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Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
PART 39AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:

Authority: 49 U.S.C. 106g, 40113, 44701.
39.13

Amended
2. The FAA amends 39.13 by a. Removing Airworthiness Directive AD 20200914, Amendment 39
19910 85 FR 30601, May 20, 2020, and b. Adding the following new AD:

20211012 Airbus SAS: Amendment 39
21545; Docket No. FAA20201178;
Project Identifier MCAI202001325T.
a Effective Date This airworthiness directive AD is effective July 29, 2021.
b Affected ADs This AD replaces AD 20200914, Amendment 3919910 85 FR 30601, May 20, 2020 AD 20200914.
c Applicability This AD applies to Airbus SAS Model A350941 and 1041 airplanes, certificated in any category, as identified in European Union Aviation Safety Agency EASA AD
20200203, dated September 23, 2020 EASA
AD 20200203.
d Subject Air Transport Association ATA of America Code 31, Instruments.
e Reason This AD was prompted by two reports of abnormal operation of the components of the ENG START panel or Electronic Centralized Aircraft Monitoring ECAM Control Panel ECP due to liquid spillage in the system, and the subsequent uncommanded engine inflight shutdown IFSD of one engine in each case. This AD was also prompted by the development of a new, water-resistant integrated control panel ICP that will address this unsafe condition. The FAA is issuing this AD to address the potential for dual-engine IFSD, possibly resulting in a forced landing with consequent damage to the airplane and injury to occupants.
f Compliance Comply with this AD within the compliance times specified, unless already done.

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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, EASA AD 20200203.
h Exceptions to EASA AD 20200203
1 Where EASA AD 20200203 refers to its effective date, this AD requires using the effective date of this AD.
2 Where EASA AD 20200203 refers to the effective date of EASA AD 20200020E, this AD requires using February 14, 2020 the effective date of AD 20200312 85 FR 7863, February 12, 2020.

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3 Where EASA AD 20200203 refers to the effective date of EASA AD 20200090, this AD requires using June 4, 2020 the effective date of AD 20200914.
4 Where paragraph 7 of EASA AD 2020
0203 specifies removing the AFM airplane flight manual changes as required by paragraph 2 or 4 of the MCAI, as applicable, this AD requires removing the AFM changes required by paragraph 1, 2, 4, or 5, as applicable, from the AFM.
5 For airplanes with Mod 116010: This AD does not require the actions specified in paragraphs 1, 3, and 4 of EASA AD
20200203, as specified in paragraph g of this AD.
6 Note 1 of EASA AD 20200203 does not apply to this AD. However, after the actions required by EASA AD 20200203, paragraphs 3 through 5, as required by paragraph g of this AD, have been accomplished on an airplane, that airplane may be operated with a damaged or missing ICP removable cover, provided provisions that address the ICP removable cover are included in the operators approved minimum equipment list MEL. After the actions required by EASA AD 20200203, paragraph 6, as required by paragraph g of this AD, have been accomplished on an airplane, that airplane may be operated without an ICP removable cover, provided provisions that address the ICP removable cover are removed from the operators approved MEL.
7 The Remarks section of EASA AD
20200203 does not apply to this AD.
i Special Flight Permit Special flight permits may be issued in accordance with 14 CFR 21.197 and 21.199
to operate the airplane to a location where the actions specified in this AD can be accomplished if the operator elects to do so, provided a removable ICP cover is installed on the flight deck.
j 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 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 k of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. 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 SASs EASA Design
PO 00000

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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 j2 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 operators 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.
k Related Information For more information about this AD, contact Kathleen Arrigotti, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200
South 216th St., Des Moines, WA 98198;
telephone and fax 2062313218.
l 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. 552a 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 20200203, dated September 23, 2020.
ii Reserved 3 For EASA AD 20200203, contact EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https
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 2062313195. This material may be found in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA20201178.
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 fedreg.legal@
nara.gov, or go to: https www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on April 30, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202113123 Filed 62321; 8:45 am BILLING CODE 491013P

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