2023-16383. Airworthiness Directives; Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.) Airplanes  

  • Start Preamble

    AGENCY:

    Federal Aviation Administration (FAA), DOT.

    ACTION:

    Final rule; request for comments.

    SUMMARY:

    The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. Model ERJ 190–300 and –400 airplanes. This AD was prompted by reports of missing parts on the main landing gear (MLG) side stay upper spindle assembly. This AD requires inspection of the left-hand (LH) and right-hand (RH) MLG side stay upper spindle assembly attachments, and corrective actions if necessary, as specified in an Agência Nacional de Aviação Civil (ANAC) 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 August 18, 2023.

    The Director of the Federal Register approved the incorporation by reference of a certain publications listed in this AD as of August 18, 2023.

    The FAA must receive comments on this AD by September 18, 2023.

    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 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.

    AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2023–1636; 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, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above.

    Material Incorporated by Reference:

    • For material incorporated by reference 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—São José dos Campos—SP, Brazil; telephone 55 (12) 3203–6600; email pac@anac.gov.br; website anac.gov.br/en/. You may find this material on the ANAC website at sistemas.anac.gov.br/certificacao/DA/DAE.asp.

    • You may view this service information 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 at regulations.gov under Docket No. FAA–2023–1636.

    Start Further Info

    FOR FURTHER INFORMATION CONTACT:

    Joshua Bragg, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 216–316–6418; email joshua.k.bragg@faa.gov.

    End Further Info End Preamble Start Supplemental Information

    SUPPLEMENTARY INFORMATION:

    Comments Invited

    The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments to an address listed under ADDRESSES . Include “Docket No. FAA–2023–1636; Project Identifier MCAI–2023–00369–T” at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this final rule because of those 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, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this final rule.

    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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to Joshua Bragg, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 216–316–6418; email joshua.k.bragg@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.

    Background

    ANAC, which is the aviation authority for Brazil, has issued ANAC AD 2023–02–02R1, effective May 10, 2023 (ANAC AD 2023–02–02R1) (also referred to as the MCAI), to correct an unsafe condition for certain Embraer S.A. Model ERJ 190–300 and –400 airplanes. The MCAI states that it was prompted by reports of missing parts on the main landing gear (MLG) side stay upper spindle assembly, which may compromise the locking and holding of the MLG side stay in its correct kinematics position.

    The FAA is issuing this AD to address a possible failure of MLG locking elements, which could cause non-annunciated loss of downlocking capability and collapse of the MLG structure during takeoff or landing.

    You may examine the MCAI in the AD docket at regulations.gov under Docket No. FAA–2023–1636. Start Printed Page 51226

    Related Service Information Under 1 CFR Part 51

    ANAC AD 2023–02–02R1 specifies procedures for a general visual inspection of the LH and RH MLG side stay upper spindle assembly attachments to determine if certain bolts, washers, locknuts, and cotter pins are correctly installed; a detailed inspection to measure the clearance between the spindle shoulder and the bushing flange and the clearance between the bushing flange and the washer on the MLG side stay upper spindle; and corrective actions including replacement with new parts and removal, reinstallation, and retorquing of the MLG side stay upper spindle. 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

    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 this State of Design Authority, it has notified the FAA of the unsafe condition described in the MCAI referenced above. The FAA is issuing this AD after determining that the unsafe condition described previously is likely to exist or develop on other products of the same type design.

    Requirements of This AD

    This AD requires accomplishing the actions specified in ANAC AD 2023–02–02R1 described previously, 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 developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, ANAC AD 2023–02–02R1 is incorporated by reference in this AD. This AD requires compliance with ANAC AD 2023–02–02R1 in its entirety through that incorporation, except for any differences identified as exceptions in the regulatory text of this AD. Service information required by ANAC AD 2023–02–02R1 for compliance will be available at regulations.gov under Docket No. FAA–2023–1636 after this AD is published.

    FAA's Justification and Determination of the Effective Date

    Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq.) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for “good cause,” finds that those procedures are “impracticable, unnecessary, or contrary to the public interest.” Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than thirty days, upon a finding of good cause.

    There are currently no domestic operators of these products. Accordingly, notice and opportunity for prior public comment are unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the forgoing reason(s), the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days.

    Regulatory Flexibility Act (RFA)

    The requirements of the RFA do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because the FAA has determined that it has good cause to adopt this rule without notice and comment, RFA analysis is not required.

    Costs of Compliance

    Currently, there are no affected U.S.-registered airplanes. If an affected airplane is imported and placed on the U.S. Register in the future, the FAA provides the following cost estimates to comply with this AD:

    Estimated Costs for Required Actions

    Labor costParts costCost per product
    1 work-hour × $85 per hour = $85$0$85

    The FAA estimates the following costs to do any necessary on-condition action[s] that would be required based on the results of any required actions. The FAA has no way of determining the number of aircraft that might need these on-condition actions:

    Estimated Costs of On-Condition Actions

    Labor costParts costCost per product
    2 work-hours × $85 per hour = $170* $0$170
    * Operator supplied parts that are in existing inventory, non-significant cost.

    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 Start Printed Page 51227 develop on products identified in this rulemaking action.

    Regulatory Findings

    This AD will not have federalism implications under Executive Order 13132. This AD will 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 that this AD:

    (1) Is not a “significant regulatory action” under Executive Order 12866, and

    (2) Will not affect intrastate aviation in Alaska.

    Start List of Subjects

    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
    End List of Subjects

    The Amendment

    Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

    Start Part

    PART 39—AIRWORTHINESS DIRECTIVES

    End Part Start Amendment Part

    1. The authority citation for part 39 continues to read as follows:

    End Amendment Part Start Authority

    Authority: 49 U.S.C. 106(g), 40113, 44701.

    End Authority
    [Amended]
    Start Amendment Part

    2. The FAA amends § 39.13 by adding the following new airworthiness directive:

    End Amendment Part

    2023–15–02 Embraer S.A. (Type Certificate Previously Held by Yaborã Indústria Aeronáutica S.A.; Embraer S.A.): Amendment 39–22514; Docket No. FAA–2023–1636; Project Identifier MCAI–2023–00369–T.

    (a) Effective Date

    This airworthiness directive (AD) is effective August 18, 2023.

    (b) Affected ADs

    None.

    (c) Applicability

    This AD applies to Embraer S.A. Model ERJ 190–300 and –400 airplanes, certificated in any category, as identified in Agência Nacional de Aviação Civil (ANAC) AD 2023–02–02R1, effective May 10, 2023 (ANAC AD 2023–02–02R1).

    (d) Subject

    Air Transport Association (ATA) of America Code 32, Landing gear.

    (e) Unsafe Condition

    This AD was prompted by reports of missing parts on the main landing gear (MLG) side stay upper spindle assembly. The FAA is issuing this AD to address a possible failure of MLG locking elements, which could cause non-annunciated loss of downlocking capability and collapse of the MLG structure during takeoff or landing.

    (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 2023–02–02R1.

    (h) Exceptions to ANAC AD 2023–02–02R1

    (1) Where ANAC AD 2023–02–02R1 refers to “01 Mar. 2023, the effective date of the original issue of this AD,” this AD requires using the effective date of this AD.

    (2) Where ANAC AD 2023–02–02R1 refers to its effective date, this AD requires using the effective date of this AD.

    (3) The “Alternative methods of compliance (AMOC)” section of ANAC AD 2023–02–02R1 does not apply to this AD.

    (i) Additional AD Provisions

    The following provisions also apply to this AD:

    (1) Alternative Methods of Compliance (AMOCs): The Manager, 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 International Validation Branch, send it to the attention of the person identified in paragraph (j) of this AD. Information may be emailed to: 9-AVS-AIR-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, 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.

    (j) Additional Information

    For more information about this AD, contact Joshua Bragg, Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 216–316–6418; email joshua.k.bragg@faa.gov.

    (k) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the incorporation by reference of the service information listed in this paragraph under 5 U.S.C. 552(a) 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.

    (i) Agência Nacional de Aviação Civil (ANAC) AD 2023–02–02R1, effective May 10, 2023.

    (ii) [Reserved]

    (3) For ANAC AD 2023–02–02R1, 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—São José dos Campos—SP, Brazil; telephone 55 (12) 3203–6600; email: pac@anac.gov.br; internet anac.gov.br/en/. You may find this ANAC AD on the ANAC website at sistemas.anac.gov.br/certificacao/DA/DAE.asp.

    (4) 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.

    (5) 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: www.archives.gov/​federal-register/​cfr/​ibr-locations.html.

    Start Signature

    Issued on July 19, 2023.

    Victor Wicklund,

    Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service.

    End Signature End Supplemental Information

    [FR Doc. 2023–16383 Filed 8–2–23; 8:45 am]

    BILLING CODE 4910–13–P

Document Information

Effective Date:
8/18/2023
Published:
08/03/2023
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; request for comments.
Document Number:
2023-16383
Dates:
This AD is effective August 18, 2023.
Pages:
51225-51227 (3 pages)
Docket Numbers:
Docket No. FAA-2023-1636, Project Identifier MCAI-2023-00369-T, Amendment 39-22514, AD 2023-15-02
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
Topics:
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
PDF File:
2023-16383.pdf
Supporting Documents:
» U.S. DOT/FAA - Supplemental AD Documents
CFR: (1)
14 CFR 39.13