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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2024-0767; Project Identifier MCAI-2023-00723-T.
(a) COMMENTS DUE DATE

    The FAA must  receive comments on this airworthiness directive (AD) by
    May 13, 2024.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD applies  to Bombardier,  Inc., Model  BD-700-2A12  airplanes,
    certificated  in  any  category, serial  numbers  70006  through 70099
    inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 26, Fire protection.

(e) UNSAFE CONDITION

    This AD was  prompted by reports  that the baggage  bay discharge push
    -button annunciator (PBA) switch was making contact but was not  fully
    engaged, and the tabs were not  fully locked. The FAA is issuing  this
    AD  to address  the possible  inability to  discharge halon  into  the
    baggage compartment in  case of a  fire. The unsafe  condition, if not
    addressed,  could  result  in  the  inability  to  control  a  baggage
    compartment fire.

(f) COMPLIANCE

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

(g) REQUIRED ACTIONS

    Within 36  months after  the effective  date of  this AD:  Perform the
    inspection and  testing of  the baggage  bay discharge  PBA switch, in
    accordance with the Accomplishment Instructions of Bombardier  Service
    Bulletin 700-26-7505, dated February 10, 2023.

(h) 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  of  the International
    Validation  Branch, mail  it to  the address  identified in  paragraph
    (i)(2)  of  this  AD. Information  may  be  emailed to:  9-AVS-AIR-730
    -AMOC@faa.gov. Before using any approved AMOC, notify your appropriate
    principal inspector, or lacking a principal inspector, the manager  of
    the responsible Flight Standards Office.

(2) CONTACTING THE MANUFACTURER: For any requirement in this AD to  obtain
    instructions   from   a  manufacturer,   the   instructions  must   be
    accomplished using  a method  approved by  the Manager,  International
    Validation Branch,  FAA; or  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.

(i) ADDITIONAL INFORMATION

(1) Refer to Transport Canada AD CF-2023-36, dated May 29, 2023 (Transport
    Canada AD CF-2023-36) for  related information. This Transport  Canada
    AD may be found in the  AD docket at regulations.gov under Docket  No.
    FAA-2024-0767.

(2) For more information about this AD, contact William Reisenauer, Aviat-
    ion Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY
    11590; phone: 516-228-7300; email: 9-avs-nyaco-cos@faa.gov.

(j) 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 700-26-7505, dated February 10, 2023.

(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
bombardier.com">ac.yul@aero.bombardier.com; website bombardier.com.

(4) 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.

(5) 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 21, 2024.  Victor Wicklund, Deputy Director, Compliance  &
Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD by May 13, 2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-0767; Project Identifier MCAI-2023-00723-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 BD-700-2A12 airplanes. This proposed AD
was prompted by reports that the baggage bay discharge push-button
annunciator (PBA) switch was making contact but was not fully engaged,
and the tabs were not fully locked. This proposed AD would require a
verification of the baggage bay discharge PBA functionality and tab
installation. 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 13, 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-2024-0767; 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 bombardier.com">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: William Reisenauer, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: 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-2024-0767; Project Identifier
MCAI-2023-00723-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
William Reisenauer, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone: 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-2023-36, dated May 29, 2023 (Transport
Canada AD CF-2023-36) (also referred to after this as the MCAI), to
correct an unsafe condition on certain Bombardier, Inc., Model BD-700-
2A12 airplanes. The MCAI states that during the execution of a
functional test procedure (FTP) during production, the baggage bay
discharge PBA switch was partially engaged and failed to make
electrical contact. Further investigation showed that in some
instances, the baggage bay discharge PBA switch was making contact but
was not fully engaged and the tabs were not fully locked, so while the
PBA may pass the FTP, vibration could eventually lead to a loss of
electrical contact and subsequent loss of baggage bay discharge PBA
switch functionality.

The FAA is issuing this AD to address the possible inability to
discharge halon into the baggage compartment in case of a fire. The
unsafe condition, if not addressed, could result in the inability to
control a baggage compartment fire.

You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-0767.

Related Service Information Under 1 CFR Part 51


The FAA reviewed Bombardier Service Bulletin 700-26-7505, dated
February 10, 2023. This service information specifies procedures for
doing a general visual inspection of the baggage bay discharge PBA
switch for proper installation and a functional operation test. 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.

Costs of Compliance


The FAA estimates that this AD, if adopted as proposed, would
affect 42 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
2 work-hours x $85 per hour = $170
$0
$170
$7,140

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: