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Federal Register / Vol. 86, No. 42 / Friday, March 5, 2021 / Rules and Regulations
i of this AD, after the maintenance or inspection program 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 l1 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 20200215, dated October 6, 2020 EASA AD 20200215.
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 20200215
1 The requirements specified in paragraphs 1 and 2 of EASA AD 2020
0215 do not apply to this AD.
2 Paragraph 3 of EASA AD 20200215
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, tasks and associated thresholds and intervals specified in paragraph 3 of EASA
AD 20200215 within 90 days after the effective date of this AD.
3 The initial compliance time for doing the tasks specified in paragraph 3 of EASA
AD 20200215 is at the applicable associated thresholds specified in paragraph 3 of EASA AD 20200215, or within 90 days after the effective date of this AD, whichever occurs later.
4 The provisions specified in paragraphs 4 and 5 of EASA AD 20200215 do not apply to this AD.
5 The Remarks section of EASA AD
20200215 does not apply to this AD.

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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 unless they are approved as specified in the provisions of the Ref.
Publications section of EASA AD 2020
0215.
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 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 of this AD.

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15:52 Mar 04, 2021

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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 Dassault Aviations EASA Design Organization Approval DOA. If approved by the DOA, the approval must include the DOA-authorized signature.

Issued on February 11, 2021.
Gaetano A. Sciortino, Deputy Director for Strategic Initiatives, Compliance & Airworthiness Division, Aircraft Certification Service.

m Related Information For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 2062313226; email tom.rodriguez@
faa.gov.

Docket No. FAA20201106; Project Identifier MCAI202001065T; Amendment 3921435; AD 20210414

n 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.
3 The following service information was approved for IBR on April 9, 2021.
i European Union Aviation Safety Agency EASA AD 20200215, dated October 6, 2020.
ii Reserved 4 The following service information was approved for IBR on January 4, 2019 83 FR
61523, November 30, 2018.
i Section 54000, Airworthiness Limitations, Revision 13, dated July 2017, of the Dassault Falcon 10 Maintenance Manual.
ii Reserved 5 For EASA AD 20200215, contact the 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.
6 For Dassault Aviation service information identified in this AD, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 2014406700; internet https www.dassaultfalcon.com.
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 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. FAA20201111.
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 fedreg.legal@
nara.gov, or go to: https www.archives.gov/
federal-register/cfr/ibr-locations.html.

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FR Doc. 202104340 Filed 3421; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39

RIN 2120AA64

Airworthiness Directives; Airbus SAS
Airplanes Federal Aviation Administration FAA, Department of Transportation DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for certain Airbus SAS Model A350941 and A3501041 airplanes. This AD was prompted by reports that suitable corrosion protection treatment had not been applied to certain areas of the seat track. This AD requires a one-time detailed inspection of the seat tracks between certain frames for suitable corrosion protection or presence of corrosion, and on-condition actions if necessary, 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 April 9, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of April 9, 2021.
ADDRESSES: For material incorporated by reference IBR in this AD, contact the 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 IBR material on the EASA website at https ad.easa.europa.eu. 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 2062313195.
It is also available in the AD docket on the internet at https
www.regulations.gov by searching for SUMMARY:

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