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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2019-0702; Product Identifier 2019-NM-118-AD.
(a) COMMENTS DUE DATE

    The FAA must receive comments by November 18, 2019.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD  applies to Bombardier, Inc.,  Model DHC-8-400, -401, and -402
    airplanes, certificated in any category,  serial numbers 4001 and 4003
    and subsequent.

(d) SUBJECT

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

(e) REASON

    This  AD  was  prompted  by  a  report  of  a  quality  escape  in the
    manufacturing of advanced pneumatic  detector (APD) switches, and  the
    presence  of  contamination on  the  switch contact  pin.  The FAA  is
    issuing this AD to address such contamination that could insulate  the
    contact  pin  from the  diaphragm  and result  in  undetected or  late
    detection of a fire.

(f) COMPLIANCE

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

(g) AFFECTED APDS

    For purposes  of this  AD, an  affected APD  is manufactured  by Kidde
    (UTAS)  and  has  a  part  number  and  serial  number  identified  in
    paragraphs (g)(1) through (10) of this AD.

(1) Part number 10-1096 (all serial numbers).

(2) Part number 10-1096-01 (all serial numbers).

(3) Part number 10-1096-02 (serial numbers before AEM9907).

(4) Part number 10-1097 (all serial numbers).

(5) Part number 10-1097-01 (all serial numbers).

(6) Part number 10-1097-02 (serial numbers before 17-0005).

(7) Part number 10-1098 (all serial numbers).

(8) Part number 10-1098-01 (serial numbers before 17-0110).

(9) Part number 10-1099 (all serial numbers).

(10) Part number 10-1099-01 (serial numbers before 17-0009).

(h) APD IDENTIFICATION AND TEST

    Within 8,000 flight hours  or 48 months,  whichever occurs first after
    the effective date of this AD:  Do the applicable actions specified in
    paragraph  (h)(1)  and  (2)  of  this  AD,   in  accordance  with  the
    Accomplishment Instructions  of  Bombardier Service Bulletin 84-26-19,
    Revision `A,' dated February 11, 2019.

(1) Determine whether any affected APD is installed on the engine nacelles
    or auxiliary power unit (APU) compartment.

(2) Do the on-aircraft test of all affected APDs.

(i) For any APD that passes the test:  Before  further  flight, reidentify
    the APD.

(ii) For any APD that fails the test,  before further flight,  replace the
     APD with an unaffected APD,  or  one provided  by Kidde that has been
     successfully tested and reidentified.

(i) RETURN OF FAILED APDS

    For any APD that fails the test specified  in paragraph (h)(2) of this
    AD:  Return the APD at the applicable time specified  in paragraph (i)
    (1) or (2) of this AD  to  Kidde Aerospace & Defense,  4200 Airport Dr
    NW, Building B,  Wilson, NC 27896-8630,  Attention Keith Fail,  Super-
    visor, Service Center.

(1) If the test was done on  or after the effective date of this AD:  Send
    the APD within 30 days after completion of the test.

(2) If the test was done  before the effective date of this AD:  Send  the
    APD within 30 days after the effective date of this AD.

(j) PARTS INSTALLATION LIMITATION

    As of the effective date of this AD, no person may install an affected
    APD,  unless the APD has been successfully tested  and reidentified in
    accordance  with  Bombardier Service Bulletin 84-26-19,  Revision `A,'
    dated February 11, 2019.

(k) CREDIT FOR PREVIOUS ACTIONS

    This paragraph provides credit  for actions required  by paragraph (h)
    of this AD,  if those actions were performed before the effective date
    of this AD using Bombardier Service Bulletin 84-26-19,  dated  October
    24, 2018.

(l) 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
    corrective  actions   from  a   manufacturer,  the   action  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.

(3) Reporting  Requirements:  A federal agency may not conduct or sponsor,
    and a  person is  not required  to respond  to, nor  shall a person be
    subject  to a  penalty  for  failure to  comply with  a collection  of
    information subject to the requirements of the Paperwork Reduction Act
    unless that  collection of  information displays  a current  valid OMB
    Control Number. The OMB Control Number for this information collection
    is 2120-0056. Public reporting  for this collection of  information is
    estimated to be approximately 1 hour per response, including the  time
    for reviewing instructions, completing and reviewing the collection of
    information.  All  responses  to this  collection  of  information are
    mandatory.  Comments  concerning  the  accuracy  of  this  burden  and
    suggestions for reducing the burden should be directed to the FAA  at:
    800 Independence Ave.  SW,  Washington,  DC 20591,  Attn:  Information
    Collection Clearance Officer, AES-200.

(m) RELATED INFORMATION

(1) Refer   to   Mandatory  Continuing  Airworthiness  Information  (MCAI)
    Canadian AD CF-2019-13, dated April 4, 2019,  for related information.
    This MCAI may be found in the AD docket on the internet at http://www.
    regulations.gov by searching for and locating Docket No. FAA-2019-0702

(2) For more information about this AD,  contact Thomas Niczky,  Aerospace
    Engineer,  Avionics and Electrical Systems Services Section,  FAA, New
    York ACO Branch,  1600 Stewart Avenue, Suite 410,  Westbury, NY 11590;
    telephone 516-228-7347;  fax 516-794-5531;  email 9-avs-nyaco-cos@faa.
    gov.

(3) For service information identified  in this AD,  contact  De Havilland
    Aircraft of Canada Ltd.,  Q-Series  Technical  Help Desk,  123 Garratt
    Boulevard, Toronto,  Ontario M3K 1Y5, Canada;  telephone 416-375-4000;
    fax  416-375-4539;   email  thd@dehavilland.com;   internet:  https://
    dehavilland.com.  You may view this service information  at  the  FAA,
    Transport Standards Branch,  2200 South 216th St., Des Moines, WA. For
    information on the availability of this material at the FAA, call 206-
    231-3195.

Issued in Des Moines, Washington, on September 24, 2019. Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification Service

DATES: The FAA must receive comments on this proposed AD  by  November 18,
2019.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0702; Product Identifier 2019-NM-118-AD]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier, Inc., Model DHC-8-400 series airplanes. This
proposed AD was prompted by a report of a quality escape in the
manufacturing of the advanced pneumatic detector (APD) switches, and
the presence of contamination on the switch contact pin. This proposed
AD would require identification and testing, and reidentification or
replacement if necessary, of affected APDs. 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
18, 2019.

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 http://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 De
Havilland Aircraft of Canada Ltd., Q-Series Technical Help Desk, 123
Garratt Boulevard, Toronto, Ontario M3K 1Y5, Canada; telephone 416-375-
4000; fax 416-375-4539; email thd@dehavilland.com; internet: https://
dehavilland.com. You may view this service information at the FAA,
Transport Standards 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 http://www.regulations.
gov by searching for and locating Docket No. FAA-2019-0702;
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 regulatory evaluation, 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: Thomas Niczky, Aerospace Engineer,
Avionics and Electrical Systems Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7347; fax 516-794-5531; 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 the ADDRESSES section. Include "Docket No. FAA-2019-0702;
Product Identifier 2019-NM-118-AD" at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this NPRM. The FAA will
consider all comments received by the closing date and may amend this
NPRM because of those comments.

The FAA will post all comments, without change, to http://www.regulations.
gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact the agency receives about this NPRM.

Discussion

Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2019-13, dated April 4,
2019 (referred to after this as the Mandatory Continuing Airworthiness
Information, or "the MCAI"), to correct an unsafe condition for
certain Bombardier, Inc., Model DHC-8-400, -401, and -402 airplanes.
You may examine the MCAI in the AD docket on the internet at http://www.
regulations.gov by searching for and locating Docket No. FAA-2019-0702.

This proposed AD was prompted by a report of a quality escape in
the manufacturing of advanced pneumatic detector (APD) switches, and
the presence of contamination on the switch contact pin. The FAA is
proposing this AD to address such contamination that could insulate the
contact pin from the diaphragm and result in undetected or late
detection of a fire. See the MCAI for additional background
information.

Related Service Information Under 1 CFR Part 51

Bombardier has issued Service Bulletin 84-26-19, Revision `A,'
dated February 11, 2019. This service information describes procedures
for identification and testing, and reidentification or replacement if
necessary, of affected APDs.

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 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. This proposed AD would
also require returning failed APDs to the manufacturer.

Costs of Compliance

The FAA estimates that this proposed AD affects 65 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 10 work-hours x $85 per hour = Up to $850 $0 Up to $850 Up to $55,250

The FAA 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 this on-condition actions:

Estimated Costs of On-Condition Actions *

Labor cost Parts cost Cost per product
Up to 124 work-hours x $85 per hour = Up to $10,540 Up to $51,076 Up to $61,616

* The FAA has received no definitive data to provide cost estimates for
the on-condition return of parts.

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 the cost estimate.

Paperwork Reduction Act

A federal agency may not conduct or sponsor, and a person is not
required to respond to, nor shall a person be subject to penalty for
failure to comply with a collection of information subject to the
requirements of the Paperwork Reduction Act unless that collection of in-
formation displays a current valid OMB control number. The control number
for the collection of information required by this NPRM is 2120-0056.
The paperwork cost associated with this NPRM has been detailed in the
Costs of Compliance section of this document and includes time for review-
ing instructions, as well as completing and reviewing the collection of
information.

Therefore, all reporting associated with this NPRM is mandatory.
Comments concerning the accuracy of this burden and suggestions for
reducing the burden should be directed to the FAA at 800 Independence
Ave. SW, Washington, DC 20591, ATTN: Information Collection Clearance
Officer, AES-200.

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.

This proposed AD is issued in accordance with authority delegated
by the Executive Director, Aircraft Certification Service, as
authorized by FAA Order 8000.51C. In accordance with that order,
issuance of ADs is normally a function of the Compliance and
Airworthiness Division, but during this transition period, the
Executive Director has delegated the authority to issue ADs applicable
to transport category airplanes and associated appliances to the
Director of the System Oversight Division.

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):