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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2020-0859; Product Identifier 2020-NM-084-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by November 16, 2020.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD applies  to Bombardier,  Inc.,  Model  BD-100-1A10 airplanes,
    certificated  in  any  category, serial  numbers  20003  through 20500
    inclusive,  and  20501  through  20669  inclusive,  fitted  with  fire
    detection and  extinguishing (FIREX)  control unit  part number  (P/N)
    474112-2.

(d) SUBJECT

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

(e) REASON

    This AD was prompted by reports of failure of a certain FIREX  control
    unit. The FAA is issuing this AD to address failure of a FIREX control
    unit, which could result in the loss of the ability to detect a fire.

(f) COMPLIANCE

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

(g) REPLACEMENT

    Within 24 months  after the effective date  of  this  AD:  Replace any
    FIREX control unit having P/N 474112-2 with a unit having P/N 474112-3
    in  accordance  with paragraphs 2.B.(1) and (3)  of the Accomplishment
    Instructions of the applicable Bombardier, Inc, service bulletin spec-
    ified in paragraphs (g)(1) and (2) of this AD.

(1) For  airplanes  having  serial numbers 20003 through 20500  inclusive:
    Bombardier Service Bulletin 100-26-01, Revision 01,  dated December 5,
    2019.

(2) For  airplanes  having  serial numbers 20501 through 20669  inclusive:
    Bombardier Service Bulletin 350-26-001, Revision 01, dated December 5,
    2019.

(h) PARTS INSTALLATION PROHIBITION

    As of the effective date of this AD,  no  person  may install  a FIREX
    control unit having P/N 474112-2 on any airplane.

(i) CREDIT FOR PREVIOUS ACTIONS

    This paragraph provides credit  for the actions required  by paragraph
    (g) of this AD,  if those actions were performed  before the effective
    date  of  this  AD  using Bombardier Service Bulletin 100-26-01, dated
    December 20, 2016;  or  Bombardier Service Bulletin 350-26-001,  dated
    December 20, 2016, as applicable.

(j) OTHER FAA AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager,  New York ACO
    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
    local Flight  Standards District  Office, as  appropriate. If  sending
    information directly to the manager of the certification office,  send
    it to ATTN: Program  Manager, Continuing Operational Safety,  FAA, New
    York ACO Branch, 1600 Stewart  Avenue, Suite 410, Westbury, NY  11590;
    telephone 516-228-7300;  fax 516-794-5531.  Before using  any approved
    AMOC,  notify  your  appropriate  principal  inspector,  or  lacking a
    principal  inspector,  the  manager  of  the  local  flight  standards
    district office/certificate holding district 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,  New York  ACO
    Branch, FAA; or Transport Canada Civil Aviation (TCCA); or  Bombardier
    Inc.'s TCCA  Design Approval  Organization (DAO).  If approved  by the
    DAO, the approval must include the DAO-authorized signature.

(k) RELATED INFORMATION

(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) TCCA AD
    CF-2020-12, dated May 1, 2020, for related information.  This MCAI may
    be found in the AD docket on the internet  at https://www.regulations.
    gov by searching for and locating Docket No. FAA-2020-0859.

(2) For more information about this AD, contact Siddeeq Bacchus, Aerospace
    Engineer, Mechanical Systems and Administrative Services Section, FAA,
    New York ACO Branch,  1600  Stewart  Avenue,  Suite 410,  Westbury, NY
    11590; telephone 516-228-7362; fax 516-794-5531; email 9-avs-nyaco-cos
    @faa.gov.

(3) For service information identified  in  this  AD,  contact Bombardier,
    Inc., 200 Cote Vertu Road West,  Dorval, Quebec H4S 2A3, Canada; North
    America toll-free telephone 1 866 538 1247  or direct-dial telephone 1
    514 855 2999;  email ac.yul@aero.bombardier.com; internet https://www.
    bombardier.com. You may view this service information at the FAA, Air-
    worthiness 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.

Issued  on  September 24, 2020.  Gaetano A. Sciortino, Deputy Director for
Strategic Initiatives, Compliance & Airworthiness Division,  Aircraft Cer-
tification Service.

DATES: The FAA must receive comments  on this proposed AD  by November 16,
2020.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2020-0859; Product Identifier 2020-NM-084-AD]
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-100-1A10 airplanes. This
proposed AD was prompted by reports of failure of a certain fire
detection and extinguishing (FIREX) control unit. This proposed AD
would require replacing FIREX control units having a certain part
number. 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 November
16, 2020.

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 https://www.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.

For service information identified in this NPRM, contact
Bombardier, Inc., 200 Cote Vertu Road West, Dorval, Quebec
H4S 2A3, Canada; North America toll-free telephone 1-866-538-1247 or
direct-dial telephone 1-514-855-2999; email ac.yul@aero.bombardier.com;
internet https://www.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.

Examining the AD Docket

You may examine the AD docket on the internet at https://www.regulations.
gov by searching for and locating Docket No. FAA-2020-0859; 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. Comments will be available in the AD docket
shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Siddeeq Bacchus, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7362; fax 516-794-5531; email 9-avs-nyaco-cos@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to participate in this rulemaking by submitting
written comments, data, or views about this proposal. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. To
ensure the docket does not contain duplicate comments, commenters
should send only one copy of written comments, or if comments are filed
electronically, commenters should submit only one time. Send your
comments to an address listed under the ADDRESSES section. Include
"Docket No. FAA-2020-0859; Product Identifier 2020-NM-084-AD" at the
beginning of your 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, as well as a report summarizing each
substantive public contact with FAA personnel concerning this proposed
rulemaking. Before acting on this proposal, the FAA will consider all
comments received by the closing date for comments. The FAA will
consider comments filed after the comment period has closed if it is
possible to do so without incurring expense or delay. The FAA may
change this NPRM because of those comments.

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 the
person identified in the FOR FURTHER INFORMATION CONTACT section. Any
commentary that the FAA receives which is not specifically designated
as CBI will be placed in the public docket for this rulemaking.

Discussion

Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2020-12, dated April
17, 2020 (referred to after this as the Mandatory Continuing
Airworthiness Information, or "the MCAI"), to correct an unsafe
condition for certain Bombardier, Inc., Model BD-100-1A10 airplanes.
You may examine the MCAI in the AD docket on the internet at https://www.
regulations.gov by searching for and locating Docket No. FAA-2020-0859.

This proposed AD was prompted by reports of failure of a certain
FIREX control unit. The subsequent investigation determined that the
potential cause of these failures is the FIREX control unit's
susceptibility to internal electrical noise. The FAA is proposing this
AD to address the failure of a FIREX control unit, which could result
in the loss of the ability to detect a fire. See the MCAI for
additional background information.

Related Service Information Under 1 CFR Part 51

Bombardier, Inc., has issued Service Bulletin 100-26-01, Revision
01, dated December 5, 2019; and Service Bulletin 350-26-001, Revision
01, dated December 5, 2019. This service information describes
procedures for replacing FIREX control units having part number (P/N)
474112-2 with units having P/N 474112-3. These documents are distinct
since they apply to different airplane configurations. 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 our bilateral agreement with the State of Design Authority, the FAA
has been notified of the unsafe condition described in the MCAI and
service information referenced above. The FAA is proposing this AD
because the FAA evaluated all the relevant information and determined
the unsafe condition described previously is likely to exist or develop
on other products of the same type design.

Proposed Requirements of This NPRM

This proposed AD would require accomplishing the actions specified
in the service information described previously.

Costs of Compliance

The FAA estimates that this proposed AD affects 223 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
1 work-hour x $85 per hour = $85
$6,389
$6,474
$1,443,702

According to the manufacturer, some or all of the costs of this
proposed AD may be covered under warranty, thereby reducing the cost
impact on affected individuals. The FAA does not control warranty
coverage for affected individuals. As a result, the FAA has included
all known costs in our cost estimate.

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) 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 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 (AD):