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PROPOSED AD MHI RJ AVIATION ULC (TYPE CERTIFICATE PREVIOUSLY HELD BY BOMBARDIER, INC.): Docket No. FAA-2023-0167; Project Identifier MCAI-2022-00762-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    April 3, 2023.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to  all  MHI  RJ  Aviation  ULC  (Type  Certificate
    previously  held   by  Bombardier,   Inc.)  airplanes   identified  in
    paragraphs  (c)(1)  through  (6)  of  this  AD,  certificated  in  any
    category.

(1) Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes.

(2) Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes.

(3) Model CL-600-2C11 (Regional Jet Series 550) airplanes.

(4) Model CL-600-2D15 (Regional Jet Series 705) airplanes.

(5) Model CL-600-2D24 (Regional Jet Series 900) airplanes.

(6) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.

(d) SUBJECT

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

(e) REASON

    This AD was prompted by  a determination that new or  more restrictive
    aircraft maintenance manual (AMM) tasks and certification  maintenance
    requirement (CMR) tasks are necessary.  The FAA is issuing this  AD to
    address  undetected  loss  of fire  extinguishing  capability  for the
    engine,  APU,  or  cargo compartment.  The  unsafe  condition, if  not
    addressed, could  result in  an inability  to put  out a  fire in  the
    engine, APU, or cargo compartment area.

(f) COMPLIANCE

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

(g) MAINTENANCE OR INSPECTION PROGRAM REVISION  FOR MODEL CL-600-2B19 AIR-
    PLANES

    For Model CL-600-2B19  airplanes: Within 60  days after the  effective
    date  of  this  AD,  revise  the  existing  maintenance  or inspection
    program, as  applicable, to  incorporate the  information specified in
    Bombardier Temporary  Revisions 2A-73  and 2A-74,  both dated  June 5,
    2020. The initial compliance time for  doing the tasks is at the  time
    specified  in  Bombardier  Temporary Revisions  2A-73 and  2A-74, both
    dated June 5, 2020, or within 60 days after the effective date of this
    AD, whichever occurs later.

(h) MAINTENANCE OR INSPECTION PROGRAM REVISION FOR OTHER MODEL AIRPLANES

    For airplanes identified in paragraphs (c)(2) through (6) of this AD:

(1) Within 60 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the information specified in Figure 1 to paragraph (h)(1) of this  AD.
    The initial compliance  time for doing  the task is  at the applicable
    time specified in paragraph (h)(1)(i) or (ii) of this AD.

    FIGURE 1 TO PARAGRAPH (H)(1) -AMM TASK FOR THE CARGO FIRE EXTINGUISHER
                                  BOTTLE                                  
    ______________________________________________________________________
                                   INTERVAL
    EFFECTIVITY                   LIMITATION              AMM TASK NOS.
    ______________________________________________________________________
        All                        10 years           26-25-01-610-801-A01
                                                      26-25-01-610-801-A02
    ______________________________________________________________________

(i) If a restoration  (previously called a hydrostatic test)  of any cargo
    compartment fire  extinguisher bottle  was accomplished  on or  before
    June 5, 2014, do the applicable maintenance task on that bottle within
    48 months after the effective date of this AD, whichever occurs later.

(ii) If a restoration (previously called a hydrostatic test)  of any cargo
     compartment fire extinguisher bottle  was accomplished  after June 5,
     2014, do  the applicable  maintenance task  on that  bottle within 10
     years after the most recent restoration was accomplished.

(2) Within 60 days after the effective date of this AD,  revise the exist-
    ing maintenance or inspection  program, as applicable, to  incorporate
    the information specified in Figure 2 to paragraph (h)(2) of this  AD.
    The initial compliance  time for doing  the task is  at the applicable
    time specified in paragraph (h)(2)(i) or (ii) of this AD.

     FIGURE 2 TO PARAGRAPH (H)(2) - AMM TASKS FOR THE ENGINE AND APU FIRE 
                                    EXTINGUISHER BOTTLES                  
    ______________________________________________________________________
                                   INTERVAL
    EFFECTIVITY                   LIMITATION              AMM TASK NOS.
    ______________________________________________________________________
        All                        10 years           26-21-07-610-801-A01
                                                      26-21-07-610-801-A02
                                                      26-22-07-610-801-A01
                                                      26-22-07-610-801-A02
    ______________________________________________________________________

(i) If a restoration (previously called a hydrostatic test)  of any engine
    or  auxiliary   power  unit   (APU)  fire   extinguisher  bottle   was
    accomplished on or before June 5, 2014, do the applicable  maintenance
    task on that bottle within 48 months after the effective date of  this
    AD.

(ii) If a restoration (previously called a hydrostatic test) of any engine
     or APU fire extinguisher bottle was accomplished  after June 5, 2014,
     do the  applicable maintenance  task on  that bottle  within 10 years
     after the most recent restoration was accomplished.

(i) NO ALTERNATIVE ACTIONS, OR INTERVALS

    After the existing maintenance or inspection program has been  revised
    as  required by  paragraphs (g)  and (h)  of this  AD, no  alternative
    actions  (e.g.,  inspections), or  intervals  may be  used  unless the
    actions,  and  intervals  are approved  as  an  alternative method  of
    compliance  (AMOC)  in  accordance with  the  procedures  specified in
    paragraph (j)(1) of this AD.

(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
    responsible  Flight  Standards  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.  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,  New York  ACO
    Branch, FAA; or Transport Canada;  or MHI RJ Aviation ULC's  Transport
    Canada Design Approval Organization (DAO). If approved by the DAO, the
    approval must include the DAO-authorized signature.

(k) ADDITIONAL INFORMATION

(1) Refer to Transport Canada AD CF-2022-32,  dated June 13, 2022, for re-
    lated information.  This Transport  Canada AD  may be  found in the AD
    docket at regulations.gov under Docket No. FAA-2023-0167.

(2) For more information about this AD, contact Gabriel Kim, Aerospace En-
    gineer,  Mechanical Systems and Administrative Services Section,  FAA,
    New York  ACO Branch,  1600 Stewart Avenue,  Suite  410,  Westbury, NY
    11590; telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov.

(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 Temporary Revision 2A-73, dated June 5, 2020.

(ii) Bombardier Temporary Revision 2A-74, dated June 5, 2020.

(3) For service information identified in this AD, contact MHI RJ Aviation
    Group, Customer Response Center, 3655 Ave des Grandes-Tourelles, Suite
    110, Boisbriand, Quebec J7H 0E2 Canada;  North America toll-free tele-
    phone 833-990-7272 or direct-dial telephone 450-990-7272; fax 514-855-
    8501; email thd.crj@mhirj.com; website mhirj.com.

(4) You may view this service information at the FAA,  Airworthiness Prod-
    ucts 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 service information  that is incorporated by refer-
    ence at the National Archives and Records Administration  (NARA).  For
    information on the availability  of this material  at NARA,  email fr.
    inspection@nara.gov,  or go to: www.archives.gov/federal-register/cfr/
    ibr-locations.html.

Issued on February 10, 2023. Christina Underwood, Acting Director, Compli-
ance & Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD by April 3, 2023.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-0167; Project Identifier MCAI-2022-00762-T]
RIN 2120-AA64

Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by 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 all MHI RJ Aviation ULC Model CL-600-2B19 (Regional Jet Series 100
& 440); CL-600-2C10 (Regional Jet Series 700, 701, & 702); CL-600-2C11
(Regional Jet Series 550); CL-600-2D15 (Regional Jet Series 705); CL-
600-2D24 (Regional Jet Series 900); and CL-600-2E25 (Regional Jet
Series 1000) airplanes. This proposed AD was prompted by a
determination that aircraft maintenance manual (AMM) tasks and
certification maintenance requirement (CMR) tasks are necessary. This
proposed AD would require revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive AMM and CMR tasks. 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 April 3,
2023.

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-2023-0167; 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 service information identified in this NPRM, contact
MHI RJ Aviation Group, Customer Response Center, 3655 Ave. des Grandes-
Tourelles, Suite 110, Boisbriand, Quebec J7H 0E2 Canada; North
America toll-free telephone 833-990-7272 or direct-dial telephone 450-
990-7272; fax 514-855-8501; email thd.crj@mhirj.com; website mhirj.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: Gabriel Kim, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 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-2023-0167; Project Identifier
MCAI-2022-00762-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
Gabriel Kim, Aerospace Engineer, Mechanical Systems and Administrative
Services Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 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-2022-32, dated June 13, 2022, (Transport
Canada AD CF-2022-32) (also referred to after this as the MCAI), to
correct an unsafe condition for all MHI RJ Aviation ULC Model CL-600-
2B19 (Regional Jet Series 100 & 440); CL-600-2C10 (Regional Jet Series
700, 701, & 702); CL-600-2C11 (Regional Jet Series 550); CL-600-2D15
(Regional Jet Series 705); CL-600-2D24 (Regional Jet Series 900); and
CL-600-2E25 (Regional Jet Series 1000) airplanes. The MCAI states that
it was discovered that the 10-year (120 months) periodic hydrostatic
tests of the engine and auxiliary power unit (APU)
fire extinguishing bottles on Model CL-600-2B19 airplanes and of the
engine, APU, and cargo compartment fire extinguishing bottles for Model
CL-600-2C10; CL-600-2C11; CL-600-2D15; CL-600-2D24; and CL-600-2E25
airplanes were not performed. This could mean that the functional test
of the pressure switch, which should be performed as part of the
hydrostatic tests, may have been omitted on several airplanes in
service. Failure to perform the pressure switch test and the 10-year
overhaul or restoration of the FIREX bottles could result in a dormant
loss of fire extinguishing capability.
The FAA is proposing this AD to address undetected loss of fire
extinguishing capability for the engine, APU, or cargo compartment. The
unsafe condition, if not addressed, could result in an inability to put
out a fire in the engine, APU, or cargo compartment area. You may
examine the MCAI in the AD docket at regulations.gov under Docket No.
FAA-2023-0167.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Bombardier Temporary Revisions 2A-73 and 2A-74,
both dated June 5, 2020. This service information specifies new or more
restrictive CMR tasks.
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 ADDRESSES.

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 revising the existing maintenance or
inspection program, as applicable, to incorporate new or more
restrictive AMM and CMR tasks.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance according to paragraph
(j)(1) of this proposed AD.

Differences Between This AD and the MCAI or Service Information

Transport Canada AD CF-2022-32 introduces new candidate
certification maintenance requirement (CCMR) intervals that the FAA
cannot mandate as CCMRs as specified in the MCAI. Therefore, the FAA
proposes to mandate two AMM tasks as specified in Figure 1 to paragraph
(h)(1) of this proposed AD and four AMM tasks as specified in Figure 2
to paragraph (h)(2) of this proposed AD.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 1,114 airplanes of U.S. registry. The FAA estimates the
following costs to comply with this proposed AD:
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.
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
agency estimates the average total cost per operator to be $7,650 (90
work-hours x $85 per work-hour).

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: