Proposed Rule2026-07881
Airworthiness Directives; Bombardier, Inc., Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
April 23, 2026
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to adopt a new airworthiness directive (AD) for certain Bombardier, Inc. Model BD-700-1A10, and BD-700-1A11 airplanes. This proposed AD was prompted by an in-service event where a main landing gear tire burst upon landing. This proposed AD would require an inspection to determine if an affected brake control unit (BCU) is installed and replacement of affected BCU. This proposed AD would also prohibit the installation of affected parts. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 91 Issue 78 (Thursday, April 23, 2026)</title>
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[Federal Register Volume 91, Number 78 (Thursday, April 23, 2026)]
[Proposed Rules]
[Pages 21747-21749]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2026-07881]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2026-3864; Project Identifier MCAI-2022-01215-T]
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 BD-700-1A10, and BD-700-1A11
airplanes. This proposed AD was prompted by an in-service event where a
main landing gear tire burst upon landing. This proposed AD would
require an inspection to determine if an affected brake control unit
(BCU) is installed and replacement of affected BCU. This proposed AD
would also prohibit the installation of affected parts. 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 June 8,
2026.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> 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 <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2026-3864; 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:
<bullet> For Transport Canada material identified in this proposed
AD, contact Transport Canada, Transport Canada National Aircraft
Certification, 159 Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada;
telephone 888-663-3639; email <a href="/cdn-cgi/l/email-protection#5a0e19741b33282d35282e3233343f29291e33283f392e332c3f297719353429333d343f293e3f343b2c333d3b383336332e3f740e191a2e39743d3974393b"><span class="__cf_email__" data-cfemail="d58196fb94bca7a2baa7a1bdbcbbb0a6a691bca7b0b6a1bca3b0a6f896babba6bcb2bbb0a6b1b0bbb4a3bcb2b4b7bcb9bca1b0fb819695a1b6fbb2b6fbb6b4">[email protected]</span></a>. You may find this material on the
Transport Canada website at tc.canada.ca/en/aviation. It is also
available at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2026-3864.
<bullet> You may view this material 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: Elizabeth Dowling, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
phone: 516-228 7300; email: <a href="/cdn-cgi/l/email-protection#e5a0898c9f848780918dcba8cba18a92898c8b82a5838484cb828a93"><span class="__cf_email__" data-cfemail="cd88a1a4b7acafa8b9a5e380e389a2baa1a4a3aa8dabacace3aaa2bb">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments using a method listed
under the ADDRESSES section. Include ``Docket No. FAA-2026-3864;
Project Identifier MCAI-2022-01215-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 this 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
<a href="http://regulations.gov">regulations.gov</a>, 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
Elizabeth Dowling, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone: 516-228 7300; email:
<a href="/cdn-cgi/l/email-protection#b6f3dadfccd7d4d3c2de98fb98f2d9c1dadfd8d1f6d0d7d798d1d9c0"><span class="__cf_email__" data-cfemail="e0a58c899a8182859488ceadcea48f978c898e87a0868181ce878f96">[email protected]</span></a>. Any commentary that the FAA receives which
is not specifically designated as CBI will be placed in the public
docket for this rulemaking.
[[Page 21748]]
Background
Transport Canada, which is the aviation authority for Canada, has
issued Transport Canada AD CF-2022-53, dated September 22, 2022 (also
referred to as the MCAI), to correct an unsafe condition for certain
Bombardier, Inc. Model BD-700-1A10, BD-700-1A11 airplanes. The MCAI
states an in-service event occurred where a main landing gear tire
burst upon landing. The investigation into the event found that with
the loss of a 5V power supply in the BCU wheel control card, a residual
current may build within the brake control valve (BCV) driver circuit.
This residual current may result in uncommanded brake pressure during
landing. If not corrected, this can cause one or more tires to burst
due to a dragging brake or a locked brake, unexpected deceleration,
degraded braking performance, directional difficulties, or brake(s)
overheating.
The FAA is proposing this AD to address the unsafe condition on
these products.
You may examine the MCAI in the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2026-3864.
Material Incorporated by Reference Under 1 CFR Part 51
Transport Canada AD CF-2022-53 specifies procedures for an
inspection to determine if BCUs with part number (P/N) GW415-7125-7
(Crane P/N 42-965-3) are installed, and replacement of affected parts
with BCU P/N GW415-7125-9 (Crane P/N 42-965-4). Transport Canada also
prohibits the installation of affected parts.
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.
FAA's Determination
These products have been approved by the civil aviation authority
of another country and are approved for operation in the United States.
Pursuant to the FAA's bilateral agreement with this State of Design
Authority, that authority has notified the FAA of the unsafe condition
described in the MCAI referenced above. The FAA is issuing this NPRM
after determining that the unsafe condition described previously is
likely to exist or develop in other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD would require accomplishing the actions specified
in Transport Canada AD CF-2022-53 described previously, except for any
differences identified as exceptions in the regulatory text of this
proposed AD.
Explanation of Required Compliance Information
In the FAA's ongoing efforts to improve the efficiency of the AD
process, the FAA developed a process to use some civil aviation
authority (CAA) ADs as the primary source of information for compliance
with requirements for corresponding FAA ADs. The FAA has been
coordinating this process with manufacturers and CAAs. As a result, the
FAA proposes to incorporate Transport Canada AD CF-2022-53 by reference
in the FAA final rule. This proposed AD would, therefore, require
compliance with Transport Canada AD CF-2022-53 in its entirety through
that incorporation, except for any differences identified as exceptions
in the regulatory text of this proposed AD. Material required by
Transport Canada AD CF-2022-53 for compliance will be available at
<a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-2026-3864 after the FAA final rule
is published.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 42 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
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Cost per Cost on U.S.
Labor cost Parts cost product operators
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2 work-hours x $85 per hour = $170........................... $0 $170 $7,140.00
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The FAA estimates the following costs to do any necessary on-
condition action 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 action:
Estimated Costs of On-Condition Actions
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Labor cost Parts cost Cost per product
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2 work-hours x $85 per hour = $170....... Up to $430,089.............. Up to $430,259.
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The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed 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
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
[[Page 21749]]
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
0
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]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
Bombardier, Inc.: Docket No. FAA-2026-3864; Project Identifier MCAI-
2022-01215-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by June 8, 2026.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model BD-700-1A10 and BD-
700-1A11 airplanes, certificated in any category, as identified in
Transport Canada AD CF-2022-53, dated September 22, 2022 (Transport
Canada AD CF-2022-53).
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
Gear.
(e) Unsafe Condition
This AD was prompted by an in-service event where a main landing
gear tire burst upon landing. The investigation into the event found
that with the loss of a 5V power supply in the brake control unit
(BCU) wheel control card, a residual current may build within the
brake control valve (BCV) driver circuit. This residual current may
result in uncommanded brake pressure during landing. The unsafe
condition, if not addressed, could result in one or more tires to
burst due to a dragging brake or a locked brake, unexpected
deceleration, degraded braking performance, directional
difficulties, or brake(s) overheating.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraphs (h) and (i) of this AD: Comply
with all required actions and compliance times specified in, and in
accordance with, Transport Canada AD CF-2022-53.
(h) Exception to Transport Canada AD CF-2022-53
Where Transport Canada AD CF-2022-53 refers to its effective
date, this AD requires using the effective date of this AD.
(i) No Reporting Requirement and No Return of Parts
Although the material referenced in Transport Canada AD CF-2022-
53 specifies to submit certain information and return parts to the
manufacturer, this AD does not include those requirements.
(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, send it to the attention of the
person identified in paragraph (j) of this AD and email to:
<a href="/cdn-cgi/l/email-protection#96d7dbd9d5d6f0f7f7b8f1f9e0"><span class="__cf_email__" data-cfemail="a3e2eeece0e3c5c2c28dc4ccd5">[email protected]</span></a>. 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 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
For more information about this AD, contact Elizabeth Dowling,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; phone: 516-228 7300; email:
<a href="/cdn-cgi/l/email-protection#6f2a0306150e0d0a1b074122412b0018030601082f090e0e41080019"><span class="__cf_email__" data-cfemail="9dd8f1f4e7fcfff8e9f5b3d0b3d9f2eaf1f4f3faddfbfcfcb3faf2eb">[email protected]</span></a>.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference of the material listed in this paragraph
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this material as applicable to do the actions
required by this AD, unless this AD specifies otherwise.
(i) Transport Canada AD CF-2022-53, dated September 22, 2022.
(ii) [Reserved]
(3) For Transport Canada material identified in this AD, contact
Transport Canada, Transport Canada National Aircraft Certification,
159 Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; telephone 888-
663-3639; email <a href="/cdn-cgi/l/email-protection#1a4e59345b73686d75686e7273747f69695e73687f796e736c7f693759757469737d747f697e7f747b6c737d7b787376736e7f344e595a6e79347d7934797b"><span class="__cf_email__" data-cfemail="782c3b5639110a0f170a0c1011161d0b0b3c110a1d1b0c110e1d0b553b17160b111f161d0b1c1d16190e111f191a1114110c1d562c3b380c1b561f1b561b19">[email protected]</span></a>. You may find this material on
the Transport Canada website at tc.canada.ca/en/aviation.
(4) You may view this material 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.
(5) You may view this material at the National Archives and
Records Administration (NARA). For information on the availability
of this material at NARA, visit <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a> or email <a href="/cdn-cgi/l/email-protection#3a5c48145354494a5f594e5355547a545b485b145d554c"><span class="__cf_email__" data-cfemail="2b4d59054245585b4e485f4244456b454a594a054c445d">[email protected]</span></a>.
Issued on April 20, 2026.
Steven W. Thompson,
Acting Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2026-07881 Filed 4-22-26; 8:45 am]
BILLING CODE 4910-13-P
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