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Federal Register / Vol. 86, No. 35 / Wednesday, February 24, 2021 / Rules and Regulations
h Terminating Action As a terminating action to the requirements of paragraph g of this AD, perform the following:
1 Do a protrusion check at all eight bolt locations using paragraph 3.C.3 of the SB.
2 Do a pull-out test at all eight bolt locations using paragraph 3.C.4 of the SB.
3 If the inserts on the HMU/MEC idler adapter fail the protrusion check or pull-out test required by paragraph h1 or 2 of this AD, replace the inserts using paragraph 3.C.5 of the SB. After replacement of the inserts is accomplished, the requirements of this AD have been met and no further action is required.
4 If the inserts on the HMU/MEC idler adapter pass both the protrusion check and the pull-out test required by paragraphs h1
and 2 of this AD, the requirements of this AD have been met and no further action is required.
i Credit for Previous Actions 1 You may take credit for any shim check of the HMU/MEC idler adapter required by paragraph g of this AD if you performed this shim check before the effective date of this AD using GE CF680C2 SB 721577 R00, dated October 31, 2018.
2 You may take credit for the terminating action required by paragraph h of this AD
if you performed this action before the effective date of this AD using GE CF680C2
SB 721577 R00, dated October 31, 2018.
j Definition For the purpose of this AD, an engine shop visit is the induction of an engine into the shop for maintenance involving the separation of pairs of major mating engine case flanges, except separation of engine flanges solely for the purposes of transportation of the engine without subsequent maintenance, which does not constitute an engine shop visit.

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k Alternative Methods of Compliance AMOCs 1 The Manager, ECO 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 manager of the certification office, send it to the attention of the person identified in Related Information. You may email your request to: ANE-AD-AMOC@
faa.gov.
2 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.
l Related Information For more information about this AD, contact Kevin M. Clark, Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803; phone: 781
2387088; fax: 781 2387199; email:
kevin.m.clark@faa.gov.

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m 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 the AD specifies otherwise.
i General Electric Company GE CF6
80C2 Service Bulletin 721577 R01, dated August 16, 2019.
ii Reserved 3 For GE service information identified in this AD, contact General Electric Company, 1 Neumann Way, Cincinnati, OH 45215;
phone: 513 5523272; email:
aviation.fleetsupport@ge.com.
4 You may view this service information at FAA, Airworthiness Products Section, Operational Safety Branch, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781 2387759.
5 You may view this service information 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 January 21, 2021.
Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202103606 Filed 22321; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20200980; Product Identifier 2020NM094AD; Amendment 3921414; AD 20210311
RIN 2120AA64

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

The FAA is superseding Airworthiness Directive AD 202002
21, which applied to all Dassault Aviation Model FALCON 2000
airplanes. AD 20200221 required revising the existing maintenance or inspection program, as applicable, to incorporate new or more restrictive airworthiness limitations. This AD
requires revising the existing maintenance or inspection program, as applicable to incorporate new or more
SUMMARY:

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restrictive airworthiness limitations, as specified in a European Union Aviation Safety Agency EASA AD, which is incorporated by reference. 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 unsafe condition on these products.
DATES: This AD is effective March 31, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of March 31, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of March 18, 2020 85 FR
7860, February 12, 2020.
ADDRESSES: For EASA material incorporated by reference IBR in this AD, contact the EASA, KonradAdenauer-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. For Dassault Aviation service information identified in this final rule, contact Dassault Falcon Jet Corporation, Teterboro Airport, P.O. Box 2000, South Hackensack, NJ 07606; telephone 201
4406700; internet https
www.dassaultfalcon.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 2062313195.
It is also available in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2020
0980.
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. FAA2020
0980; 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 final rule, any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South
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