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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2023-1505; Project Identifier MCAI-2023-00246-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive  (AD) by
    September 8, 2023.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Bombardier, Inc., Model CL-600-2B16 (601-3A, 601-3R
    and 604 Variants) airplanes, certificated in any category, serial num-
    bers identified in Bombardier Service Bulletin 605-35-008, dated Octo-
    ber 28, 2022.

(d) SUBJECT

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

(e) UNSAFE CONDITION

    This AD  was prompted  by sleeve  loops on  some passenger oxygen mask
    lanyards that  had improper  crimping and  unsealed ends.  The FAA  is
    issuing this  AD to  address the  defective oxygen  mask lanyards. The
    unsafe condition, if not addressed, could result in no oxygen flow  to
    the mask during an emergency situation.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) INSPECTION OF THE PASSENGER OXYGEN MASK ASSEMBLIES

    Within 48 months from the effective date of this AD, visually  inspect
    the passenger oxygen mask lanyards in the cabin or lavatory oxygen box
    assemblies  as applicable  for crimped  lanyards and  sealed ends,  in
    accordance with paragraph 2.C.  of the Accomplishment Instructions  of
    Bombardier Service Bulletin 605-35-008, dated October 28, 2022.

(1) If all passenger oxygen mask lanyards are crimped and the lanyard ends
    are sealed: No further action is required by this paragraph.

(2) If any passenger oxygen mask lanyard is not crimped properly,  or  any
    lanyard end is not sealed properly: Before further flight, replace the
    passenger oxygen mask lanyard in  accordance with Section 2.D. of  the
    Accomplishment Instructions of Bombardier Service Bulletin 605-35-008,
    dated October 28, 2022.

(h) PARTS INSTALLATION PROHIBITION

    As of the  effective date of  this AD,  no person may install,  on any
    airplane, a passenger  oxygen mask lanyard  assembly provided with  an
    oxygen box lanyard kit containing a lot number in paragraph (h)(1)  or
    (2) of this AD.

(1) Oxygen box lanyard kit part number  (P/N) CDKC29-006-501,  lot  number
    2011007411, 2012010412, 2101018703, 2101035167, 2102030139, 2104003817
    or 2105005522.

(2) Oxygen box lanyard kit  P/N  CDKC29-006-503,  lot  number  2011029525,
    2012006900, 2103007412, or 2103029992.

(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 manager, International  Validation
    Branch, mail it to the address identified in paragraph (j)(2) of  this
    AD or  email to:  9-AVS-AIR-730-AMOC@faa.gov. If  mailing information,
    also  submit information  by email.  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 Transport  Canada or  Bombardier, Inc.'s
    Transport Canada  Design Approval  Organization (DAO).  If approved by
    the DAO, the approval must include the DAO-authorized signature.

(j) ADDITIONAL INFORMATION

(1) Refer to Transport Canada CF-2023-06,  dated February 9, 2023, for re-
    lated information.  This  Transport Canada AD  may be found  in the AD
    docket at regulations.gov under Docket No. FAA-2023-1505.

(2) For  more information  about this AD,  contact  Gabriel Kim,  Aviation
    Safety Engineer,  FAA,  1600 Stewart Avenue,  Suite 410,  Westbury, NY
    11590; telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov.

(k) 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.

(i) Bombardier Service Bulletin 605-35-008, dated October 28, 2022.

(ii) [Reserved]

(3) For service information identified in this AD, contact Bombardier Bus-
    iness Aircraft  Customer  Response  Center,  400 Cote-Vertu Road West,
    Dorval, Quebec H4S 1Y9, Canada;  telephone 514-855-2999; email ac.yul@
    aero.bombardier.com; website bombardier.com.

(4) 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.

(5) You may view  this service information  that is incorporated by refer-
    ence 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.

Issued on July 19, 2023.  Victor Wicklund,  Deputy Director,  Compliance &
Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by September 8,
2023.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1505; Project Identifier MCAI-2023-00246-T]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., 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 Bombardier, Inc., Model CL-600-2B16 (601-3A, 601-3R, and
604 Variants) airplanes. This proposed AD was prompted by sleeve loops
on some passenger oxygen mask lanyards that had improper crimping and
unsealed ends. This proposed AD would require an inspection of the
passenger oxygen mask lanyards and replacement of defective oxygen mask
lanyards. This proposed AD would also prohibit the installation of
affected 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 September
8, 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-2023-1505; 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, 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 service information identified in this NPRM, contact
Bombardier Business Aircraft Customer Response Center, 400 Cote-
Vertu Road West, Dorval, Quebec H4S 1Y9, Canada; telephone 514-
855-2999; email ac.yul@aero.bombardier.com; website bombardier.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-
228-7300; 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-2023-1505; Project Identifier
MCAI-2023-00246-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 NPRM.

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 516-228-7300; email 9-avs-nyaco-cos
@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

Transport Canada, which is the aviation authority for Canada, has
issued Transport Canada CF-2023-06, dated February 9, 2023 (Transport
Canada AD CF-2023-06) (also referred to after this as the MCAI), to
correct an unsafe condition on certain Bombardier, Inc., Model CL-600-
2B16 (601-3A, 601-3R, and 604 Variants) airplanes. The MCAI states the
sleeve loops on certain passenger oxygen mask lanyards were found to
have improper crimping and unsealed ends.
This proposed AD addresses these defective oxygen mask lanyards,
which could result in no oxygen flow to the mask during an emergency
situation.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1505.

Related Rulemaking

The FAA issued AD 2017-16-13, Amendment 39-18990 (82 FR 39518,
August 21, 2017) (AD 2017-16-13), for certain Bombardier, Inc., Model
CL-600-2B16 (601-3A, 601-3R, and 604 Variants) airplanes. AD 2017-16-13
resulted from a report indicating that the lanyard length of the
passenger drop-down oxygen masks is too long. AD 2017-16-13 requires replacing
the existing oxygen mask lanyards with lanyards of the correct length.
The FAA issued AD 2017-16-13 to prevent improper oxygen flow
functionality to the passenger oxygen masks in the event of an
emergency.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Bombardier Service Bulletin 605-35-008, dated
October 28, 2022. This service information specifies procedures for
visual inspection of the existing passenger oxygen mask lanyards
installed in the cabin or lavatory oxygen box assemblies, and
replacement of the defective oxygen mask lanyards. The defective oxygen
mask lanyards had improperly crimped sleeve loops and unsealed ends.
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.

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
and service information referenced above. 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.

Proposed AD Requirements in This NPRM

This proposed AD would require accomplishing the actions specified
in the service information already described. This proposed AD would
also prohibit the installation of affected parts.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 120 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:

Estimated Costs for Required Actions

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Inspection 1 work-hour x $85 per hour = $85
$0
$85
$10,200

The FAA estimates the following costs to do any necessary on-
condition action 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 this on-condition action:

Estimated Costs of On-Condition Actions

Action
Labor cost
Parts cost
Cost per product
Replacement 2 work-hours x $85 per hour = $170
$1,149
$1,319

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.

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) 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 adding the following new airworthiness
directive: