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Federal Register / Vol. 86, No. 34 / Tuesday, February 23, 2021 / Rules and Regulations
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 20200114, dated May 20, 2020 EASA AD 20200114.
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 20200114
1 The requirements specified in paragraphs 1 and 2 of EASA AD 2020
0114 do not apply to this AD.
2 Paragraph 3 of EASA AD 20200114
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 20200114 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 20200114 is at the applicable associated thresholds specified in paragraph 3 of EASA AD 20200114, 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 20200114 do not apply to this AD.
5 The Remarks section of EASA AD
20200114 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, and intervals are allowed unless they are approved as specified in the provisions of the Ref.
Publications section of EASA AD 2020
0114.
l Terminating Action for Certain Actions in AD 20102605
Accomplishing the actions required by paragraph g or i of this AD terminates the requirements of paragraph g1 of AD 2010
2605, for Dassault Aviation Model FALCON
2000EX airplanes only.
m 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 n of this AD.
Information may be emailed to: 9-AVS-AIR-

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21:28 Feb 22, 2021

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730-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.
n 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.
o 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 March 30, 2021.
i European Union Aviation Safety Agency EASA AD 20200114, dated May 20, 2020.
ii Reserved 4 The following service information was approved for IBR on May 4, 2020 85 FR
17487, March 30, 2020.
i Chapter 540, Airworthiness Limitations, DGT 113877, Revision 12, dated November 2018, of the Dassault Falcon 2000EX Maintenance Manual.
ii Reserved 5 For EASA AD 20200114, 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. For Dassault Aviation material, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606;
telephone 2014406700; internet https
www.dassaultfalcon.com.
6 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. FAA20200976.
7 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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Issued on February 1, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202103576 Filed 22221; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20201020; Project Identifier MCAI202000988T; Amendment 3921401; AD 20210218
RIN 2120AA64

Airworthiness Directives; Airbus Defense and Space S.A. Formerly Known as Construcciones Aeronauticas, S.A. Airplanes Federal Aviation Administration FAA, Department of Transportation DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for all Airbus Defense and Space S.A. Model CN235, CN235100, CN235200, and CN235300 airplanes and Model C295 airplanes. This AD was prompted by cracks found on certain leftand right-hand stringers in a certain area of the fuselage. This AD requires repetitive inspections for cracking or broken rivets of certain leftand right-hand stringers and surrounding structure, and repair 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 March 30, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of March 30, 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
SUMMARY:

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