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2024-14-05 BOMBARDIER, INC.: Amendment 39-22786; Docket No. FAA-2024-0767; Project Identifier MCAI-2023-00723-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective December 17, 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)
    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

    For  more  information  about  this  AD,  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.

(j) MATERIAL INCORPORATED BY REFERENCE

(1) The  Director of  the Federal  Register approved  the incorporation by
    reference  (IBR) of  the material  listed in  this  paragraph  under 5
    U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this material 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  Bombardier  material identified  in this  AD, 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.

(4) You may view this material 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  July 10,  2024. James  D. Foltz,  Deputy Director, Compliance &
Airworthiness Division, Aircraft Certification Service.

EDITORIAL NOTE: This document was  received for publication by the  Office
of the Federal Register on November 5, 2024.

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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2024-0767; Project Identifier MCAI-2023-00723-T;
Amendment 39-22786; AD 2024-14-05]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD-700-2A12 airplanes. 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. This AD requires a verification of
the baggage bay discharge PBA functionality and tab installation. The
FAA is issuing this AD to address the unsafe condition on these
products.

DATES: This AD is effective December 17, 2024.

The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 17, 2024.

ADDRESSES:

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 final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.

Material Incorporated by Reference:

For Bombardier material, contact Bombardier Business
Aircraft Customer Response Center, 400 C[ocirc]te-Vertu Road West,
Dorval, Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-2999; email
bombardier.com">ac.yul@aero.bombardier.com; website bombardier.com.

You may view this material 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. It is also available at regulations.gov under
Docket No. FAA-2024-0767.

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:

Background


The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Bombardier,
Inc., Model BD-700-2A12 airplanes. The NPRM published in the Federal
Register on March 28, 2024 (89 FR 21443). The NPRM was prompted by AD
CF-2023-36, dated May 29, 2023, issued by Transport Canada, which is
the aviation authority for Canada (referred to after this as the MCAI).
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.

In the NPRM, the FAA proposed to require a verification of the
baggage bay discharge PBA functionality and tab installation. 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 on
these products, 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.

Discussion of Final Airworthiness Directive

Comments


The FAA received no comments on the NPRM or on the determination of
the cost to the public.

Conclusion


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
referenced above. The FAA reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
Except for minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.

Related Material 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.

Costs of Compliance


The FAA estimates that this AD affects 42 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this 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 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


This AD will not have federalism implications under Executive Order
13132. This AD will 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 this AD:

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

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

(3) Will 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 Amendment


Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 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: