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2024-07-10 BOMBARDIER, INC.: Amendment 39-22731; Docket No. FAA-2023-2402; Project Identifier MCAI-2023-00370-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective June 6, 2024.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD  applies to Bombardier, Inc.,  Model CL-600-2B16 (604 Variant)
    airplanes,  certificated in any category,  with  serial  numbers  5301
    through 5665 inclusive, 5701 through 5990 inclusive, and 6050 and sub-
    sequent.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 32, Landing gear.

(e) UNSAFE CONDITION

    This AD was prompted  by a report indicating  that a new filter  plate
    connector for the nose wheel steering (NWS) system electronic  control
    module (ECM) does not meet certain certification requirements. The FAA
    is  issuing  this  AD  to  address  this  non-compliant  filter  plate
    connector, which, if  not replaced, could  result in a  malfunction of
    the  NWS  system  causing potential  uncommanded  steering  or lateral
    excursion from the runway.

(f) COMPLIANCE

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

(g) VERIFICATION OF AIRPLANE TECHNICAL RECORDS

    Within 24 months after the effective date of this AD: Inspect the ser-
    ial number of the ECM,  part number (P/N) 601-86100-27,  in accordance
    with Section 2.B.  Part A  of the Accomplishment Instructions  of  the
    applicable service information  listed in figure (1)  to the introduc-
    tory text of paragraph (g) of this AD  to determine if the serial num-
    ber of the ECM, P/N 601-86100-27, is listed in Table 1 of Section 1.A.
    of the applicable service information  listed in figure (1) to the in-
    troductory text of paragraph (g) of this AD.  A review  of maintenance
    records is also acceptable if the serial number of the ECM can be con-
    clusively determined from that review.

         FIGURE 1 TO THE INTRODUCTORY TEXT OF PARAGRAPH (G) -             
               APPLICABLE BOMBARDIER SERVICE BULLETINS                    
    ______________________________________________________________________
                                                        APPLICABLE
       MODEL                 SERIAL NOS.            BOMBARDIER SERVICE
                                                         BULLETIN
    ______________________________________________________________________
    CL-600-2B16           6050 and subsequent       650-32-006, dated
                                                    October 18, 2021

    CL-600-2B16           5701 through 5990         605-32-009, dated
                                                    October 18, 2021

    CL-600-2B16           5301 through 5665         604-32-032, dated
                                                    October 18, 2021
    ______________________________________________________________________

(1) If the serial number  of the ECM is listed in Table 1  of Section 1.A.
    of the applicable  service information or  is not reidentified  on the
    nameplate as SB-1,  then  the actions of paragraph (h) of this AD  are
    required.

(2) If the serial number  of the ECM is not  listed in Table 1  of Section
    1.A. of the applicable service  information or is reidentified on  the
    nameplate as SB-1, then  the actions of paragraph  (h) of this AD  are
    not required.

(h) REPLACEMENT

    For  airplanes  identified  in  paragraph (g)(1)  of this AD:  Do  the
    actions specified in paragraphs (h)(1) and (2) of this AD.

(1) Within 24 months after the effective date of this AD: Replace the ECM,
    P/N 601-86100-27,  identified  in  paragraph (g)(1)  of  this  AD,  in
    accordance with Section 2.C. Part B of the Accomplishment Instructions
    of the applicable service information listed in figure 1 to the intro-
    ductory text of paragraph (g) of this AD.

(2) Prior to return to service,  complete the operational test  of the NWS
    system in accordance  with Section 2.D. of the Accomplishment Instruc-
    tions of the applicable service information  listed in figure 1 to the
    introductory text of paragraph (g) of this AD.

(i) PARTS INSTALLATION LIMITATION

    As of the effective date of this AD,  it is prohibited to install ECM,
    P/N 601-86100-27,  as a replacement part,  if  the  serial  number  is
    listed in Table 1 of Section 1.A.  of  the applicable service informa-
    tion listed in figure 1  to the introductory text  of paragraph (g) of
    this AD,  unless the ECM  has been reidentified  with SB-1 on the name
    plate.

(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, International  Validation
    Branch, mail it to the address identified in paragraph (k)(2) 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  accom-
    plished using a method approved by the Manager,  International Valida-
    tion Branch, FAA; or Transport Canada; or Bombardier, Inc.'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-2023-14R1, dated May 15, 2023, for re-
    lated information.  This Transport Canada AD  may  be  found in the AD
    docket at regulations.gov under Docket No. FAA-2023-2402.

(2) For more information about this AD,  contact Steven Dzierzynski, Avia-
    tion Safety 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) Bombardier Service Bulletin 604-32-032, dated October 18, 2021.

(ii) Bombardier Service Bulletin 605-32-009, dated October 18, 2021.

(iii) Bombardier Service Bulletin 650-32-006, dated October 18, 2021.

(3) For service information identified in this AD, contact Bombardier Bus-
    iness Aircraft  Customer  Response  Center,  400 Cote-Vertu Road West,
    Dorval, Quebec H4S 1Y9, Canada;  telephone 514-855-2999; email ac.yul@
    aero.bombardier.com; website bombardier.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 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 April 2, 2024.  Victor Wicklund,  Deputy Director,  Compliance &
Airworthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, Aviation Safety Engi-
neer, 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-2023-2402; Project Identifier MCAI-2023-00370-T;
Amendment 39-22731; AD 2024-07-10]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model CL-600-2B16 (604 Variant) airplanes.
This AD was prompted by a report indicating that a new filter plate
connector for the nose wheel steering (NWS) system electronic control
module (ECM) does not meet certain certification requirements. This AD
requires replacing all affected ECMs. This AD also prohibits the
installation of affected parts under certain conditions. The FAA is
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective June 6, 2024.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of June 6, 2024.

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-2402; 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 service information identified in this final rule,
contact Bombardier Business Aircraft Customer Response Center, 400
Cote-Vertu Road West, Dorval, Quebec H4S 1Y9, Canada;
telephone 514-855-2999; email ac.yul@aero.bombardier.com; website
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. It is also available at
regulations.gov under Docket No. FAA-2023-2402.

FOR FURTHER INFORMATION CONTACT: Steven Dzierzynski, 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 Bombardier,
Inc., Model CL-600-2B16 (601-3A, 601-3R, and 604 Variants) airplanes.
The NPRM published in the Federal Register on December 28, 2023 (88 FR
89633). The NPRM was prompted by AD CF-2023-14R1, dated May 15, 2023
(Transport Canada AD CF-2023-14R1) (referred to after this as the
MCAI), issued by Transport Canada, which is the aviation authority for
Canada. The MCAI states that the manufacturer of the NWS system ECM,
part number (P/N) 601-86100-27, introduced a new filter plate connector
that does not meet the certification requirements related to the
susceptibility of electronic components to high intensity radiated
field. This non-compliant filter plate connector, if not replaced,
could result in a malfunction of the NWS system causing potential un-
commanded steering or lateral excursion from the runway.
In the NPRM, the FAA proposed to require replacing all affected
non-compliant ECMs. 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-2023-2402.

Discussion of Final Airworthiness Directive

Comments

The FAA received comments from two commenters, Bombardier and
NetJets. The following presents the comments received on the NPRM and
the FAA's response to each comment.

Request to Provide a Figure Title

Both Bombardier and NetJets requested that a title be provided for
the figure referenced in paragraph (g) of the NPRM because the title is
missing.
The FAA agrees. The title ``Figure 1 to the introductory text of
paragraph (g)--Applicable Bombardier Service Bulletins'' has been added
to the referenced figure.

Request To Change the Applicability

Bombardier also requested that the Applicability of the proposed AD
be changed. Bombardier noted that Model 601-3A and 601-3R variants are
not impacted by this issue and should not be subject to this AD.
The FAA agrees. The Applicability of this AD has been changed
accordingly.

Request for Clarification of Service Information Effectivity

NetJets noted that Bombardier Service Bulletin 650-32-006 is
effective only for serial numbers 6050 through 6171. NetJets requested
that the proposed AD be revised to provide direction for airplane
serial numbers outside that range.
The FAA does not agree to revise this AD but will clarify.
Bombardier has confirmed that all instructions in Service Bulletin 650-
32-006 can be accomplished on serial numbers 6172 and subsequent.
Because the affected ECMs are rotable parts, the FAA has determined
that these parts could later be installed on airplanes that were
initially delivered with acceptable ECMs, thereby subjecting those
airplanes to the unsafe condition. The FAA has not changed this AD as a
result of this comment.

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

The FAA reviewed the following Bombardier service information.
Service Bulletin 604-32-032, dated October 18, 2021.
Service Bulletin 605-32-009, dated October 18, 2021.
Service Bulletin 650-32-006, dated October 18, 2021.
This service information specifies procedures for removing and
replacing all affected non-compliant ECMs, P/N 601-86100-27. 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.

Costs of Compliance

The FAA estimates that this AD affects 164 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs for Required Actions

Labor cost
Parts cost
Cost per product
Cost on U.S. operators
6 work-hours x $85 per hour = $510
$75,972
$76,482
$12,543,048

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this AD may be covered under warranty, thereby reducing the cost impact
on affected operators.

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: