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2024-10-09 MHI RJ AVIATION ULC (TYPE CERTIFICATE PREVIOUSLY HELD BY BOMBARDIER, INC.): Amendment 39-22755; Docket No. FAA-2024-0219; Project Identifier MCAI-2023-00764-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective July 19, 2024.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to MHI RJ Aviation ULC  (Type  Certificate  previously
    held by Bombardier, Inc.) Model CL-600-2B19 (Regional Jet Series 100 &
    440) airplanes, certificated in any category,  as identified in Trans-
    port Canada AD CF-2023-41,  dated  June 15, 2023  (Transport Canada AD
    CF-2023-41).

(d) SUBJECT

    Air Transport Association (ATA) of America Code 05,  Time Limits/Main-
    tenance Checks.

(e) UNSAFE CONDITION

    This AD was prompted  by a determination  that a more restrictive air-
    worthiness limitation is necessary.  The  FAA  is  issuing  this AD to
    address failure of the strap modification to the fuselage station (FS)
    409 + 128 bulkhead.  The unsafe condition, if not addressed, could re-
    sult in the loss of the structural integrity of the airplane.

(f) COMPLIANCE

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

(g) REQUIREMENTS

    Except as specified in paragraph (h)  of this AD:  Comply with all re-
    quired actions and compliance times specified in,  and  in  accordance
    with, Transport Canada AD CF-2023-41.

(h) EXCEPTION TO TRANSPORT CANADA AD CF-2023-41

(1) Where Transport Canada AD CF-2023-41  refers  to  its  effective date,
    this AD requires using the effective date of this AD.

(2) Where paragraph A. of Transport Canada AD CF-2023-41 specifies to "in-
    corporate the revised task AWL number 53-41-180  in Appendix B  of the
    MRM CSP A-053 Part 2,"  this AD requires replacing that text with "re-
    vise the existing maintenance or inspection program, as applicable, by
    incorporating the revised task  AWL number 53-41-180  specified in MHI
    RJ Temporary Revision 2B-2283, dated March 16, 2023."

(3) The initial compliance time for doing the task  specified in paragraph
    A. of Transport Canada AD CF-2023-41 is at the applicable  "threshold"
    as specified in the service information referenced in paragraph B.  of
    Transport Canada AD CF-2023-41, or within 60 days after the  effective
    date of this AD, whichever occurs later.

(4) This AD does not adopt paragraph B. of Transport Canada AD CF-2023-41.

(i) PROVISIONS FOR ALTERNATIVE ACTIONS AND INTERVALS

    After the existing maintenance or inspection program  has been revised
    as required by paragraph (g) of this AD, no alternative actions (e.g.,
    inspections) and  intervals are  allowed unless  they are  approved as
    specified in  the provisions  of the  "Corrective Actions"  section of
    Transport Canada AD CF-2023-41.

(j) 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  (k)
    of  this   AD  or   email  to:   9-AVS-NYACO-COS@faa.gov.  If  mailing
    information,  also  submit  information  by  email.  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 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

    For more information about this AD contact Mark Taylor, Aviation Safe-
    ty Engineer, FAA,  1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
    phone 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) Transport Canada AD CF-2023-41, dated June 15, 2023.

(ii) [Reserved]

(3) For Transport Canada AD CF-2023-41 contact Transport Canada, Transport
    Canada National Aircraft Certification,  159 Cleopatra Drive,  Nepean,
    Ontario K1A 0N5,  Canada;  phone 888-663-3639;  email TC.Airworthiness
    Directives-Consignesdenavigabilite.TC@tc.gc.ca.   You  may  find  this
    Transport Canada AD  on the Transport Canada  website tc.canada.ca/en/
    aviation.

(4) You may view this material at the FAA, Airworthiness Products Section,
    Operational Safety Branch,  2200 South 216th Street,  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 May 15, 2024.  Victor Wicklund,  Deputy  Director,  Compliance &
Airworthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Mark Taylor,  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-2024-0219; Project Identifier MCAI-2023-00764-T;
Amendment 39-22755; AD 2024-10-09]
RIN 2120-AA64

Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.) Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain MHI RJ Aviation ULC Model CL-600-2B19 (Regional Jet Series 100
& 440) airplanes. This AD was prompted by a determination that a more
restrictive airworthiness limitation is necessary. This AD requires
revising the existing maintenance or inspection program, as applicable,
to incorporate a more restrictive airworthiness limitation, as
specified in a Transport Canada AD, which is incorporated by reference.
The FAA is issuing this AD to address the unsafe condition on these
products.

DATES: This AD is effective July 19, 2024.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 19,
2024.

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-0219; 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 material, contact Transport Canada, Transport Canada
National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario
K1A 0N5, Canada; telephone 888-663-3639; email
TC.AirworthinessDirectives-Consignesdenavigabilite.TC@tc.gc.ca; website
tc.canada.ca/en/aviation.
You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th Street,
Des Moines, WA. For information on the availability of this material at
the FAA, call 206-231-3195. It is also available in the AD docket at
regulations.gov under Docket No. FAA-2024-0219.

FOR FURTHER INFORMATION CONTACT: Mark Taylor, 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 MHI RJ Aviation
ULC Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. The
NPRM published in the Federal Register on February 2, 2024 (89 FR
7299). The NPRM was prompted by AD CF-2023-41, dated June 15, 2023,
issued by Transport Canada, which is the aviation authority for Canada
(Transport Canada AD CF-2023-41) (also referred to as the MCAI). The
MCAI states that a more restrictive airworthiness limitation has been
developed due to reports of an unclear effectivity for airworthiness
limitation (AWL) task number 53-41-180 in the Maintenance Requirements
Manual (MRM), Part 2. If the revised task, AWL number 53-41-180, is not
performed at the required intervals, failures of the strap modification
to the fuselage station (FS) 409 + 128 bulkhead could remain undetected
and could result in the loss of the structural integrity of the
airplane.
In the NPRM, the FAA proposed to require revising the existing
maintenance or inspection program, as applicable, to incorporate a more
restrictive airworthiness limitation, as specified in Transport Canada
AD CF-2023-41. The FAA is issuing this AD to address the unsafe
condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-0219.

Discussion of Final Airworthiness Directive

Comments

The FAA received comments from one commenter, Air Wisconsin
Airlines. The following presents the comments received on the NPRM and
the FAA's response to each comment.

Request for Change to Applicability

Air Wisconsin Airlines noted that the proposed applicability in
paragraph (c) of the proposed AD, which references the applicability in
Transport Canada AD CF-2023-41, does not list the applicable reference
serial numbers 7946 through 8113. The commenter requested that the
proposed AD be revised to list the applicable serial numbers, if they
are the same as those listed in Transport Canada AD CF-2023-41.
The FAA disagrees with correcting the applicability of this AD.
Paragraph (c) of this AD states that the AD affects the airplanes
identified in Transport Canada AD CF-2023-41, which has the
applicability as affecting airplanes with serial numbers 7946 through
8113. No changes have been made to this AD regarding this issue.

Request for Clarification of the Applicability of a Task

Air Wisconsin Airlines requested clarification of whether paragraph
(h)(2) of the proposed AD would require revising the maintenance or
inspection program to incorporate a revised task for all airplanes or
only certain airplanes.
The FAA agrees to clarify. Revising the maintenance or inspection
program to incorporate a revised AWL task affects all airplanes
identified in the applicability in paragraph (c) of the AD. A task
within an AWL might have an effectivity for specific airplanes. No
changes have been made to this AD regarding this issue.

Request for Clarification of the Fuselage Station of the Strap
Modification


Air Wisconsin Airlines requested that paragraph (e) of the proposed
AD regarding the location of the strap modification be changed from ``(FS)
409 and 128'' to ``(FS) 409 + 128''. MHI RJ TR 2B-2283 lists the
aircraft station as ``fuselage (FS) 409 + 128 bulkhead.'' In the NPRM,
the location is listed as ``(FS) 409 and 128 bulkhead,'' which sounds
like 2 different locations.
The FAA agrees with the commenter. The FAA has confirmed with the
manufacturer that the location of the strap modification is FS 409 +
128. The FAA has changed this final rule to reflect the proper
location.

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, considered the
comments received, 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, and any other changes described previously, this AD is adopted
as proposed in the NPRM. None of the changes will increase the economic
burden on any operator.

Related Service Information Under 1 CFR Part 51

Transport Canada AD CF-2023-41 specifies procedures for a more
restrictive airworthiness limitation for AWL task number 53-41-180.
This material 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 78 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the existing 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

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: