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2020-03-17 BOMBARDIER, INC.: Amendment 39-19841; Docket No. FAA-2019-0526; Product Identifier 2019-NM-023-AD.
(a) EFFECTIVE DATE

    This AD is effective April 2, 2020.

(b) AFFECTED ADS

    This  AD  replaces  AD  2015-24-04,  Amendment 39-18336  (80 FR 74673,
    November 30, 2015) ("AD 2015-24-04").

(c) APPLICABILITY

    This AD applies to the Bombardier, Inc, airplanes, certificated in any
    category, identified in paragraphs (c)(1) through (4) of this AD, with
    a Class C cargo compartment configuration.

(1) Model  CL-600-2B19  (Regional Jet Series 100 & 440) airplanes,  serial
    numbers 7003 and subsequent.

(2) Model  CL-600-2C10  (Regional  Jet  Series 700, 701, & 702) airplanes,
    serial numbers 10002 and subsequent.

(3) Model  CL-600-2D15  (Regional  Jet  Series  705)  airplanes  and Model
    CL-600-2D24 (Regional Jet Series 900) airplanes,  serial numbers 15001
    and subsequent.

(4) Model CL-600-2E25 (Regional Jet Series 1000) airplanes, serial numbers
    19001 and subsequent.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 25, Equipment/Furnish-
    ings.

(e) REASON

    This AD was prompted by reports of damaged decompression window louver
    panel assemblies (WLPAs), and detached blowout panels (BOPs).  The FAA
    is issuing this AD  to address damaged or  detached WLPAs and BOPs.  A
    detached  WLPA  or  BOP  could  delay  smoke  detection  in  the cargo
    compartment  in  the  event  of  a  fire,  and  could  result  in   an
    uncontrolled fire in the cargo compartment.

(f) COMPLIANCE

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

(g) INSPECTIONS, CORRECTIVE ACTION AND TERMINATING ACTION FOR MODEL CL-600
    -2B19 AIRPLANES

(1) At the applicable time specified  in  paragraph  (g)(1)(i)  or (ii) of
    this AD: Do detailed inspections for damaged or detached WLPAs, and do
    all applicable corrective actions before further flight, in accordance
    with the  Accomplishment Instructions  of Bombardier  Service Bulletin
    601R-25-201, Revision C, dated May 11, 2017.

(i) For airplanes with the accumulation of 780 total flight hours  or more
    as of December 15, 2015 (the effective date of AD 2015-24-04): Inspect
    within 100 flight hours after December 15, 2015.

(ii) For airplanes  that have accumulated less than 780 total flight hours
     as of December 15, 2015 (the effective date of AD 2015-24-04) Inspect
     before accumulating 880 total flight hours after December 15, 2015.

(2) Within 30 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the information specified in Task C26-25-115-01, "Detailed  Inspection
    of  the  Window  Louver  Panel  Assembly  (WLPA)  in  Aft  Cabin/Cargo
    Compartment Bulkhead,"  provided in  Bombardier CL-600-2B19  Temporary
    Revision (TR) 2A-69, dated August 30, 2018 (which is a TR to  Appendix
    A -  Certification Maintenance  Requirements (CMR),  of Part  2 of the
    Bombardier  CL-600-2B19  Maintenance  Requirements  Manual  (MRM), CSP
    -A053).  The initial  compliance time  for accomplishing  the task  is
    within  880  flight  hours  from  the  last  inspection  performed  as
    specified  in  Bombardier Service  Bulletin  601R-25-201, Revision  C,
    dated  May  11,  2017.  Accomplishing  the  actions  required  by this
    paragraph terminates the inspection requirement in paragraph (g)(1) of
    this AD.

(h) INSPECTIONS, CORRECTIVE ACTION AND TERMINATING ACTION FOR MODEL CL-600
    -2C10, CL-600-2D15, CL-600-2D24, AND CL-600-2E25 AIRPLANES

(1) At the applicable time specified  in  paragraph (h)(1)(i)  or  (ii) of
    this AD:  Do detailed  inspections for  damaged or  detached WLPAs and
    BOPs, and do all applicable corrective actions before further  flight,
    in  accordance  with  the  Accomplishment  Instructions  of Bombardier
    Service Bulletin 670BA-25-100, Revision C, dated May 11, 2017.

(i) For airplanes with the accumulation of 780 total flight hours  or more
    as of December 15, 2015 (the effective date of AD 2015-24-04): Inspect
    within 100 flight hours after December 15, 2015.

(ii) For airplanes  that have accumulated less than 780 total flight hours
     as of December 15, 2015 (the effective date of AD 2015-24-04) Inspect
     before accumulating 880 total flight hours after December 15, 2015.

(2) Within 30 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the information specified in Task 255000-208, "Detailed Inspection  of
    the Aft  Cargo Compartment  Window-Louver Panel  Assembly and  Blowout
    Panels Along with Their  Respective Cage Assemblies," as  specified in
    CRJ Series Regional Jet (Bombardier)  TR MRB-0079, dated May 29,  2017
    (which is a  TR to Part  1 of the  Bombardier CRJ Series  Regional Jet
    MRM, CSP  B-053). The  initial compliance  time for  accomplishing the
    task is within 880 flight hours from the last inspection performed  in
    accordance with Bombardier Service Bulletin 670BA-25-100, Revision  C,
    dated  May  11,  2017.  Accomplishing  the  actions  required  by this
    paragraph terminates the inspection requirement in paragraph (h)(1) of
    this AD.

(i) CREDIT FOR PREVIOUS ACTIONS

(1) This paragraph provides credit  for actions required  by paragraph (g)
    (1) of this AD,  if those actions were performed  before the effective
    date of this AD using the service information identified in paragraphs
    (i)(1)(i) through (iii) of this AD.

(i) Bombardier Service Bulletin 601R-25-201 dated July 21, 2015, which was
    incorporated by reference in AD 2015-24-04,  Amendment 39-18336 (80 FR
    74673, November 30, 2015).

(ii) Bombardier Service Bulletin 601R-25-201 Revision A, dated October 21,
     2015, which is not incorporated by reference in this AD.

(iii) Bombardier Service Bulletin 601R-25-201,  Revision B, dated February
      2, 2016, which is not incorporated by reference in this AD.

(2) This paragraph provides credit  for actions required  by paragraph (h)
    (1) of this AD,  if those actions were performed  before the effective
    date of this AD using the service information identified in paragraphs
    (i)(2)(i) through (iii) of this AD.

(i) Bombardier Service Bulletin 670BA-25-100,  dated July 21, 2015,  which
    was incorporated by reference in AD 2015-24-04, Amendment 39-18336 (80
    FR 74673, November 30, 2015).

(ii) Bombardier Service Bulletin 670BA-25-100,  Revision A,  dated October
     21, 2015, which is not incorporated by reference in this AD.

(iii) Bombardier Service Bulletin 670BA-25-100, Revision B, dated February
      2, 2016, which is not incorporated by reference in this AD.

(j) OTHER FAA AD PROVISIONS

(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.

(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.

(k) RELATED INFORMATION

(1) Refer   to   Mandatory  Continuing  Airworthiness  Information  (MCAI)
    Canadian  AD  CF-2015-28R2,  dated  February  4,  2019;  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-2019-0526.

(2) For more information about this AD, contact Darren Gassetto, Aerospace
    Engineer, Mechanical Systems and Administrative Services Section, FAA,
    New York  ACO Branch,  1600 Stewart Avenue,  Suite 410,  Westbury,  NY
    11590; telephone 516-228-7323; fax 516-794-5531; email 9-avs-nyaco-cos
    @faa.gov.

(3) Service information  identified in this AD that is not incorporated by
    reference is available at the addresses specified in paragraphs (l)(3)
    and (4) of this AD.

(l) 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 601R-25-201,  Revision C,  dated  May 11,
    2017.

(ii) Bombardier Service Bulletin 670BA-25-100,  Revision C,  dated May 11,
     2017.

(iii) Bombardier CL-600-2B19  Temporary Revision 2A-69,  dated  August 30,
      2018.

(iv) CRJ Series Regional Jet  (Bombardier)  Temporary  Revision  MRB-0079,
     dated May 29, 2017.

(3) For service information  identified  in this AD,  contact  Bombardier,
    Inc.,  400 Côte-Vertu Road West, Dorval, Québec H4S 1Y9, Canada; Wide-
    body Customer Response Center North America toll-free telephone 1-866-
    538-1247  or  direct-dial  telephone 1-514-855-2999; fax 514-855-7401;
    email ac.yul@aero.bombardier.com; Internet http://www.bombardier.com.

(4) 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.

(5) You  may  view  this  service  information  that  is  incorporated  by
    reference at the National Archives and Records Administration  (NARA).
    For information on the availability  of this material  at NARA,  email
    fedreg.legal@nara.gov,  or  go  to:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued on February 12, 2020.  Lance T. Gant,  Director,  Compliance & Air-
worthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Darren  Gassetto,   Aerospace  Engineer,
Mechanical Systems and Administrative Services Section,  FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 516-
228-7323; fax 516-794-5531; email 9-avs-nyaco-cos@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0526; Product Identifier 2019-NM-023-AD; Amendment
39-19841; AD 2020-03-17]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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

SUMMARY: The FAA superseding Airworthiness Directive (AD) 2015-24-04,
which applied to certain Bombardier, Inc., Model CL-600-2B19 (Regional
Jet Series 100 & 440) airplanes, Model CL-600-2C10 (Regional Jet Series
700, 701, & 702) airplanes, Model CL-600-2D15 (Regional Jet Series 705)
airplanes, Model CL-600-2D24 (Regional Jet Series 900) airplanes, and
Model CL-600-2E25 (Regional Jet Series 1000) airplanes. AD 2015-24-04
required repetitive inspections of the cage assembly for damaged or
detached window louver panel assemblies (WLPAs) and blowout panels
(BOPs), and corrective actions if necessary. This AD requires one-time
inspections of the WLPAs and BOPs, corrective actions if necessary, and
a revision of the existing maintenance or inspection program, as
applicable, to incorporate new airworthiness limitations, which would
terminate the inspection requirement. This AD was prompted by a
determination that new airworthiness limitations, as well as additional
actions, are necessary to address the unsafe condition. The FAA is
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective April 2, 2020.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of April 2,
2020.

ADDRESSES: For service information identified in this final rule,
contact Bombardier, Inc., 400 Cote-Vertu Road West, Dorval,
Quebec H4S 1Y9, Canada; Widebody Customer Response Center North
America toll-free telephone 1-866-538-1247 or direct-dial telephone 1-
514-855-2999; fax 514-855-7401; email ac.yul@aero.bombardier.com;
internet http://www.bombardier.com. You may view this referenced
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. It is also available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2019-0526.

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-2019-
0526; 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 regulatory evaluation, 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.

FOR FURTHER INFORMATION CONTACT: Darren Gassetto, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7323; fax 516-794-5531; email 9-avs-nyaco-cos@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2015-28R2, dated
February 4, 2019 (referred to as the Mandatory Continuing Airworthiness
Information, or ``the MCAI''), to correct an unsafe condition for
certain Bombardier, Inc., Model CL-600-2B19 (Regional Jet Series 100 &
440) airplanes, Model CL-600-2C10 (Regional Jet Series 700, 701, & 702)
airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model
CL-600-2D24 (Regional Jet Series 900) airplanes, and Model CL-600-2E25
(Regional Jet Series 1000) 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-2019-0526.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2015-24-04, Amendment 39-18336 (80 FR
74673, November 30, 2015) (``AD 2015-24-04''). AD 2015-24-04 applied to
certain Bombardier, Inc., Model CL-600-2B19 (Regional Jet Series 100 &
440) airplanes, Model CL-600-2C10 (Regional Jet Series 700, 701, & 702)
airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes, Model
CL-600-2D24 (Regional Jet Series 900) airplanes, and Model CL-600-2E25
(Regional Jet Series 1000) airplanes. The NPRM published in the Federal
Register on September 20, 2019 (84 FR 49484). The NPRM was prompted by
a determination that new airworthiness limitations, as well as
additional actions, are necessary to address the unsafe condition. The
NPRM proposed to require one-time inspections of the WLPAs and BOPs,
corrective actions if necessary, and a revision of the existing
maintenance or inspection program, as applicable, to incorporate new
airworthiness limitations, which would terminate the inspection
requirement. The FAA is issuing this AD to address damaged or detached
WLPAs and BOPs, which could delay smoke detection in the cargo
compartment in the event of a fire and result in an uncontrolled fire
in the cargo compartment. See the MCAI for additional background
information.

Action Since the NPRM Was Issued

Since the NPRM was issued, the FAA has determined that the
applicability identified in paragraph (c) of this AD needs to be
revised to better identify the affected airplanes. Therefore, the FAA
has revised paragraph (c) of this AD to add that affected airplanes
have a Class C cargo compartment configuration, which matches the
applicability in the MCAI. This revision does not change the number of
affected airplanes of U.S. registry.

Comments

The FAA gave the public the opportunity to participate in
developing this final rule. The following presents the comments
received on the NPRM and the FAA's response to the comments.

Support for the NPRM

The Air Line Pilots Association, International indicated its
support for the NPRM.

Request for Clarification of Global Alternative Method of Compliance
(AMOC)


Air Wisconsin Airlines requested clarification that the content and
intent of Global AMOC 2015-24-04, Log #19-02, dated February 13, 2019,
is acceptable for the repetitive inspections specified in the proposed
AD. Air Wisconsin stated that the section of the global AMOC which
states, in part, ``Operators shall perform the initial inspection and
phase-in schedule per SB 601R-25-201 and SB 670BA-25-100, as mandated
by AD and continue with the instructions as per published airplane
maintenance manual (AMM) tasks . . .'' which are ``. . . AMM Task 25-
50-00-220-801 and AMM Task 25-50-00-220-803, in lieu of the
accomplishment instructions specified in SB 601R-25-201 and SB 670BA-
25-100.'' Air Wisconsin concluded that paragraph (j) of the proposed AD
does not indicate any previously approved AMOCs are acceptable, or
specify the method of compliance for repetitive inspections, although
implied through the required implementation of Certification
Maintenance Requirements (CMR) Task C26-25-115-01 and Maintenance
Review Manual (MRM) Task 255000-208.
The FAA acknowledges the commenter's concern and provides the
following clarification. Global AMOC 2015-24-04, Log #19-02, dated
February 13, 2019, was issued specifically for the actions required by
AD 2015-24-04, which is superseded by this final rule. This AD already
incorporates CMR Task C26-25-115-01, as specified in Bombardier CL-600-
2B19 Temporary Revision (TR) 2A-69, dated August 30, 2018 (required by
paragraph (g)(2) of this AD), and MRM Task 255000-208, as specified in
CRJ Series Regional Jet (Bombardier) TR MRB-0079, dated May 29, 2017
(required by paragraph (h)(2) of this AD). Accomplishing the actions
required by paragraphs (g)(2) and (h)(2) of this AD terminates the
repetitive inspections specified in paragraphs (g)(1) and (h)(1) of
this AD, which require the inspections be done in accordance with
Bombardier Service Bulletins 601R-25-201 and 670BA-25-100, both
Revision C, both dated May 11, 2017. Therefore, this AD has not been
changed in this regard.

Conclusion

The FAA reviewed the relevant data, considered the comment
received, and determined that air safety and the public interest
require adopting this final rule with the change described previously
and minor editorial changes. The FAA has determined that these minor
changes:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
The FAA also determined that these changes will not increase the
economic burden on any operator or increase the scope of this final
rule.

Related Service Information Under 1 CFR Part 51

Bombardier has issued the following service information:
Bombardier Service Bulletin 601R-25-201, Revision C, dated
May 11, 2017.
Bombardier Service Bulletin 670BA-25-100, Revision C,
dated May 11, 2017.

This service information describes procedures for repetitive detailed
inspections for damage of the cage assembly, WLPAs, and BOPs, and
repair or replacement of damaged parts. These documents are unique
since they apply to different airplane models.
Bombardier has also issued the following service information:
Bombardier CL-600-2B19 Temporary Revision (TR) 2A-69,
dated August 30, 2018.
CRJ Series Regional Jet (Bombardier) TR MRB-0079, dated
May 29, 2017.
This service information describes an airworthiness limitation task
for a detailed inspection of the aft cargo compartment WLPAs and BOPs.
These TRs are unique since they apply to different airplane models.
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 1,008 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs for Required Actions *

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Retained Inspections from AD 2015-24-04 2 work-hours x $85 per hour = $170
$0
$170
$171,360

* Table does not include estimated costs for revising the maintenance or
inspection program.

The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
agency recognizes that this number may vary from operator to operator.
In the past, the FAA has estimated that this action takes 1 work-hour
per airplane. Since operators incorporate maintenance or inspection
program changes for their affected fleet(s), the FAA has determined
that a per-operator estimate is more accurate than a per-airplane
estimate. Therefore, the FAA estimates the total cost per operator to
be $7,650 (90 work-hours x $85 per work-hour).
The FAA has received no definitive data that would enable the
agency to provide cost estimates for the on-condition actions specified
in this AD.

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 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.

Adoption of 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 removing Airworthiness Directive (AD)
2015-24-04, Amendment 39-18336 (80 FR 74673, November 30, 2015), and
adding the following new AD: