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Federal Register / Vol. 86, No. 239 / Thursday, December 16, 2021 / Rules and Regulations
e Reason This AD was prompted by reports of bushing migration, loss of nut torque on the engine pylon lower inboard and outboard link fittings, a loose lower link assembly, and damaged nuts; and the need to shorten the compliance time for the modification of the pylon lower link fitting attaching parts. The FAA is issuing this AD to prevent loss of integrity of the lower link fittings of the engine pylon, which could lead to separation of the engine from the wing.
f Compliance Comply with this AD within the compliance times specified, unless already done.
g Requirements For airplanes identified in Agencia Nacional de Aviac ao Civil ANAC AD 2020
0602R02, effective November 30, 2020
ANAC AD 20200602R02: Except as specified in paragraphs h and i of this AD, comply with all required actions and compliance times specified in, and in accordance with, ANAC AD 20200602R02.
h Exceptions to ANAC AD 20200602R02
1 Where ANAC AD 20200602R02 refers to its effective date, this AD requires using the effective date of this AD.
2 Where ANAC AD 20200602R02 refers to July 3, 2014, this AD requires using September 2, 2014 the effective date of AD
20141616.
3 Where ANAC AD 20200602R02 refers to April 25, 2017, this AD requires using November 2, 2018 the effective date of AD
20181928.
4 Paragraphs y, Alternative methods of compliance AMOCs, and z, Material incorporated by reference, of ANAC AD
20200602R02 do not apply to this AD.
5 Where ANAC AD 20200602R02
specifies replace immediately, this AD
requires replacing before further flight.
6 Paragraph w, Parts installation prohibition, of ANAC AD 20200602R02
does not apply to this AD, except as specified in paragraph i of this AD.

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i Parts Installation Prohibition As of September 2, 2014 the effective date of AD 20141616, no person may install a lock assembly identified in Embraer Service Bulletin 190540013, dated November 27, 2012; or Embraer Service Bulletin 190LIN
540004, dated December 20, 2012; at the inboard or outboard lower link fitting on any airplane.
j Additional 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,
VerDate Sep<11>2014

16:14 Dec 15, 2021

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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 ANAC; or ANACs authorized Designee. If approved by the ANAC Designee, the approval must include the Designees authorized signature.
3 Required for Compliance RC: Except as specified by paragraph h of this AD, for service information that contains steps that are labeled as Required for Compliance RC, the provisions of paragraphs j3i and ii of this AD apply.
i The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. If a step or substep is labeled RC Exempt, then the RC
requirement is removed from that step or substep. An AMOC is required for any deviations to RC steps, including substeps and identified figures.
ii Steps not labeled 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 RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition.
k Related Information For more information about this AD, contact Krista Greer, Aerospace Engineer, Large Aircraft Section, International Validation Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 2062313221; email krista.greer@
faa.gov.
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.
3 The following service information was approved for IBR on January 20, 2022.
i Agencia Nacional de Aviac ao Civil ANAC AD 20200602R02, effective November 30, 2020.
ii Reserved 4 The following service information was approved for IBR on September 2, 2014 79
FR 48018, August 15, 2014.
i Embraer Service Bulletin 190540013, dated November 27, 2012.
ii Embraer Service Bulletin 190LIN54
0004, dated December 20, 2012.
5 For ANAC AD 20200602R02, contact ANAC, Aeronautical Products Certification Branch GGCP, Rua Dr. Orlando Feirabend
PO 00000

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Filho, 230Centro Empresarial Aquarius Torre BAndares 14 a 18, Parque Residencial Aquarius, CEP 12.246190Sao Jose dos CamposSP, Brazil; telephone 55
12 32036600; email pac@anac.gov.br;
internet www.anac.gov.br/en/. You may find this ANAC AD on the ANAC website at https sistemas.anac.gov.br/certificacao/DA/
DAE.asp.
6 For Embraer service information identified in this AD, contact Embraer S.A., Technical Publications Section PC 060, Av.
Brigadeiro Faria Lima, 2170Putim12227
901 Sao Jose dos CamposSPBrazil;
telephone +55 12 39275852 or +55 12 3309
0732; fax +55 12 39277546; email distrib@
embraer.com.br; internet http
www.flyembraer.com. For Embraer service information that is applicable to Yabora Industria Aeronautica S.A. Model ERJ 190
100 ECJ airplanes, contact Embraer S.A., Technical Publications Section PC 560, Rodovia Presidente Dutra, km 134, 12247
004 Distrito Eugenio de MeloSao Jose dos CamposSPBrazil; telephone +55 12
39270386; email distrib@embraer.com.br;
internet https
www.mytechcare.embraer.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.
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 fr.inspection@nara.gov, or go to: https
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on November 24, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202127187 Filed 121521; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 107
Docket No. FAA20211158; Notice No.
1072101NOA

Accepted Means of Compliance;
Operations Over Human Beings, Category 2 and Category 3 Small Unmanned Aircraft Federal Aviation Administration, DOT.
ACTION: Notification of availability.
AGENCY:

This document announces the acceptance of a means of compliance MOC in accordance with a rule issued by the FAA on January 21, 2021, and went into effect on April 21, 2021. The Administrator finds the Virginia Tech
SUMMARY:

E:FRFM16DER1.SGM

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