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PROPOSED AD 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) hav-
    ing 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.

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

(10) ATR-GIE Avions de Transport Regional Model ATR42-200, -300, -320, and
     -500 airplanes.

(11) ATR-GIE  Avions de Transport  Regional  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 hav-
    ing 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 al-
    ready 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 in-
    spection 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 informa-
    tion identified in paragraphs (h)(1) through (3) of this AD.

(i) If the inspection was done on  or after September 5, 2023  (the effec-
    tive 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 Sep-
     tember 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 effec-
    tive 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 Sep-
     tember 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 ASSEM-
    BLIES

    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.

(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: Sub-
     mit 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: Re-
     turn 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 in-
    spector, or lacking a principal inspector,  the manager of the respon-
    sible Flight Standards Office.

(3) AMOCs approved  for AD 2023-13-11 are approved as AMOCs for the corre-
    sponding 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 Prod-
    ucts 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 Admin-
    istration (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.

Issued on March 18, 2024.  Victor Wicklund,  Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD by May 9, 2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-0759; Project Identifier AD-2023-01040-T]
RIN 2120-AA64

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

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.

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.

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 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

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Serial number inspection (retained action from AD 2023-13-11) 1 work-hour x $85 per hour = $85 None $85 $321,045
Reporting (retained action from AD 2023-13-11) 1 work-hour x $85 per hour = $85 $0 85 321,045

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

Action Labor cost Parts cost Cost per product
Detailed inspection 1 work-hour x $85 per hour = $85 $0 $85
Replacement 1 work-hour x $85 per hour = $85 (*) 85
Return of parts 1 work-hour x $85 per hour = $85 ** 50 135

* 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.

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

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]

2. The FAA amends Sec. 39.13 by:

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

b. Adding the following new AD: