preamble attached >>>
ADs updated daily at www.Tdata.com
PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2023-1710; Project Identifier MCAI-2023-00243-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    September 28, 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
    numbers 5580 through 5665 inclusive, 5701 through 5988 inclusive,  and
    6050 and subsequent.

(d) SUBJECT

    Air Transport Association (ATA) of America Code: 36, Pneumatic.

(e) UNSAFE CONDITION

    This AD was prompted by reports that sensing elements of the bleed air
    leak detection system were  manufactured with insufficient salt  fill.
    The FAA is  issuing this AD  to address insufficient  salt fill, which
    can result in an  inability to detect hot  bleed air leaks, which  can
    cause damage to  surrounding structures and  systems that can  prevent
    continued safe flight and landing.

(f) COMPLIANCE

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

(g) DEFINITIONS

    For the purposes of this  AD, the definitions specified in  paragraphs
    (g)(1) and (2) of this AD apply.

(1) Affected part:  A sensing element marked with a date code before A2105
    and having a part number listed in Kidde Aerospace and Defense Service
    Bulletin CFD-26-1,  Revision 6,  dated  February 28, 2022;  unless the
    sensing element meets the conditions specified in paragraphs (g)(1)(i)
    and (ii) of this AD, or has passed the test specified in paragraph (h)
    of this AD.

(i) Has been tested  in accordance with the Accomplishment Instructions of
    the Kidde Aerospace and Defense Service Bulletin CFD-26-1, Revision 6,
    dated February 28, 2022, and passed the test; and

(ii) Has been marked  on one face of its connector hex nut  in  accordance
     with paragraph 3.C., Identification Procedure, of the Kidde Aerospace
     and Defense Service Bulletin CFD-26-1, Revision 6, dated February 28,
     2022.

(2) Serviceable part: A sensing element that is not an affected part.

(h) TESTING

    For airplane serial numbers 5580 through 5665 inclusive, 5701  through
    5988 inclusive, and 6050  through 6174 inclusive: Within  7,800 flight
    cycles or 96 months, whichever  occurs first, from the effective  date
    of this AD, test the bleed air leak detection system sensing  elements
    to  determine  if  they  are  serviceable,  in  accordance  with   the
    Accomplishment  Instructions  of  the  applicable  service information
    identified in paragraphs (h)(1) through (3) of this AD. If the sensing
    element is found serviceable, before further flight, mark the  sensing
    element  with  a  green mark  in  accordance  with the  Accomplishment
    Instructions  of  the  applicable  service  information  identified in
    paragraphs (h)(1) through  (3) of this  AD. If the  sensing element is
    found  not serviceable,  before further  flight,  replace  the sensing
    element with a serviceable part in accordance with the  Accomplishment
    Instructions  of  the  applicable  service  information  identified in
    paragraphs (h)(1) through (3) of this AD.

(1) For Model CL-600-2B16 airplanes,  serial numbers 5580 through 5665 in-
    clusive (Challenger 604):  Use Bombardier Service Bulletin 604-36-005,
    dated December 23, 2022.

(2) For Model CL-600-2B16 airplanes,  serial numbers 5701 through 5988 in-
    clusive (Challenger 605):  Use Bombardier Service Bulletin 605-36-002,
    dated December 23, 2022.

(3) For Model CL-600-2B16 airplanes,  serial numbers 6050 through 6174 in-
    clusive (Challenger 650):  Use Bombardier Service Bulletin 650-36-001,
    dated December 23, 2022.

(i) PARTS INSTALLATION PROHIBITION

    As of the effective date of this AD, no person may install an affected
    part on any airplane.

(j) NO REPORTING REQUIREMENT

    Although the  service information  referenced in  paragraph (g)(1)  of
    this AD and paragraphs (h)(1) through (3) of this AD specify to submit
    certain information to the manufacturer, this AD does not include that
    requirement.

(k) 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 (l)(2) of  this
    AD or email 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  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.

(3) Required for Compliance (RC):  Except as required  by paragraph (k)(2)
    of this AD,  if any service  information contains procedures  or tests
    that are identified as RC, those procedures and tests must be done  to
    comply with this AD; any  procedures or tests that are  not identified
    as  RC  are  recommended.  Those procedures  and  tests  that  are not
    identified  as  RC may  be  deviated from  using  accepted methods  in
    accordance  with  the  operator's  maintenance  or  inspection program
    without obtaining  approval of  an AMOC,  provided the  procedures and
    tests identified as RC can be done and the airplane can be put back in
    an airworthy condition. Any substitutions or changes to procedures  or
    tests identified as RC require approval of an AMOC.

(l) ADDITIONAL INFORMATION

(1) Refer to Transport Canada AD CF-2023-05,  dated February 8, 2023,  for
    related information.  This Transport Canada AD  may be found in the AD
    docket at regulations.gov under Docket No. FAA-2023-1710.

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

(m) 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 604-36-005, dated December 23, 2022.

(ii) Bombardier Service Bulletin 605-36-002, dated December 23, 2022.

(iii) Bombardier Service Bulletin 650-36-001, dated December 23, 2022.

(iv) Kidde Aerospace and Defense  Service Bulletin  CFD-26-1,  Revision 6,
     dated February 28, 2022.

Note 1 to paragraph (m)(2)(iv):  The revision level of this service bulle-
tin is only identified on the transmittal sheet.

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

(4) For  Kidde Aerospace & Defense service information  identified in this
    AD, contact Kidde Aerospace & Defense, 4200 Airport Drive NW, Building
    B, Wilson, NC 27896; telephone 319-295-5000; website kiddetechnologies
    .com/aviation.com.

(5) 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.

(6) 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 August 3, 2023.  Victor Wicklund,  Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD  by September 28,
2023.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1710; Project Identifier MCAI-2023-00243-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 reports from
the supplier that sensing elements of the bleed air leak detection
system were manufactured with insufficient salt fill, which can result
in an inability to detect hot bleed air leaks. This proposed AD would
require testing of all affected overheat detection sensing elements of
the bleed air leak detection system, and replacement if necessary. 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
28, 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-2023-1710; 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 Bombardier 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.
For Kidde Aerospace & Defense service information
identified in this NPRM, contact Kidde Aerospace & Defense, 4200
Airport Drive NW, Building B, Wilson, NC 27896; telephone: 319-295-
5000; website: kiddetechnologies.com/aviation.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: Chirayu Gupta, 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-2023-1710; Project Identifier
MCAI-2023-00243-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
Chirayu Gupta, 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 AD CF-2023-05, dated February 8, 2023
(Transport Canada AD CF-2023-05) (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 that Bombardier received reports from the supplier of the
overheat detection sensing elements of a manufacturing quality escape.
Some of the sensing elements of the bleed air leak detection system
were manufactured with insufficient salt fill, which can result in an
inability to detect hot bleed air leaks and cause damage to surrounding
structures and systems that can prevent continued safe flight and
landing.
The FAA is proposing this AD to address the unsafe condition on
these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1710.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Bombardier Service Bulletin 604-36-005, Bombardier
Service Bulletin 605-36-002, and Bombardier Service Bulletin 650-36-
001, all dated December 23, 2022. This service information specifies
procedures for testing affected bleed air leak detection system sensing
elements (i.e., those marked with a date code before ``A2105'' (which
corresponds to January 31, 2021) with a part number defined in this
service information) to determine if they are serviceable, and
replacing failed sensing elements with serviceable ones. These
documents are distinct since they apply to different airplane serial
numbers.
The FAA reviewed Kidde Aerospace & Defense Service Bulletin CFD-26-
1, Revision 6, dated February 28, 2022. This service information
specifies affected continuous fire detector part numbers and testing
procedures.
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 694 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:

Estimated Costs for Required Actions

Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Up to 37 work-hours x $85 per hour = Up to $3,145
$0
Up to $3,145 Up to $2,182,630

The estimates the following costs to do any necessary on-condition
actions 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 cost
Parts cost
Cost per product
37 work-hours x $85 per hour = $3,145
* $4,000
$7,145

* The FAA has received no definitive data on which to base the cost
estimates for the parts specified in this proposed AD. This is the
estimated cost for replacement of 2 percent of the failed sensing
elements. If all sensing elements failed, the estimated parts cost
would be $40,000 for each airplane.

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: