification 
Service.
[FR Doc. 2020-15335 Filed 7-16-20; 8:45 am]
BILLING CODE 4910-13-P