Airworthiness Directives; Yaborã Indústria Aeronáutica S.A. (Type Certificate Previously Held by Embraer S.A.) Airplanes

Published date27 November 2020
Citation85 FR 75964
Record Number2020-26045
SectionProposed rules
CourtFederal Aviation Administration
Federal Register, Volume 85 Issue 229 (Friday, November 27, 2020)
[Federal Register Volume 85, Number 229 (Friday, November 27, 2020)]
                [Proposed Rules]
                [Pages 75964-75966]
                From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
                [FR Doc No: 2020-26045]
                [[Page 75964]]
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                DEPARTMENT OF TRANSPORTATION
                Federal Aviation Administration
                14 CFR Part 39
                [Docket No. FAA-2020-1035; Project Identifier MCAI-2020-01017-T]
                RIN 2120-AA64
                Airworthiness Directives; Yabor[atilde] Ind[uacute]stria
                Aeron[aacute]utica S.A. (Type Certificate Previously Held by Embraer
                S.A.) Airplanes
                AGENCY: Federal Aviation Administration (FAA), DOT.
                ACTION: Notice of proposed rulemaking (NPRM).
                -----------------------------------------------------------------------
                SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
                for certain Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A.
                Model EMB-135, EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -
                145EP airplanes. This proposed AD was prompted by reports that
                calculations provided by the automatic takeoff thrust control system
                (ATTCS) are incorrect under certain conditions. This proposed AD would
                require updating the software of the installed full authority digital
                engine control (FADEC) systems, as specified in an Ag[ecirc]ncia
                Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD, which will be
                incorporated by reference. The FAA is proposing this AD to address the
                unsafe condition on these products.
                DATES: The FAA must receive comments on this proposed AD by January 11,
                2021.
                ADDRESSES: You may send comments, using the procedures found in 14 CFR
                11.43 and 11.45, by any of the following methods:
                 Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
                 Fax: 202-493-2251.
                 Mail: U.S. Department of Transportation, Docket
                Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
                Jersey Avenue SE, Washington, DC 20590.
                 Hand Delivery: Deliver to Mail address above between 9
                a.m. and 5 p.m., Monday through Friday, except Federal holidays.
                 For ANAC material incorporated by reference (IBR) in this AD,
                contact National Civil Aviation Agency (ANAC), Aeronautical Products
                Certification Branch (GGCP), Rua Dr. Orlando Feirabend Filho, 230--
                Centro Empresarial Aquarius--Torre B--Andares 14 a 18, Parque
                Residencial Aquarius, CEP 12.246-190--S[atilde]o Jos[eacute] dos
                Campos--SP, BRAZIL, Tel: 55 (12) 3203-6600; Email: [email protected];
                internet www.anac.gov.br/en/. You may find this IBR material on the
                ANAC website at https://sistemas.anac.gov.br/certificacao/DA/DAE.asp.
                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 206-231-3195. It is also available in the AD docket on the
                internet at https://www.regulations.gov by searching for and locating
                Docket No. FAA-2020-1035.
                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. FAA-2020-
                1035; 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 NPRM, any comments received, and other information. The street
                address for Docket Operations is listed above. Comments will be
                available in the AD docket shortly after receipt.
                FOR FURTHER INFORMATION CONTACT: Kathleen Arrigotti, Aerospace
                Engineer, Large Aircraft Section, International Validation Branch, FAA,
                2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-
                3218; email [email protected].
                SUPPLEMENTARY INFORMATION:
                Comments Invited
                 The FAA invites you to participate in this rulemaking by submitting
                written comments, data, or views about this proposal. The most helpful
                comments reference a specific portion of the proposal, explain the
                reason for any recommended change, and include supporting data. To
                ensure the docket does not contain duplicate comments, commenters
                should send only one copy of written comments, or if comments are filed
                electronically, commenters should submit only one time. Send your
                comments to an address listed under the ADDRESSES section. Include
                ``Docket No. FAA-2020-1035; Project Identifier MCAI-2020-01017-T'' at
                the beginning of your comments.
                 Except for Confidential Business Information (CBI) as described in
                the following paragraph, and other information as described in 14 CFR
                11.35, the FAA will post all comments received, without change, as well
                as a report summarizing each substantive public contact with FAA
                personnel concerning this proposed rulemaking. Before acting on this
                proposal, the FAA will consider all comments received by the closing
                date for comments. The FAA will consider comments filed after the
                comment period has closed if it is possible to do so without incurring
                expense or delay. The FAA may change this NPRM because of those
                comments.
                Confidential Business Information
                 CBI is commercial or financial information that is both customarily
                and actually treated as private by its owner. Under the Freedom of
                Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
                disclosure. If your comments responsive to this NPRM contain commercial
                or financial information that is customarily treated as private, that
                you actually treat as private, and that is relevant or responsive to
                this NPRM, it is important that you clearly designate the submitted
                comments as CBI. Please mark each page of your submission containing
                CBI as ``PROPIN.'' The FAA will treat such marked submissions as
                confidential under the FOIA, and they will not be placed in the public
                docket of this NPRM. Submissions containing CBI should be sent to the
                person identified in the FOR FURTHER INFORMATION CONTACT section. Any
                commentary that the FAA receives which is not specifically designated
                as CBI will be placed in the public docket for this rulemaking.
                Discussion
                 The ANAC, which is the aviation authority for Brazil, has issued
                ANAC AD 2020-07-02, effective July 21, 2020 (``ANAC AD 2020-07-02'')
                (also referred to as the Mandatory Continuing Airworthiness
                Information, or ``the MCAI''), to correct an unsafe condition for
                certain Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A. Model
                EMB-135, EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP
                airplanes. Model EMB-145EU, EMB-145LU, and EMB-145MK airplanes are not
                certificated by the FAA and are not included on the U.S. type
                certificate data sheet; this AD therefore does not include those
                airplanes in the applicability.
                 This proposed AD was prompted by reports that calculations provided
                by the ATTCS do not take into consideration the required engine air
                bleed during operations with a single engine and anti-ice system on.
                The FAA is proposing this AD to address the risk of over-prediction of
                the operational margins, without the necessary alert being provided to
                the flightcrew in some situations. This condition, if not corrected,
                could lead to a performance reduction during takeoff, in which case
                [[Page 75965]]
                the aircraft may not be able to take off safely. See the MCAI for
                additional background information.
                Related Service Information Under 1 CFR Part 51
                 ANAC AD 2020-07-02 describes procedures for updating the software
                of the installed FADECs to version B9.4 or B9.4.1. This material is
                reasonably available because the interested parties have access to it
                through their normal course of business or by the means identified in
                the ADDRESSES section.
                FAA's Determination and Requirements of This Proposed AD
                 This product has been approved by the aviation authority of another
                country, and is approved for operation in the United States. Pursuant
                to the FAA's bilateral agreement with the State of Design Authority,
                the FAA has been notified of the unsafe condition described in the MCAI
                and service information referenced above. The FAA is proposing this AD
                because the FAA evaluated all the relevant information and determined
                the unsafe condition described previously is likely to exist or develop
                in other products of the same type design.
                Proposed AD Requirements
                 This proposed AD would require accomplishing the actions specified
                in ANAC AD 2020-07-02 described previously, as incorporated by
                reference, except for any differences identified as exceptions in the
                regulatory text of this AD.
                Explanation of Required Compliance Information
                 In the FAA's ongoing efforts to improve the efficiency of the AD
                process, the FAA initially worked with Airbus and the European Union
                Aviation Safety Agency (EASA) to develop a process to use certain EASA
                ADs as the primary source of information for compliance with
                requirements for corresponding FAA ADs. The FAA has since coordinated
                with other manufacturers and civil aviation authorities (CAAs) to use
                this process. As a result, ANAC AD 2020-07-02 will be incorporated by
                reference in the FAA final rule. This proposed AD would, therefore,
                require compliance with ANAC AD 2020-07-02 in its entirety, through
                that incorporation, except for any differences identified as exceptions
                in the regulatory text of this proposed AD. Service information
                specified in ANAC AD 2020-07-02 that is required for compliance with
                ANAC AD 2020-07-02 will be available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2020-
                1035 after the FAA final rule is published.
                Costs of Compliance
                 The FAA estimates that this proposed AD affects 494 airplanes of
                U.S. registry. The FAA estimates the following costs to comply with
                this proposed AD:
                 Estimated Costs for Required Actions
                ----------------------------------------------------------------------------------------------------------------
                 Cost per Cost on U.S.
                 Labor cost Parts cost product operators
                ----------------------------------------------------------------------------------------------------------------
                5 work-hours x $85 per hour = $425........................... $0 $425 $209,950
                ----------------------------------------------------------------------------------------------------------------
                Authority for This Rulemaking
                 Title 49 of the United States Code specifies the FAA's authority to
                issue rules on aviation safety. Subtitle I, section 106, describes the
                authority of the FAA Administrator. Subtitle VII: Aviation Programs,
                describes in more detail the scope of the Agency's authority.
                 The FAA is issuing this rulemaking under the authority described in
                Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
                Under that section, Congress charges the FAA with promoting safe flight
                of civil aircraft in air commerce by prescribing regulations for
                practices, methods, and procedures the Administrator finds necessary
                for safety in air commerce. This regulation is within the scope of that
                authority because it addresses an unsafe condition that is likely to
                exist or develop on products identified in this rulemaking action.
                Regulatory Findings
                 The FAA determined that this proposed AD would not have federalism
                implications under Executive Order 13132. This proposed AD would not
                have a substantial direct effect on the States, on the relationship
                between the national Government and the States, or on the distribution
                of power and responsibilities among the various levels of government.
                 For the reasons discussed above, I certify this proposed
                regulation:
                 (1) Is not a ``significant regulatory action'' under Executive
                Order 12866,
                 (2) Will not affect intrastate aviation in Alaska, and
                 (3) Will not have a significant economic impact, positive or
                negative, on a substantial number of small entities under the criteria
                of the Regulatory Flexibility Act.
                List of Subjects in 14 CFR Part 39
                 Air transportation, Aircraft, Aviation safety, Incorporation by
                reference, Safety.
                The Proposed Amendment
                 Accordingly, under the authority delegated to me by the
                Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
                PART 39--AIRWORTHINESS DIRECTIVES
                0
                1. The authority citation for part 39 continues to read as follows:
                 Authority: 49 U.S.C. 106(g), 40113, 44701.
                Sec. 39.13 [Amended]
                0
                2. The FAA amends Sec. 39.13 by adding the following new airworthiness
                directive (AD):
                Yabor[atilde] Ind[uacute]stria Aeron[aacute]utica S.A. (Type
                Certificate Previously Held by Embraer S.A.): Docket No. FAA-2020-
                1035; Project Identifier MCAI-2020-01017-T.
                (a) Comments Due Date
                 The FAA must receive comments by January 11, 2021.
                (b) Affected ADs
                 None.
                (c) Applicability
                 This AD applies to Yabor[atilde] Ind[uacute]stria
                Aeron[aacute]utica S.A. Model EMB-135BJ, -135ER, -135KE, -135KL, and
                -135LR airplanes, EMB-145, -45ER, -145MR, -145LR, -145XR, -145MP,
                and -145EP, certificated in any category, as identified in
                Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC) AD
                2020-07-02, effective July 21, 2020 (``ANAC AD 2020-07-02'').
                (d) Subject
                 Air Transport Association (ATA) of America Code 73, Engine fuel
                and control.
                (e) Reason
                 This AD was prompted by reports that calculations provided by
                the automatic takeoff thrust control system (ATTCS) are incorrect
                under certain conditions. The FAA is issuing this AD to address the
                risk of over-prediction of the operational margins,
                [[Page 75966]]
                without the necessary alert being provided to the flightcrew in some
                situations. This condition, if not corrected, could lead to a
                performance reduction during takeoff, in which case the airplane may
                not be able to take off safely.
                (f) Compliance
                 Comply with this AD within the compliance times specified,
                unless already done.
                (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, ANAC AD 2020-07-02.
                (j) Exceptions to ANAC AD 2020-07-02
                 (1) Where ANAC AD 2020-07-02 refers to its effective date, this
                AD requires using the effective date of this AD.
                 (2) The ``Alternative method of compliance (AMOC)'' section of
                ANAC AD 2020-07-02 does not apply to this AD.
                (k) 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 (l)(2) of
                this AD. Information may be emailed to: [email protected].
                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 ANAC's
                authorized Designee. If approved by the ANAC Designee, the approval
                must include the Designee's authorized signature.
                (l) Related Information
                 (1) For information about ANAC AD 2020-07-02, contact National
                Civil Aviation Agency (ANAC), Aeronautical Products Certification
                Branch (GGCP), Rua Dr. Orlando Feirabend Filho, 230--Centro
                Empresarial Aquarius--Torre B--Andares 14 a 18, Parque Residencial
                Aquarius, CEP 12.246-190--S[atilde]o Jos[eacute] dos Campos--SP,
                BRAZIL, Tel: 55 (12) 3203-6600; Email: [email protected]; internet
                www.anac.gov.br/en/. You may find this IBR material on the ANAC
                website at https://sistemas.anac.gov.br/certificacao/DA/DAE.asp. 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
                206-231-3195. This material may be found in the AD docket on the
                internet at https://www.regulations.gov by searching for and
                locating Docket No. FAA-2020-1035.
                 (2) 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 206-231-3218; email [email protected].
                 Issued on November 19, 2020.
                Lance T. Gant,
                Director, Compliance & Airworthiness Division, Aircraft Certification
                Service.
                [FR Doc. 2020-26045 Filed 11-25-20; 8:45 am]
                BILLING CODE 4910-13-P
                

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