2024-06032. Airworthiness Directives; AVOX Systems Inc. (Formerly Scott Aviation) Oxygen Cylinder and Valve Assemblies; and Oxygen Valve Assemblies  

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    AGENCY:

    Federal Aviation Administration (FAA), DOT.

    ACTION:

    Notice of proposed rulemaking (NPRM).

    SUMMARY:

    The FAA proposes to supersede Airworthiness Directive (AD) 2023–13–11, which applies to certain AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies; and oxygen valve assemblies; installed on but not limited to various transport airplanes. AD 2023–13–11 requires an inspection of the oxygen valve assemblies, and oxygen cylinder and valve assemblies, to determine the serial number of the valve, cylinder, and entire assembly; and for certain assemblies and parts, a detailed inspection for correct spacing of the gap between the bottom of the packing retainer and top of the valve body on the assemblies and replacement of assemblies having unacceptable gaps. AD 2023–13–11 also limits the installation of affected parts under certain conditions and requires reporting inspection results and returning certain assemblies to the manufacturer. Since the FAA issued AD 2023–13–11, the manufacturer identified additional assemblies and parts subject to the unsafe condition. This proposed AD would continue to require the actions specified in AD 2023–13–11 and require similar actions for those additional assemblies and parts. 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 May 9, 2024.

    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–2024–0759; 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.

    Material Incorporated by Reference:

    • For service information identified in this NPRM, contact AVOX Systems Inc., 225 Erie Street, Lancaster, NY 14086; telephone 716–683–5100; website safranaerosystems.com.

    • 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.
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    FOR FURTHER INFORMATION CONTACT:

    Gabriel Kim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7343; email 9-avs-nyaco-cos@faa.gov.

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    SUPPLEMENTARY INFORMATION:

    Comments Invited

    The FAA invites you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under ADDRESSES . Include “Docket No. FAA–2024–0759; Project Identifier AD–2023–01040–T” at the beginning of your comments. The most helpful comments reference a specific portion of the proposal, 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 the proposal 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 proposed AD.

    Confidential Business Information

    CBI is commercial or financial information that is both customarily and Start Printed Page 20559 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 Gabriel Kim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7343; email 9-avs-nyaco-cos@faa.gov. Any commentary that the FAA receives that is not specifically designated as CBI will be placed in the public docket for this rulemaking.

    Background

    The FAA issued AD 2023–13–11, Amendment 39–22496 (88 FR 50011, August 1, 2023) (AD 2023–13–11), for certain AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies; and oxygen valve assemblies; installed on but not limited to various transport airplanes. AD 2023–13–11 was prompted by reports of cylinder and valve assemblies having oxygen leakage from the valve assembly vent hole, caused by the absence of a guide that maintains appropriate spacing between certain parts, and by a determination that additional assemblies and parts are affected by the unsafe condition addressed by AD 2022–04–09, Amendment 39–21951 (87 FR 10958, February 28, 2022) (AD 2022–04–09) (which was superseded by AD 2023–13–11). AD 2023–13–11 requires an inspection of the oxygen valve assemblies, and oxygen cylinder and valve assemblies, to determine the serial number of the valve, cylinder, and entire assembly. For assemblies and parts with certain serial numbers, AD 2023–13–11 also requires a detailed inspection for correct spacing of the gap between the bottom of the packing retainer and top of the valve body on the assemblies, and replacement of assemblies having unacceptable gaps. AD 2023–13–11 also limits the installation of affected parts under certain conditions and requires reporting inspection results and returning certain assemblies to the manufacturer. The agency issued AD 2023–13–11 to address oxygen leakage from the cylinder and valve assemblies, which could result in decreased or insufficient oxygen supply during a depressurization event; and heating or flow friction, which could cause an ignition event in the valve assembly.

    Actions Since AD 2023–13–11 Was Issued

    Since the FAA issued AD 2023–13–11, the manufacturer identified additional assemblies and parts, including a new part number 89794050 for oxygen cylinder and valve assemblies, that are subject to the unsafe condition. New service information has been issued that expands the population of discrepant parts, providing more serial numbers for which to inspect.

    FAA's Determination

    The FAA is issuing this NPRM after determining that the unsafe condition described previously is likely to exist or develop on other products of the same type design.

    Related Service Information Under 1 CFR Part 51

    The FAA reviewed the following service information. This service information specifies procedures for an inspection to determine the serial numbers of the oxygen cylinder and valve assemblies, and the oxygen valve assemblies, a detailed inspection for correct spacing of the gap between the bottom of the packing retainer and top of the valve body on the assemblies, parts marking, inspection report, and return of parts to the manufacturer. These documents are distinct since they apply to different assembly part numbers.

    • AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 04, dated November 9, 2023.
    • AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 06, dated August 30, 2023.
    • AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 05, dated September 29, 2023.

    This AD also requires the following service information, which the Director of the Federal Register approved for incorporation by reference as of September 5, 2023 (88 FR 50011, August 1, 2023).

    • AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 03, dated June 7, 2021.
    • AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 03, dated March 11, 2022.
    • AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 03, dated June 18, 2021.

    This service information 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.

    Proposed AD Requirements in This NPRM

    This proposed AD would retain all of the requirements of AD 2023–13–11. This proposed AD would apply to additional assemblies and parts, including a new part number, 89794050, for oxygen cylinder and valve assemblies. This proposed AD would require accomplishing the actions specified in the service information described previously. This proposed AD would also limit the installation of affected parts under certain conditions and require returning the affected parts and sending the inspection results to the manufacturer.

    Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would affect 3,777 oxygen cylinder and valve assemblies, and oxygen valve assemblies, installed on various transport category airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD:

    Estimated Costs

    ActionLabor costParts costCost per productCost on U.S. operators
    Serial number inspection (retained action from AD 2023-13-11)1 work-hour × $85 per hour = $85None$85$321, 045
    Reporting (retained action from AD 2023–13–11)1 work-hour × $85 per hour = $85$085321,045
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    The FAA estimates the following costs to do any necessary actions that would be required based on the results of the proposed inspection. The FAA has no way of determining the number of aircraft that might need these actions:

    On-Condition Costs

    ActionLabor costParts costCost per product
    Detailed inspection1 work-hour × $85 per hour = $85$0$85
    Replacement1 work-hour × $85 per hour = $85(*)85
    Return of parts1 work-hour × $85 per hour = $85** 50135
    * The FAA has received no definitive data on the parts cost for the on-condition replacement.
    ** The FAA has received no definitive data to provide cost estimates for the on-condition return of parts, except the FAA estimates that it would take about 1 work-hour per product to comply with the associated paperwork necessary for the return of parts and cost approximately $50 to ship.

    The FAA has included all known costs in its cost estimate. According to the manufacturer, however, some or all of the costs of this proposed AD may be covered under warranty, thereby reducing the cost impact on affected operators.

    Paperwork Reduction Act

    A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a currently valid OMB Control Number. The OMB Control Number for this information collection is 2120–0056. Public reporting for this collection of information is estimated to be approximately 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden to: Information Collection Clearance Officer, Federal Aviation Administration, 10101 Hillwood Parkway, Fort Worth, TX 76177–1524.

    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 has 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 that the proposed regulation:

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

    (2) Would not affect intrastate aviation in Alaska, and

    (3) Would not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act.

    Start List of Subjects

    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
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    The Proposed Amendment

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

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    PART 39—AIRWORTHINESS DIRECTIVES

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

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

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    [Amended]
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    2. The FAA amends § 39.13 by:

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    a. Removing Airworthiness Directive (AD) 2023–13–11, Amendment 39–22496 ( 88 FR 50011, August 1, 2023), and

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    b. Adding the following new AD:

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    AVOX Systems Inc. (formerly Scott Aviation): Docket No. FAA–2024–0759; Project Identifier AD–2023–01040–T

    (a) Comments Due Date

    The FAA must receive comments on this airworthiness directive (AD) by May 9, 2024.

    (b) Affected ADs

    This AD replaces AD 2023–13–11, Amendment 39–22496 (88 FR 50011, August 1, 2023) (AD 2023–13–11).

    (c) Applicability

    This AD applies to AVOX Systems Inc. (formerly Scott Aviation) oxygen cylinder and valve assemblies having part number (P/N) 89794050, 89794077, 89794015, 891511–14, 806835–01, 807982–01, 808433–01, or 891311–14; and oxygen valve assemblies (body and gage assemblies) having P/N 807206–01. These assemblies might be installed on, but not limited to, the aircraft identified in paragraphs (c)(1) through (12) of this AD, certificated in any category.

    (1) Airbus SAS Model A300 B2–1A, B2–1C, B2K–3C, B2–203, B4–2C, B4–103, and B4–203 airplanes.

    (2) Airbus SAS Model A300 B4–601, B4–603, B4–620, B4–622, B4–605R, B4–622R, F4–605R, F4–622R, and C4–605R Variant F airplanes.

    (3) Airbus SAS Model A310–203, –204, –221, –222, –304, –322, –324, and –325 airplanes.

    (4) Airbus SAS Model A318–111, –112, –121, and –122 airplanes.

    (5) Airbus SAS Model A319–111, –112, –113, –114, –115, –131, –132, –133, and –151N airplanes.

    (6) Airbus SAS Model A320–211, –212, –214, –216, –231, –232, –233, –251N, –252N, –253N, –271N, –272N, and –273N airplanes.

    (7) Airbus SAS Model A321–111, –112, –131, –211, –212, –213, –231, –232, –251N, –252N, –253N, –271N, –272N, –251NX, –252NX, –253NX, –271NX, and –272NX airplanes.

    (8) Airbus SAS Model A330–201, –202, –203, –223, –243, –301, –302, –303, –321, –322, –323, –341, –342, –343, and –941 airplanes. Start Printed Page 20561

    (9) Airbus Model A340–211, –212, –213, –311, –312, –313, –541, and –642 airplanes.

    (10) ATR—GIE Avions de Transport Régional Model ATR42–200, –300, –320, and –500 airplanes.

    (11) ATR—GIE Avions de Transport Régional Model ATR72–101, –102, –201, –202, –211, –212, and –212A airplanes.

    (12) The Boeing Company Model 747–8 series airplanes.

    (d) Subject

    Air Transport Association (ATA) of America Code 35, Oxygen.

    (e) Unsafe Condition

    This AD was prompted by reports of cylinder and valve assemblies having oxygen leakage from the valve assembly vent hole, caused by the absence of a guide that maintains appropriate spacing between certain parts, and by the manufacturer identifying additional assemblies and parts affected by the unsafe condition. The FAA is issuing this AD to address oxygen leakage from cylinder and valve assemblies. The unsafe condition, if not addressed, could result in decreased or insufficient oxygen supply during a depressurization event; and heating or flow friction, which could cause an ignition event in the valve assembly.

    (f) Compliance

    Comply with this AD within the compliance times specified, unless already done.

    (g) Retained Definition of Detailed Inspection, With No Changes

    This paragraph restates the requirements of paragraph (g) of AD 2023–13–11, with no changes. For the purposes of this AD, a detailed inspection is an intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required.

    (h) Retained Identification of Affected Cylinder and Valve Assemblies, With No Changes

    This paragraph restates the requirements of paragraph (h) of AD 2023–13–11, with no changes. Within 60 days after September 5, 2023 (the effective date of AD 2023–13–11), inspect the oxygen valve assemblies, and oxygen cylinder and valve assemblies, to determine if the serial numbers of the valve, cylinder, and entire assembly, are listed in Appendix 1 or Appendix 2, “Affected Shipments,” of the applicable service information identified in paragraphs (h)(1) through (3) of this AD. A review of airplane maintenance records is acceptable in lieu of this inspection if the serial numbers can be conclusively determined from that review.

    (1) AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 03, dated June 7, 2021.

    (2) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 03, dated March 11, 2022.

    (3) AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 03, dated June 18, 2021.

    (i) Retained Inspection of the Gap, Parts Marking Actions, and Replacement, With No Changes

    This paragraph restates the requirements of paragraph (i) of AD 2023–13–11, with no changes. If, during any inspection or records review required by paragraph (h) of this AD, any oxygen valve assembly, valve or cylinder of an oxygen cylinder and valve assembly, or oxygen cylinder and valve assembly having an affected serial number is found: Before further flight, do a detailed inspection for correct spacing of the gap between the bottom of the packing retainer and top of the valve body, in accordance with paragraph 3.C. of the Accomplishment Instructions of the applicable service information identified in paragraphs (h)(1) through (3) of this AD.

    (1) If the gap is found to be acceptable, as defined in the applicable service information identified in paragraphs (h)(1) through (3) of this AD, before further flight, do the parts marking actions in accordance with paragraph 3.D.(1) of the Accomplishment Instructions of the applicable service information identified in paragraphs (h)(1) through (3) of this AD.

    (2) If the gap is found to be unacceptable, as defined in the applicable service information identified in paragraphs (h)(1) through (3) of this AD, before further flight, remove the affected assembly, in accordance with paragraphs 3.D.(2) or 3.D.(3), as applicable, of the Accomplishment Instructions of the applicable service information identified in paragraphs (h)(1) through (3) of this AD; and replace with a serviceable assembly.

    (j) Retained Reporting and Return of Parts, With No Changes

    This paragraph restates the requirements of paragraph (j) of AD 2023–13–11, with no changes.

    (1) Report the results of the inspection required by paragraph (i) of this AD within the applicable time specified in paragraph (j)(1)(i) or (ii) of this AD. Report the results in accordance with paragraph 3.D.(1)(a) of the Accomplishment Instructions of the applicable service information identified in paragraphs (h)(1) through (3) of this AD.

    (i) If the inspection was done on or after September 5, 2023 (the effective date of AD 2023–13–11): Submit the report within 30 days after the inspection.

    (ii) If the inspection was done before September 5, 2023 (the effective date of AD 2023–13–11): Submit the report within 30 days after September 5, 2023.

    (2) If, during the inspection required by paragraph (i) of this AD, any gap is found to be unacceptable, within the applicable time specified in paragraph (j)(2)(i) or (ii) of this AD, return the assembly to the manufacturer in accordance with paragraph 3.D.(2) or 3.D.(3), as applicable, of the Accomplishment Instructions of the applicable service information identified in paragraphs (h)(1) through (3) of this AD, except you are not required to contact AVOX Systems Inc. for shipping instructions.

    (i) If the inspection was done on or after September 5, 2023 (the effective date of AD 2023–13–11): Return the assembly within 30 days after the inspection.

    (ii) If the inspection was done before September 5, 2023 (the effective date of AD 2023–13–11): Return the assembly within 30 days after September 5, 2023.

    (k) Retained Parts Installation Limitation, With No Changes

    This paragraph restates the requirements of paragraph (k) of AD 2023–13–11, with no changes. As of September 5, 2023 (the effective date of AD 2023–13–11), no AVOX Systems Inc. oxygen valve assembly, or valve or cylinder that is part of an oxygen cylinder and valve assembly, or oxygen cylinder and valve assembly having an affected serial number identified in Appendix 1, “Affected Shipments,” or Appendix 2, “Affected Shipments,” of any AVOX Systems Inc. service information identified in paragraphs (h)(1) through (3) of this AD may be installed on any airplane unless the requirements of paragraph (i) of this AD have been accomplished on that affected assembly.

    (l) New Identification of Additional Affected Cylinder and Valve Assemblies

    Within 60 days after the effective date of this AD, inspect the oxygen valve assemblies, and oxygen cylinder and valve assemblies, to determine if the serial numbers of the valve, cylinder, and entire assembly, are listed in Appendix 3, “Affected Shipments,” of the applicable service information identified in paragraphs (l)(1) through (3) of this AD. A review of airplane maintenance records is acceptable in lieu of this inspection if the serial numbers can be conclusively determined from that review.

    (1) AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 04, dated November 9, 2023.

    (2) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 06, dated August 30, 2023.

    (3) AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 05, dated September 29, 2023.

    (m) New Inspection of the Gap, Parts Marking Actions, and Replacement for Additional Parts

    If, during any inspection or records review required by paragraph (l) of this AD, any oxygen valve assembly, valve or cylinder of an oxygen cylinder and valve assembly, or oxygen cylinder and valve assembly having an affected serial number is found: Before further flight, do a detailed inspection for correct spacing of the gap between the bottom of the packing retainer and top of the valve body, in accordance with paragraph 3.C. of the Accomplishment Instructions of the applicable service information identified in paragraphs (l)(1) through (3) of this AD.

    (1) If the gap is found to be acceptable, as defined in the applicable service information identified in paragraphs (l)(1) through (3) of this AD, before further flight, do the parts marking actions in accordance with paragraph 3.D.(1) of the Accomplishment Instructions of the applicable service information identified in paragraphs (l)(1) through (3) of this AD. Start Printed Page 20562

    (2) If the gap is found to be unacceptable, as defined in the applicable service information identified in paragraphs (l)(1) through (3) of this AD, before further flight, remove the affected assembly, in accordance with paragraphs 3.D.(2) or 3.D.(3), as applicable, of the Accomplishment Instructions of the applicable service information identified in paragraphs (l)(1) through (3) of this AD; and replace with a serviceable assembly.

    (n) New Reporting and Return of Additional Parts

    (1) Report the results of the inspection required by paragraph (m) of this AD within the applicable time specified in paragraph (n)(1)(i) or (ii) of this AD. Report the results in accordance with paragraph 3.D.(1)(a) of the Accomplishment Instructions of the applicable service information identified in paragraphs (l)(1) through (3) of this AD.

    (i) If the inspection was done on or after the effective date of this AD: Submit the report within 30 days after the inspection.

    (ii) If the inspection was done before the effective date of this AD: Submit the report within 30 days after the effective date of this AD.

    (2) If, during the inspection required by paragraph (m) of this AD, any gap is found to be unacceptable, within the applicable time specified in paragraph (n)(2)(i) or (ii) of this AD, return the assembly to the manufacturer in accordance with paragraph 3.D.(2) or 3.D.(3), as applicable, of the Accomplishment Instructions of the applicable service information identified in paragraphs (l)(1) through (3) of this AD, except you are not required to contact AVOX Systems Inc. for shipping instructions.

    (i) If the inspection was done on or after the effective date of this AD: Return the assembly within 30 days after the inspection.

    (ii) If the inspection was done before the effective date of this AD: Return the assembly within 30 days after the effective date of this AD.

    (o) New Parts Installation Limitation

    As of the effective date of this AD, no AVOX Systems Inc. oxygen valve assembly, or valve or cylinder that is part of an oxygen cylinder and valve assembly, or oxygen cylinder and valve assembly having an affected serial number identified in Appendix 3, “Affected Shipments,” of any AVOX Systems Inc. service information identified in paragraphs (l)(1) through (3) of this AD may be installed on any airplane unless the requirements of paragraph (m) of this AD have been accomplished on that affected assembly.

    (p) Credit for Previous Actions

    (1) This paragraph provides credit for the actions specified in paragraphs (h) or (i) of this AD, if those actions were performed before September 5, 2023 (the effective date of AD 2023–13–11), using the service information specified in paragraphs (p)(1)(i) through (iii) of this AD. This service information is not incorporated by reference in this AD.

    (i) AVOX Systems Inc. Service Bulletin 10015804–35–01, dated March 6, 2019; and AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 01, dated July 9, 2019.

    (ii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 1, dated September 4, 2019.

    (iii) AVOX Systems Inc. Service Bulletin 10015804–35–03, dated April 11, 2019; and AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 01, dated May 21, 2019.

    (2) This paragraph provides credit for the actions specified in paragraphs (h) or (i) of this AD, if those actions were performed before September 5, 2023 (the effective date of AD 2023–13–11), using the service information specified in paragraphs (p)(2)(i) through (iii) of this AD, which was incorporated by reference in AD 2022–04–09.

    (i) AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 02, dated October 16, 2019.

    (ii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 2, dated October 31, 2019.

    (iii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 02, dated October 15, 2019.

    (3) This paragraph provides credit for the actions specified in paragraphs (h), (i), (l), or (m) of this AD, if those actions were performed before the effective date of this AD, using the service information specified in paragraphs (p)(3)(i) through (ii) of this AD. This service information is not incorporated by reference in this AD.

    (i) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 04, dated June 30, 2023; or Revision 05, dated August 14, 2023.

    (ii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 04, dated June 12, 2023.

    (q) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, East Certification 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 manager of the East Certification Branch, send it to ATTN: Program Manager, Continuing Operational Safety, at the address identified in paragraph (r) of this AD or email to: 9-avs-nyaco-cos@faa.gov.

    (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.

    (3) AMOCs approved for AD 2023–13–11 are approved as AMOCs for the corresponding provisions of this AD.

    (r) Related Information

    (1) For more information about this AD, contact Gabriel Kim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516–228–7343; email 9-avs-nyaco-cos@faa.gov.

    (2) Service information identified in this AD that is not incorporated by reference is available at the address specified in paragraph (s)(5) of this AD.

    (s) 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. 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.

    (3) The following service information was approved for IBR on [DATE 35 DAYS AFTER PUBLICATION OF THE FINAL RULE].

    (i) AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 04, dated November 9, 2023.

    (ii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 06, dated August 30, 2023.

    (iii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 05, dated September 29, 2023.

    (4) The following service information was approved for IBR on September 5, 2023 (88 FR 50013, August 1, 2023).

    (i) AVOX Systems Inc. Alert Service Bulletin 10015804–35–01, Revision 03, dated June 7, 2021.

    (ii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–02, Revision 03, dated March 11, 2022.

    (iii) AVOX Systems Inc. Alert Service Bulletin 10015804–35–03, Revision 03, dated June 18, 2021.

    (5) For service information identified in this AD, contact AVOX Systems Inc., 225 Erie Street, Lancaster, NY 14086; telephone 716–683–5100; website safranaerosystems.com.

    (6) 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.

    (7) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/​federal-register/​cfr/​ibr-locations or email fr.inspection@nara.gov.

    Start Signature

    Issued on March 18, 2024.

    Victor Wicklund,

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

    End Signature End Supplemental Information

    [FR Doc. 2024–06032 Filed 3–22–24; 8:45 am]

    BILLING CODE 4910–13–P

Document Information

Published:
03/25/2024
Department:
Federal Aviation Administration
Entry Type:
Proposed Rule
Action:
Notice of proposed rulemaking (NPRM).
Document Number:
2024-06032
Dates:
The FAA must receive comments on this proposed AD by May 9, 2024.
Pages:
20558-20562 (5 pages)
Docket Numbers:
Docket No. FAA-2024-0759, Project Identifier AD-2023-01040-T
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:
2024-06032.pdf
CFR: (1)
14 CFR 39.13